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Garmin Software Version 0563.11 Cockpit Reference Guide

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1. Af k A f TUG _ lt F O w ee 5 ATI r A 7 On 9 M Figure 7 42 Turn to intercept OPSHN to FSHER Leg 190 00384 09 Rev A SECTION 7 NAVIGATION 19 After passing OPSHN the next leg of the arrival turns magenta as shown in Figure 7 43 The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active os 115x om d52 Tek 352 AARRE 196 975 118 688 con FPL ACTIVE FLIGHT PLAN 136 975 118 000 cone DEAE Lila P F WORTH UF ACTIVE FLIGHT PLAN KHEC KCOS ri hd J r Gl TE BPYNON Ber vaag KOTO tein mel see T TBE is Arrival KOOS TBEDBRY TALL OPSHN 31H ee eee a FT KFU pug OPSHN ee PT s i FSHER 357 G n 10300FT PYNON 357 11 9 10300FT Aperooch KCOS RNAV 35Rors LPY HABLE iof a21 ROH 3000F FALUR 261 KINH BDO CEGIM fof 351 EWH 7Bir CURRENT VHV PROFILE ACTIVE UNU WPT SOOOFT of HABLE iof WS TGT D SFPH FPA 25 VS REQ F TIHE TOTOO 1004 S ry FPL Figure 7 43 Tracking the OPSHN to FSHER Leg 20 The flight continues through the arrival procedure to PYNON see Figure 7 44 At a point 31 nautical miles from the destination airport the phase of flight scaling for the CDI changes to Terminal Mode and is annunciated by displaying TERM on the HSI There will be a descent to HABUK in the next leg Note the TOD point on the map Annunciations for the upcoming turn and descent as well as the VDI and
2. 6 2 6 2 FLIGHT DIRECTOR OPERATION With the flight director activated the aircraft can be hand flown to follow the path shown by the Command Bars Maximum commanded pitch 20 15 and bank 22 angles vertical acceleration and roll rate are limited to values established during AFCS certification The flight director also provides commands to the autopilot Activating the Flight Director Pressing the FD or AP Key when the flight director is not active activates the flight director in default pitch roll modes Pushing the GA Switch or any flight director mode key activates the flight director in the respective mode s The flight director may be turned off by pressing the FD Key Command Bars Upon activation of the flight director Command Bars are displayed on the PFD as a single cue If the attitude information sent to the flight director becomes invalid or unavailable the Command Bars are removed from the display The Command Bars do not override the aircraft symbol Command Bars T T Aircraft Symbol Figure 6 2 Command Bars Autopilot Roll Modes Status Pitch Modes Armed Active Active Mode Amed Reference AFCS Status Box Command Bars 110 100 Selected Heading TAS 120KT GPS is Selected Navigation Source INSET 136 975 136 975 8 888 con 11 118 888 conz Selected Altitude Selected Course XPDR IDENT TMR REF NRST Figure 6 3 PFD AFCS Display Garmin G1000 Cockpit Reference
3. 2 Turn the large FMS Knob to move the cursor to the Frequencies box 3 Turn either FMS Knob to scroll through the list placing the cursor on the desired frequency If a listed frequency has sector or altitude restrictions the frequency is preceded by an info i designation Press the ENT Key to view the information The following may be displayed with the frequency e TX transmit only e RX receive only e PT part time frequency 4 Press the ENT Key to place the selected frequency in the standby field of the COM or NAV box 5 To remove the cursor press the FMS Knob Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 23 SECTION 7 NAVIGATION 7 5 INTERSECTION INFORMATION 7 6 NDB INF 17 95 ORMATION NOE I t Select the Intersection Information Page NORTH LIP iN 1 Turn the large FMS Knob to select the WPT page z R Qroup z a ftv 2 Turn the small FMS Knob to select the second Satie rectangular page icon Figure 7 58 NDB Information Page Select the NDB Information Page 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the third rectangular page icon Figure 7 57 Intersection Information Page Access Information on an Intersection View Information on a Specific NDB 1 With the Intersection Information Page displayed 1 With the NDB Information Page displayed press press the F
4. Figure 6 31 Departure 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 25 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 26 Intercepting a VOR Radial During climb out the autopilot continues to fly the aircraft in Heading Select Mode Airway V4 to Salina VOR SLN should now be intercepted Since the enroute flight plan waypoints correspond to VORs flight director Navigation Mode using either VOR or GPS as the navigation source may be used In this scenario VOR Navigation Mode is used for navigation to the first VOR waypoint in the flight plan Intercepting a VOR radial 1 Arm VOR Navigation Mode a Tune the VOR frequency b Press the CDI Softkey to set the navigation source to VOR c Use the CRS Knob to set the Selected Course to 255 Note that at this point the flight director is still in Heading Select Mode and the autopilot continues to fly 290 Salina VOR d Press the NAV Key This arms VOR Navigation Mode and the white VOR annunciation appears to the left of the active lateral mode VOR HDG AP ALT 12000FT 2 As the aircraft nears the Selected Course the flight director transitions trom Heading Select to VOR Navigation Mode and the VOR annunciation flashes green The autopilot begins turning to intercept the Selected Course 3 The autopilot continues the turn until the aircraft is established on the Selected Course Figure 6 32 Interceptin
5. 2 SECTION 4 NAV COM amp TRANSPONDER Enter Code Using Softkeys Press the XPDR Softkey to display the transponder Mode Selection softkeys Press the CODE Softkey to display the transponder Code Selection softkeys which includes the digit softkeys Press the appropriate digit softkeys to enter the code in the four digit code field of the Transponder Status Box When the last digit is entered the transponder code becomes active When entering a code press the BKSP Softkey as needed to back up and change code digits Enter Code Using the FMS Knob 1 2 Press the XPDR Softkey to display the transponder Mode Selection softkeys Press the CODE Softkey to display the transponder Code Selection softkeys which includes the digit softkeys Turn the small FMS Knob to enter the first two digits Turn the large FMS Knob to place the cursor in position to change the second two digits Turn the small FMS Knob to enter the second two digits Press the ENT Key to activate the code immediately or wait 10 seconds and the code will become active Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 4 5 SECTION 4 NAV COM amp TRANSPONDER Flight ID Reporting If so configured the Flight ID may be entered in the Timer Reterence Window REFERENCES TIMER 0 00 00 UP START GLIDE SOKT OFF MINIMUMS 4BARO 15 FT FLIGHT ID AIR265 Flight ID Figure 4 16 Timer References Window 1 Press
6. 5500 5000 DON T SINK 4500 Height Above Terrain Feet 0 500 1000 1500 2000 2500 3000 3500 4000 Sink Rate Feet Per Minute 4000 3500 Figure 10 29 Negative Climb Rate 3000 Five Hundred Aural Alert The purpose of the aural alert message Five hundred is to provide an advisory alert to the air crew that the aircraft is five hundred feet above terrain When the 1000 aircraft descends within 500 feet of terrain the aural message Five hundred is heard There are no display annunciations or pop up alerts that accompany the aural 2000 4000 6000 8000 10000 12000 message Descent Rate 2500 2000 Height Above Terrain Feet 1500 Figure 10 28 Excessive Descent Rate Displaying Terrain and Obstacles on the Navigation Map Negative Climb Rate After Takeoff 1 With the Navigation Map displayed press the MAP Alert NCR Softkey The purpose of the Negative Climb Rate After Takeoff 2 Press the TERRAIN Softkey Terrain and obstacle alert is to provide suitable alerts to the pilot when the proximity are now displayed on the map system determines that the aircraft is losing altitude closing upon terrain after takeoff The aural message Don t Sink is given for NCR alerts accompanied by an annunciation and a pop up terrain alert on the display Figure 10 29 illustrates the envelope for alerts 190 00384 09 Rev A Garmin G1000 Cockpit Reference G
7. The COM1 and or COM2 transfer switch is stuck in the enabled or pressed posi 7 tion Press the transfer switch again to cycle its operation If the problem persists COM2 RMT XFR COM2 remote the G1000 system should be serviced transfer key is stuck RAIM UNAVAIL RAIM is not GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity available trom FAF to MAP waypoints Monitoring RAIM from the FAF to the MAP waypoints LOI GPS integrity lost Crosscheck es NE with other NAVYS Loss of GPS integrity monitoring ik a iol J o Jeo Loss of GPS navigation due to insufficient satellites tion Insufficient satellites wii ay pie 7 ae Loss of GPS navigation due to position error E navigation Position error GPS NAV LOST 7 Loss of GPS Loss of GPS navigation due to GPS failure navigation GPS tail ABORT APR Loss ol GPS navigation ai approach due to loss of GPS navigation Abort approach 13 14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 13 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Message Comments S O TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav Change hdg reference to TRUE angle is set to AUTO iat aa ll A failure has been detected in the GPS1 and or GPS2 receiver The receiver is GPS2 FAIL GPS2 is inoperative unavailable The G1000 syst
8. 16 Upon reaching TOD a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7 40 coo i Keep Vertical Align Indicated Deviation Pointer __ Vertical Speed Centered with Required Vertical Speed Figure 7 40 VDI amp RVSI Showing Correctly Established Descent 17 When the aircraft is one minute from the bottom of descent BOD this is annunciated as shown in Figure 7 41 Upon reaching the OPSHN offset waypoint three miles before OPSHN the aircraft will be at 10 000 feet 122 008 ee e o z 7 Figure 7 41 Approaching Bottom of Descent BOD at OPSHN 190 00384 09 Rev A 18 The aircraft is approaching OPSHN The upcoming turn and next heading is annunciated at the top left of the PFD as seen in Figure 7 42 Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI 136 975 136 975 Lis Tr 258 ere H0 39 136 975 118 688 com PL ACTIVE FLIGHT PLAN 196 975 118 000 cone NORTH UP ns LT ACTIVE FLIGHT PLAN KIKE KCOS Airway W263 TBE KOWTO TBE Se ae Arrival KCOS TBE DBRY 7ALL OPSHH 3HH OPSHY PY HOM 352 11 9 SAORFT Approach RCOS RNAV 35Riors LPY HABUK inf B Sih so00r1 FALUR 261 SOH BED CURRENT Vii PROFILE ACTIVE UNU WPT SOOOFT of HABLE iof WS TGT DE3FPH FPA 2 WS REQ 136 975 136 975
9. 4 VS REQ V DEV Figure 7 19 V4 is Loaded in the Flight Plan 5 V4 is now made the active leg of the flight plan a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight SLN The TO waypoint of the leg is selected in order to activate the leg c Press the ACT LEG Softkey The confirmation window is now displayed as in Figure 7 20 Note the TOP to SLN leg is actually part of V4 TOP gt SLN ACTIVAT ERT umn O16 31 Figure 7 20 Comfirm Active Leg d Verity the displayed leg is the desired leg and press the ENT Key Note in Figure 7 21 the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg Note also the crosstrack 190 00384 09 Rev A SECTION 7 NAVIGATION XTK distance on the HSI indicating 16 9 nm to the intercept point Note the phase of flight remained in Terminal TERM mode up to this point because a departure leg was active Since aleg after the departure is now active the current CDI flight phase is ENR Enroute and CDI scaling has changed to 2 0 nm om 259 Tk 4 eve 9 46 136 975 118 088 com FPL ACTIVE FLIGHT PLAN 136 975 118 000 conz _HORTH UF ACTIVE FLIGHT PLAN KHKC 7 KCOS HCI TIFTO Enroute CEKIS VASCO CURRENT Vit PROFILE ACTIVE Vill WPT va TGT HOG 360 i 4 k ha W u k gt i M Y pria m cers Ps rade eta bd Mapas 30 4 Figure 7 21 V
10. Abnormal COM operation 12 2 Activate a flight plan 8 3 Active channel 11 16 Active flight plan 8 2 ADF 1 7 5 3 ADS B RR 1 10 7 10 9 13 6 AFCS 13 4 Age 10 6 AHRS 13 19 Aircraft alerts 13 3 AIRMET 10 5 Airport frequency 7 26 Airport information 7 22 Airspace alerts 7 29 Airspeed indicator 2 3 Airspeed Reference 6 8 Airspeed trend vector 2 3 Airways 8 5 Alerting system 13 1 Alerts 13 1 Alert levels 13 2 Alert Pop Up 10 20 ALT 1 4 1 8 2 4 6 4 6 6 6 13 7 19 10 8 Altitude alerting 2 4 Altitude constraints 1 10 7 12 Altitude hold 1 4 Altitude Hold Mode 6 6 Altitude mode 10 8 Altitude Reference 6 6 6 13 Altitude restrictions 1 11 Altitude trend vector 2 4 Altitude volume 10 8 ALT Knob 1 4 Ammeter 3 3 3 9 AP 1 4 Approach ILS 6 31 Missed 6 33 WAAS 6 32 Approaches 9 2 Approach activation 4 4 190 00384 09 Rev A Approach markers Signal augmentation 5 2 Approach Mode 6 20 Approach Mode AFCS 6 31 6 32 AP DISC Switch 6 1 6 34 Arrivals 9 1 Assist 3 4 3 6 3 7 Attitude indicator 2 3 Audio alerting system 13 1 Audio panel 4 3 5 1 Audio Panel controls SPKR 5 2 Audio panel controls ADF 5 3 DME 5 3 NAV1 5 3 NAV2 5 3 Aural alerts 13 6 Automatic audio muting 11 18 Auto tuning 4 4 Automatic Flight Control System AFCS Status Annunciations 6 34 Status Box 6 2 Automatic squelch 4 3 Autopilot 6 22 6 23 Autopilot disconnect 6 16 6 23 Backcourse Mode 6 21 Barometric mini
11. Aviation Data 3 Press the ENT Key PAGE MENU OPTIONS Inhibit Terrain View Arc Show Aviation Data Press the FMS CRSR knob to return to base page Figure 10 20 Terrain SVS Page Menu TERRAIN SVS Alerts Alerts are issued when flight conditions meet parameters that are set within TERRAIN SVS software algorithms TERRAIN SVS alerts typically employ a CAUTION or a WARNING alert severity level or both When an alert is issued visual annunciations are displayed and aural alerts are simultaneously issued Table 10 1 shows TERRAIN SVS alert types with corresponding annunciations and aural messages When an alert is issued annunciations appear on the PFD and MFD The TERRAIN SVS Alert Annunciation is shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD If the TERRAIN SVS Page is not displayed at the time a pop up alert appears on the MFD To acknowledge the pop up alert e Press the CLR Key returns to the currently viewed page or e Press the ENT Key accesses the TERRAIN SVS Page 10 12 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE PFD MFD Alert Type Alert Annunciation MFD Pop Up Alert Aural Message Reduced Required Terrain Clearance TERRAIN Warning Terrain Terrain Warning RTC Imminent Terrain Impact Warning ITI TERRAIN Warning Terrain Terrain Reduced Required Obstacle Clearanc
12. Continuous Aural Tone Aural tone is inhibited while the aircraft is on the ground KAP 140 installations only CAUTION Alerts 172R 172S 182T T182T 206H and T206H Annunciation Window Text Audio Alert Single Aural Tone CAUTION Alerts T182 T206 and 206 with Prop De Ice Only Annunciation Window Text Audio Alert Single Aural Tone 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III eee SECTION 13 ANNUNCIATIONS amp ALERTS 13 4 AFCS ALERTS System Status Annunciation wi TAB 11T ree TABLA 117 95 es i DiE mg 436 975 118 AAP co 95 FT J cont 196 975 118 088 cov System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD Figure 13 5 AFCS System Status Annunciation Aileron Mistrim Right i baie Roll servo providing sustained force in the indicated direction Aileron Mistrim Left Elevator Mistrim Down Pitch servo providing sustained force in the indicated direction Elevator Mistrim Up Pitch Trim Failure PTRM If AP engaged take control of the aircraft and disengage AP Roll Failure 30E Roll axis control failure AP inoperative Pitch Failure PTCH Pitch axis control failure AP inoperative System Failure l Oey AP and MET are unavailable FD may still be available Performing preflight system test aural alert sounds at completion Do not press the AP DISC Switch during servo power u
13. SECTION 7 NAVIGATION Enter a Direct to Destination 1 Press the Direct to Key E 2 Turn the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identitier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the VNAV altitude field 7 Turn the small FMS Knob to enter the desired VNAV altitude 8 Press the ENT Key The option to select MSL or AGL is now displayed 9 Turn the small FMS Knob to select MSL or AGL 10 Press the ENT Key The cursor is placed in the VNAV offset distance field 11 Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to 12 Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the COURSE field 13 Turn the small FMS Knob to enter the desired course to the waypoint 14 Press the ENT Key to highlight ACTIVATE 15 Press the ENT Key again to activate the Direct to Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Select a Direct to Destination to a Flight Plan Waypoint 1 While navigating an active flight plan press the Direct to Key 2 Turn the small FMS
14. Was 100Ff1 l 1000F1 u 3ONH VIEH VNV PROF CNCL VNV VNY amp Figure 7 47 Descending Turn to the Initial Approach Fix IAF 23 After crossing FALUR the next waypoint is the FAF The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator as shown in Figure 7 48 when the final SECTION 7 NAVIGATION approach course becomes active Note the BARO MIN Box is now displayed indicating the Decision Altitude entered when the approach was loaded FPL ACTIVE FLIGHT PLAN 136 975 118 009 conz Anka ACTIVE FLIGHT PLAN TR KMKC KCOS B268FT NO DATA na DTK E FSHER Mi Dn N PYNON ee AY fee ted Approoch KCOS RNAV 35Roes LPV HABUK lof ee AA pa FALUR oat pase L CEGIX fof 351 5 5N 7e00F1 RHSSR aap EE GIGBFT MOGAL mahp CURRENT UNV PROFILE ACTIVE VNV WPT VS TGT TERRAIN 100r7 1000F7 i 10 10 F 8608 346 WL S 33 y Sar aks MIN 29 921N A eavarr Figure 7 48 cia to the FAF The descent continues through the FAF CEGIX using the Glidepath Indicator as one would use a glideslope indicator to obtain an altitude AT 7 800 feet at the FAF Note the altitude restriction lines over and under At the altitude in t
15. X XM radio 11 16 XM radio volume 11 18 XM satellite radio 11 16 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton S040 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 190 00384 09 Rev A 2004 2008 Garmin Ltd or its subsidiaries
16. and press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 8 SECTION 8 FLIGHT PLANNING 8 8 8 18 DELETE A FLIGHT PLAN 1 From the Flight Plan Catalog Page press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the flight plan to be deleted 3 Press the DELETE Softkey 4 A Delete flight plan confirmation window is displayed With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key 8 19 GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key on the MFD to display the Active Flight Plan Page 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan 3 Press the LD WPT Softkey The selected waypoint is inserted at the end of the flight plan The default user waypoint naming is USROOO USROO1 USROO2 and so on 4 Ifthe selected waypoint is to be placed elsewhere in the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor 5 After placing the cursor at the desired point in the list of waypoints press the LD WPT Softkey 6 To change the user waypoint name follow the procedure for modifying a user waypoint Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 8 20 TRIP PLANNING
17. 12 SHCMVOLTS ON 12 35 7 VOLTS 6 6 Qe 38 7 vours Wl De 245 voits 245 M BATT S 13 0 6 AMPS OB Model 172R M BATT 65 13 6 6 AMPS 6 6 Model 172S M BATT 5 OR oo ars 00 Model 182T M BATT S 13 0 0 AMPS OA Model 206H Figure 3 1 Engine Display Normally aspirated Aircraft Exhaust Gas Temperature Indicator EGT Normally aspirated Aircraft Displays the exhaust gas temperature of the hottest cylinder number shown in triangular pointer in degrees Fahrenheit F Turbine Inlet Temperature Indicator TIT Turbocharged Aircraft Displays the temperature at the turbine inlet in degrees Fahrenheit F 3 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Vacuum Pressure Indicator VAC Models 172R and 172S Displays vacuum pressure Fuel Quantity Indicator FUEL QTY GAL Shows the quantity of fuel in the tanks in gallons ranging from zero to full F for each fuel tank left L and right R When full the indicator displays to 35 gallons per side 26 gallons for the Models 172R and 1725 190 00384 09 Rev A 11 Engine Hours Tach ENG HRS Models 172R and 172S A numeric readout gives the time in hours the engine has been in service 12 Voltmeter M E BUS VOLTS Displays the main and essential bus voltages 13 Ammeter M S BATT AMPS Shows the main and standby battery load in amperes Cruise Manifold CL Pressure HAN IN E
18. Any map display indication should be compared with approved navigation sources Select the MAP Page Group 1 Turn the large FMS Knob until MAP is highlighted in the page group box in the lower right of the MFD display 2 Turn the small FMS Knob to select the first MAP page indicated by a solid rectangular icon 136 975 118 009 corz NORTH UP Figure 7 1 Navigation Map Page Enroute 7 2 SECTION 7 NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD Identifier E Geographic B KMIA SE USA Region Facility Name MIAMI INTL City Sigetveg VNAV Target Altitude un m Offset Before Selected cd 3000 5m Direct to a i a ae om E Map Orientation WARN Fi Map of the ge Selected Waypoint Map Range LOCATION Bearing BRG 129 DIS Distance Direct to COURSE a 146 Activate Field Figure 7 2 MFD Direct to Window Enter a Direct to Destination 1 2 3 4 5 6 1 8 Press the Direct to G8 Key Enter the destination waypoint identifier Press the ENT Key to confirm the identifier The Activate field is highlighted If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 Turn the large FMS Knob to place the cursor over the VNAV altitude field Enter the desired altitude Press the ENT Key The option to select MSL or AGL is now displayed Turn the small FMS Knob to sel
19. Minimums View Figure 11 22 Selecting Day Night or Automatic View 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 13 SECTION 11 ADDITIONAL FEATURES 4 Turn the small FMS Knob to choose between Day Auto and Night Options 5 If Auto Mode is selected turn the large FMS Knob to select the percentage field Use the small FMS Knob to change the percentage value The percentage value is the day night crossover point based on the percentage of backlighting intensity For example if the value is set to 15 the day night display changes when the display backlight reaches 15 of full brightness The display must be changed in order for the new setting to become active This may be accomplished by selecting another page or changing the display range 6 Press the FMS Knob when finished to remove the Chart Setup Menu 11 4 FLITECHARTS The optional FliteCharts feature resembles the paper version of National Aeronautical Charting Office NACO terminal procedures charts The charts are displayed with high resolution and in color for applicable charts FliteCharts database subscription is available from Garmin FliteCharts functions are displayed on three levels of softkeys While on the Navigation Map Page Nearest Airports Page or Flight Plan Page pressing the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys CHRT OPT CHRT INFO
20. P approach CDI scaling figures z LL Ar j Enroute Missed o Departure Terminal Oceanic if gt 200 nm Terminal Approach d Ranreach from nearest airport pP pp O Drawing not to scale Figure 2 22 Phases of Flight CDI Scaling QO 5 CDI scale is set to the smaller of 0 3 nm S E or an angle set by the system D D oO Q Q o Z T o 5 E g q gt 3 0 2 g 5 z 5 Ss 2 angle based 5 L angle set Q 5 ondatabase A by system O I information z 4 4 H Ly e x Ul a FAF FAF Landing iE Threshold A O CDI scale varies if Vectors To Final is activated CDI scale varies if Vectors To Final is activated Drawing not to scale Drawing not to scale Figure 2 23 Typical LNAV and LNAV V Approach CDI Scaling Figure 2 24 Typical LNAV VNAV and LPV Approach CDI Scaling WAAS Systems Only 2 10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys The BRG1 pointer is a single line pointer The BRG2 pointer is a double line pointer Press the BRG1 or BRG2 Softkey to cycle through selecting NAV1 2 GPS or ADF for display using the corresponding pointer ae r Information Bearing 1 Bearing Window me Pointer CDI NAVI Bearing Bearing 2 Information Information Window Window Figure 2 25 HSI with Bearing Information Distance to Bear
21. group 2 Turn the small FMS Knob to select the sixth rectangular page icon Select and Load the Nearest ARTCC FSS or Weather Frequency 1 With the Nearest Frequencies Page displayed press the ARTCC FSS or WX Softkey to place the cursor in the appropriate field 2 Turn the FMS Knobs to select the desired facility or frequency 190 00384 09 Rev A SECTION 7 NAVIGATION 3 Press the ENT Key to load the frequency into the COM frequency standby field 4 Press the FMS Knob to remove the flashing cursor 7 15 NEAREST AIRSPACES 136 975 118 000 con AIRSPACE ALERTS Figure 7 67 Nearest Airspaces Page Select the Nearest Airspaces Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the seventh rectangular page icon Airspace Alerts Box e If the projected course takes the aircraft inside an airspace within the next ten minutes Ahead is displayed e If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside Ahead lt 2 nm is displayed e If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside Within 2 nm is displayed Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION 7 30 If the aircraft has entered an airspace Inside is displayed View Additional Details for a Li
22. ii ak ok a J L E oa k kar Toe A BUUUOU Figure 12 3 Loss of Hazard Functions with Loss of GPS Position 190 00384 09 Rev A 12 6 DEAD RECKONING WARNING DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to deter mine a position Changes in wind speed and or wind direction compound the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in Figure 12 4 In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of
23. maneuver The AP annunciation is temporarily replaced by CWS in white for the duration of CWS maneuvers In most scenarios releasing the CWS Button reengages the autopilot with a new reference Refer to the flight director modes section for CWS behavior in each mode Control Wheel Steering Po ROL CHS ALTS Figure 6 27 CWS Annunciation Disengaging the Autopilot Automatic disengagement occurs due to e System failure e Inability to compute default flight director modes FD also disengages automatically e Invalid sensor data Automatic autopilot disengagement is indicated by a flashing red AP annunciation and by the autopilot disconnect aural alert which continue until acknowledged by pushing the AP DISC or MET Switch Autopilot Automatically Disengaged a ALTS Figure 6 28 Automatic Autopilot Disengagement 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL The autopilot is manually disengaged by pushing the AP DISC Switch GA Switch MET ARM Switch or the AP Key on the MFD Manual disengagement is indicated by a five second flashing yellow AP annunciation and a three second autopilot disconnect aural alert After man ual disengagement the autopilot disconnect aural alert may be cancelled by pushing the MET ARM or AP DISC Switch AP DISC Switch also cancels the flashing AP an nunciation Autopilot Manually Disengaged o ROL SE TEE Figure 6 29 Manual Autopilot Disengag
24. the FliteCharts subscription but rather the availability of a particular airport chart selection or procedure for a selected airport If there is a problem in rendering the data such as a data error or a failure of an individual chart the banner UNABLE TO DISPLAY CHART is then displayed Chart Options Pressing the CHRT OPT Softkey displays the next level of softkeys the chart options level Figure 8 35 Pressing the ALL Softkey shows the entire chart on the screen Figure 11 24 Airport Information Page ALL View Selected Pressing the FIT WIDTH Softkey fits the width of the chart in the display viewing area Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right 190 00384 09 Rev A SECTION 11 ADDITIONAL FEATURES Day Night View FliteCharts can be displayed on a white or black background for day or night viewing The Day View offers a better presentation in a bright environment Selecting Day Night or Automatic View 1 While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS see Figure 11 22 2 Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to move to the COLOR SCHEME Option see Figure 11 22 4 Turn the small FMS Knob to choose between Day Auto and Night Options 5 If Auto Mode is selected turn the large FMS Knob to select the percentage field Use t
25. view channels that have been programmed Selecting a category 1 2 190 00384 09 Rev A Press the CATGRY Softkey on the XM Radio Page Press the CAT and CAT Softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Figure 11 26 Highlight the desired category with the small FMS Knob and press the ENT Key Selecting All Categories places all channels in the list Figure 11 26 Categories List SECTION 11 ADDITIONAL FEATURES Presets Up to 15 channels from any category can be assigned a preset number The preset channels are selected by pressing the PRESETS and MORE Soitkeys Then the preset channel can be selected directly and added to the channel list for the Presets category Setting a preset channel number 1 2 3 4 On the XM Radio Page while listening to an Active Channel that is wanted for a preset press the PRESETS Softkey to access the first five preset channels PS1 PS5 Figure 11 27 Press the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels Press any one of the PS1 PS15 softkeys to assign a number to the active channel Press the SET Softkey on the desired channel number to save the channel as a preset Pressing the BACK Soltkey or waiting during 45 seconds of softkey inact
26. 0 cccccs sess 2 3 Speed INGICATION ssc seseesseesstesssesseessecsessesseeseesessean 2 3 E NCS E E E ATA 2 3 Airspeed Trend VeCtor ssessessessecssessesssesssessesseeaseesees 2 3 Vspeed RETEreNCeS e a E 2 3 2 2 Attitude Indicator 0 0 0 ccs 2 3 23 AUM nanona 2 4 Selected Altitude Bug c scessessesecsessessesseeseesessean 2 4 Altitude Trend Vector c cssssssessesssssssssesssessessseaneesees 2 4 Barometric Setting BOX cscsssssessssessesesees 2 4 AUGE AENG setanin 2 4 Metric DIS GY cerecrisekonheiod niaan dened tivitenncnsnebaddioe 2 5 Low Altitude ANNUNClatiON cscessceseesseseessesteeseeseen 2 5 2 4 Vertical Deviation Glidepath Glideslope Indicato See ee eee nee ee eee ae 2 6 2 5 Marker Beacon Annunciation 0 2 7 2 6 Vertical Speed Indicator 0 cccceees 2 7 2 7 Barometric Altitude Minimume 2 7 2 8 Horizontal Situation Indicator HSI 2 8 CONSE POI O aosa oaoaraa a aE EERS 29 Course Deviation Indicator CDI ccceeeceseeeeeeeees 2 9 Bearing Pointers and Information WindowS 2 11 DIM Ne 610 ON Saree Reece etn eset ree tereeentn rte 2 11 Navigation SOUCO saviessceunotamuntecnteannatacmtanatieshatenin 2 11 2 9 Wind Dat cscs cesses tesserae 2 12 2 10 Generic Timer 00 ccc cesses teases teaees 2 13 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 3 1 Engine Display 0 0 c cccccccscesteeseesteeeesean 3 1 3 2 L
27. 190 00384 09 Rev A FLIGHT PLAN With either the Active or Stored Flight Plan displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to select the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window Figure 8 20 Remove Waypoint Confirmation With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor 8 16 SECTION 8 FLIGHT PLANNING INVERT AND ACTIVATE A STORED FLIGHT PLAN From the Flight Plan Catalog Page press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Press the INVERT Softkey Invert and activate stored flight plan is displayed With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location 8 17 COPY A FLIGHT PLAN From the Flight Plan Catalog press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be copied Press the COPY Softkey A Copy to flight plan confirmation window is displayed With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL
28. Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact Warning 101 PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up OF or Obstacle Obstacle Pull Up Pull Up Reduced Required Terrain Clearance Caution Caution Terrain Caution Terrain RTC or Terrain Ahead Terrain Ahead Imminent Terrain Impact Caution ITI Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Aural Message Reduced Required Obstacle Clearance Caution Obstacle Caution Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead Imminent Obstacle Impact Caution IOI Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Premature Descent Alert Caution PDA Altitude Callout 500 Nme Five Hundred Excessive Descent Rate Caution EDR Sink Rate Negative Climb Rate Caution NCR Don t Sink or Too Low Terrain 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 21 SECTION 10 HAZARD AVOIDANCE The following system status annunciations may also be issued PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert TAWS System Test Fail TAWS FAIL TAWS System Failure No GPS position or excessively degraded TAWS N A None TAWS Not Available GPS signal TAWS Available will be heard when sufficient GPS signal is re established System Testpass Test pass Nme TAWS
29. B Added CO Guardian Added new Fuel Totalizer Updated G1000 System Messages 190 00384 06 Rev A Added GDU 7 00 WAAS VNAV amp Charts software parameters Added AFCS for the 182 and 206 Added database loading instructions Updated G1000 System Messages Combined previous system software numbers into 0563 00 190 00384 07 Rev A Added GDU 8 02 parameters Airways and ADS B 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III RR 1 RECORD OF REVISIONS Part Number Change Summary 190 00384 08 Rev A Added GDU 8 20 parameters including gradient background on the PFD and GFC 700 tor the C172 190 00384 09 Added GDU 9 03 parameters Removed gradient background Added Additional Features section Changed tab structure Revision Dat of Revision Affected Pages RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 1 SYSTEM OVERVIEW 0000000000 1 1 1 1 PFD MFD Controls 0 0 0 0 ccccccccceeesteeseesteen 1 2 1 2 PFD Softke ys cesses 1 5 1 3 MFD Softkeys ssc coesencrcensemaniecparnnienes 1 8 1 4 MFD Page Groups 1 9 1 5 Vertical Navigation ceca 1 10 1 6 Backlighting 0 0 0 0 cc ccc cesses tesserae 1 12 1 7 Database Updates sees 1 12 Jeppesen Aviation Database cccessessesesecseeren 1 12 ar ata dg eG a eeaeesn mene 1 13 SECTION 2 FLIGHT INSTRUMENTS 00000 2 1 2 1 Airspeed Indicatol
30. BAXK Osoki Figure 4 11 Ground Mode Standby Mode Manual Press the STBY Softkey In Standby Mode the tran sponder does not reply to interrogations but new codes can be entered STBY Mode White Code Number and ae XPDR 6943 STBY eT ick Wen Figure 4 12 Standby Mode Manual ON Mode Press the ON Softkey ON Mode generates Mode A and Mode S replies but Mode C altitude reporting is in hibited ON Mode No Altitude Reporting MOO e ALERTS Figure 4 13 ON Mode 190 00384 09 Rev A Altitude Mode Automatic or Manual Altitude Mode is automatically selected when the aircraft becomes airborne Altitude Mode may also be selected manually by pressing the ALT Softkey All transponder replies requesting altitude information are provided with pressure altitude information ALT Mode Mode C Altitude Reporting xPoR 6543 ALT cL E ALERTS Figure 4 14 Altitude Mode Reply Status When the transponder sends replies to interrogations an R indication appears momentarily in the reply status field Reply Indication Figure 4 15 Reply Indication Code Selection VFR Code Selection 1 Press the XPDR Softkey to display the transponder Mode Selection softkeys 2 Press the VFR Softkey to enter the VFR code Pressing the VFR Softkey again restores the previous identification code NOTE The pre programmed VFR Code is set at the factory to 1200 190 00384 09 Rev A 1
31. COM Volume Level 4 3 AUTOMATIC SQUELCH Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COMS standby frequency then by pressing the VOL PUSH SQ Knob When Automatic Squelch is disabled a white SQ appears next to the COM frequency 190 00384 09 Rev A SECTION 4 NAV COM amp TRANSPONDER Squelch Indication 121 988 so 118 680 coms sa 118 400 comz Figure 4 7 Squelch Indication 4 4 QUICKLY ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Transfer Key for approximately two 2 seconds automatically tunes the selected COM radio to the emergency frequency 4 5 OPTIONAL NAV RADIOS DME Radio optional The DME Tuning Window is displayed by pressing the DME Softkey DME TUNING Di NAY 1 Figure 4 8 Radio Tuning Window Changing the DME tuning source 1 From the tuning window turn the large FMS Knob to highlight the DME source field 2 Turn the small FMS Knob to display the selection window Turn the FMS Knob to select the desired mode and press the ENT Key Figure 4 9 DME Selection Window Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 4 3 SECTION 4 NAV COM amp TRANSPONDER ADF Radio optional The G1000 does not support tuning of the ADF in Nav III aircraft ADF tuning is accomplished through the Bendix King KR 87 ADF Radio ADF volume must also be adjusted through the KR 87 4 6
32. DP STAR APR WX and GO BACK The chart selection softkeys appear on the Airport Information Page Pressing the GO BACK Softkey reverts to the top level softkeys and previous page Pressing the CHRT OPT Softkey displays the available terminal chart and advances to the next level of softkeys ALL FIT WDTH FULL SCN and BACK While viewing the CHRT OPT Soitkeys after 45 seconds of softkey inactivity the system reverts to the chart selection softkeys If a chart is available for the destination airport or the airport selected in the active flight plan the chart appears on the screen When no flight plan is active or when not flying to a direct to destination pressing the SHW CHRT Softkey displays the chart for the nearest airport if available SHW CHRT Jfcurrorr _ cnet Jf mro JE oe f srar Il ar E w JL eoe nnnnenunieanieeuannk D Presssing the GO BACK Softkey returns to the top level softkeys and previous page Co Waf EO OO MEO Mfewmfusoi fead nnnWnienenoinannrnieunrnnrniuanndk sw Pressing the BACK Softkey returns to the Chart Selection Softkeys Figure 11 23 FliteCharts Softkeys Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A NOTAMs are not available with FliteCharts The NOTAM Softkey label appears subdued and is disabled When no terminal procedure chart is available the banner CHART NOT AVAILABLE appears on the screen The CHART NOT AVAILABLE banner does not refer to
33. FREQUENCY AUTO TUNING Auto tuning on the PFD NEAREST AIRPORTS 51K 124 6 8NM UNICOM 122 708 RNWY KLWC 278 18 2NM UNICOM 123 000 RNWY 11 4NM 133 000 RNWY IDENT TMRVREF WAST CAUTION Figure 4 10 Nearest Airports Window PFD 1 Press the NRST Softkey to display the Nearest Airports Window 2 Turn either FMS Knob to highlight the desired frequency 3 Press the ENT Key to place the frequency in the standby field of the active COM 4 Press the Frequency Transfer Key to place the frequency in the active field NAV frequencies are entered automatically in the NAV frequency active or standby field depending in CDI selection upon approach loading or approach activation Auto tuning on the MFD Auto tuning on the MFD is done in much the same way as on the PFD Use the FMS Knobs to select the desired frequency on any of the information pages Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 4 7 TRANSPONDER Mode Selection The STBY ON ALT GND VFR CODE and IDENT Softkeys can be accessed by pressing the XPDR Softkey Ground Mode Automatic or Manual GND is displayed when the aircraft is on the ground or when the GND Softkey is pressed The transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely address Mode S interrogations pT
34. FT TA A MAPR o i I Vor Figure 7 50 Missed Approach Active 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION 26 The aircraft continues climbing to AT or ABOVE 10 000 feet at MOGAL A holding pattern is established at the MAHP MOGAL as shown in Figure 7 51 PL ACTIVE FLIGHT PLAN 136 975 118 809 conz DTK DIS Approach KCOS RNAV 35Rees LPV BUK iof CURRENT VNV PROFILE ACTIVE UNU WPT VS TGT PH FPA 5 REG PH 0 TO TERRAIN VS REO TIME T 00 V DEV 100Ff1 l y co 71000r1 m i TIN a SNAMI CNCL VNV Figure 7 51 Establishing the Holding Pattern 27 The aircraft maintains 10 000 feet while following the magenta line through the hold as in Figure 7 52 136 975 118 688 conz NORTH UP OREH Ue ACTIVE FLIGHT PLAN DTK DIS Approach KCOS RNAV 35Rees LPV JK iof CURRENT VNV PROFILE ACTIVE UNV WPT VS TGT PH FPA S REO PH E TO TO TERRAIN VS REO TIME TO TOD V DEV 109Ff1 1000F7 M Spi CNCL VNV Figure 7 52 Hold Established l 21 SECTION 7 NAVIGATION 7 4 AIRPORT INFORMATION 118 000 con Sor te Soest ioe Serr OIT p Figure 7 53 Airport Information Page e k Select the Airport Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the first rectangular page icon Initially information
35. G1000 system MANIFEST GIA2 software should be serviced mismatch communication halted MANIFEST GFC software mismatch 3 l a Incorrect servo software is installed or gain settings are incorrect communication halted COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP COM The transmitter is operating at reduced power If the problem persists the G1000 ere al system should be serviced Reducing transmitter power Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A A GIA mismatch has been detected where only one is WAAS capable The system has detected an over temperature condition in COM1 and or COM2 SECTION 13 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories Cont COM1 SERVICE COM1 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 COM2 SERVICE COM needs may still be usable The G1000 system should be serviced when possible service Return unit for repair COM1 PTT COM1 push to talk ke enk P y The COM1 and or COM2 external push to talk switch is stuck in the enable or O kk pressed position Press the PTT switch again to cycle its operation nee 7 PUENAOAAKKEY 1 Tithe problem persists the G1000 system should be serviced COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck LOI GPS integrity lost Cros
36. Guide for the Cessna Nav III 6 19 SECTION 6 AUTOMATIC FLIGHT CONTROL When the CDI has automatically switched from GPS to LOC during a LOC ILS approach GPS Navigation Mode remains active providing GPS steering guidance until the localizer signal is captured LOC Navigation Mode is armed in anticipation of localizer signal capture if the APR Key is not pressed prior to the automatic source switch If Navigation Mode is active and either of the following occur the flight director reverts to Roll Hold Mode wings rolled level e Different VOR is tuned while in VOR Navigation Mode VOR Navigation Mode reverts to armed e Navigation source is manually switched e Localizer signal is not captured by the final approach fix FAF Changing the Selected Course The Selected Course on the PFD is controlled using the CRS Knob Pressing the CWS Button and hand tlying the aircraft does not change the Selected Course while in Navigation Mode The autopilot guides the aircraft back to the Selected Course or GPS flight plan when the CWS Button is released Approach Mode GPS VAPP LOC NOTE The selected navigation receiver must have a Valid VOR or LOC signal or active GPS course for the flight director to enter Approach Mode Approach Mode is activated when the APR Key is pressed Approach Mode acquires and tracks the selected navigation receiver on the HSI GPS VOR or LOC depending on the loaded approach This mode u
37. Guide for the Cessna Nav III 190 00384 09 Rev A AFCS Status Box Flight director roll modes are shown on the left and pitch on the right Armed modes are annunciated in white and active in green Autopilot status is displayed in the center of the AFCS Status Box 6 3 FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes Unless otherwise specified all mode keys are alternate action i e press on press off In the absence of specific mode selection the flight director reverts to the default pitch and or roll mode s Armed modes are annunciated in white and active in green in the AFCS Status Box Under normal operation when the control for the active flight director mode is pressed the flight director reverts to the default mode s for the axis es Automatic transition from armed to active mode is indicated by the white armed mode annunciation moving to the green active mode field and flashing for ten seconds A flashing yellow mode annunciation and annunciator light indicate loss of sensor AHRS ADC IAU or navigation data VOR LOC GPS VNAV WAAS required to compute commands When such a loss occurs the system automatically begins to roll the wings level or maintain the pitch angle depending on the affected axis The flashing annunciation stops when the affected mode key is pressed or another mode for the axis is selected If after ten seconds no action is taken t
38. HSI whichever is less The height is 200 feet or one half full scale deviation on the VDI whichever is less The altitude at which the pathway boxes are displayed is 190 00384 09 Rev A determined by the higher of either the selected altitude or the VNAV altitude programmed for the active leg in the flight plan Figure 11 3 The color of the rectangular boxes may be magenta green or white depending on the route of flight and navigation source selected The active GPS or GPS overlay flight plan leg is represented by magenta boxes that correspond to the Magenta CDI A localizer course is represented by green boxes that correspond to a green CDI An inactive leg of an active flight plan is represented by white boxes corresponding to a white line drawn on the Inset map or MFD map indicating an inactive leg ACTIVE FLIGHT PLAN KMKC KEOS DIS ALT FSHER Joe JANH 10000QFT PYNOM 959 11 9WH 100ABFT Approach KCOS RNAY 35Reps LPY HABUK inf Bi Programmed Altitudes ANH 6370r 10000F 1 CURRENT Vili PROFILE ACTIVE VNV WPT TBRGRFT ot VS TGT S6FPH FPA rs vS REG ____FPH TIME TO TOD 20 Y DEV gt FU Selected __ Altitude 5 12000 OPSHN 3N Figure 11 3 Programmed and Selected Altitude 190 00384 09 Rev A SECTION 11 ADDITIONAL FEATURES Pathways provide supplemental glidepath information on an active ILS LPV LNAV VNAV and some LNAV approaches Pathways are intended as an aid to sit
39. III 1 13 SECTION 1 SYSTEM OVERVIEW Blank Page 1 14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display unless otherwise indicated navi 1 8 08 117 95 119 700 124 158 con nav2 108 00 117 95 136 975 118 000 corz i 1 4 JAB cul a TT a pA Fone E 70 7 wred Fe i 1 fa m an TAS 90kT ELOS E EEN F 29 9211 r i i i Fr E PoR niLa 06 06 25 APDR Sa ela ALERTS INSET PFD O8S A NAV Frequency Box Turn Rate Indicator Airspeed Indicator Barometric Setting Box True Airspeed Box Vertical Speed Indicator Heading Box Altimeter Current Track Indicator Selected Altitude Box Horizontal Situation Indicator COM Frequency Box Outside Air Temperature Box Navigation Status Box Slip Skid Indicator Attitude Indicator System Time Box O OOOQOOO 000000000 Ie Transponder Status Box Figure 2 1 Default PFD Information 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Ji SECTION 2 FLIGHT INSTRUMENTS navi 110 90 nave 108 30 110 50 100r i AUENWARNH E peat AMIA EEE D ai Lin F ere URE Pi Mei DOTTE INSET A Traffic Annunciation 2 Vspeed References G Selected Heading Box Wind Data Window G Inset Map 6 BRGI Infor
40. Knob to the left to display a list ACTIVATE Figure 7 8 Flight Plan Waypoint List PFD 3 Turn the large FMS Knob to select the desired waypoint 4 Press the ENT Key The cursor is now displayed on ACTIVATE 5 Press the ENT Key again to activate a Direct to Select a Direct to Destination to a Nearest Airport 1 Press the Direct to E Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 8 The list is only populated when navigating a flight plan OFFSET 5NM Ds 1074m ACTIVATE Figure 7 9 Nearest Airport List PFD 3 Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position as shown in Figure 7 9 190 00384 09 Rev A 4 Turn the large FMS Knob to select the desired airport 5 Press the ENT Key The cursor is now displayed on ACTIVATE 6 Press the ENT Key again to activate a Direct to Select a Direct to Destination to a Recently Entered Identifier 1 Press the Direct to GE Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 8 The list is only populated when navigating a flight plan OFFSET SNH DIS 10741A ACTIVATE Figure 7 10 Recently Entered Waypoints List PFD 3 Turn the small FMS Knob to the right to display the RECENT waypoints as shown in Figure 7 10 4 Turn the large FMS Knob to sele
41. Softkey provides specific public awareness and protection weather warnings for Tornado Severe Thunderstorm and Flood conditions provided by the National Weather Service NWS The display is updated every 5 minutes SECTION 10 HAZARD AVOIDANCE CYCLONE Pressing the CYCLONE Softkey shows the current location of cyclones hurricanes and tropical storms and their projected track at various time intervals The update rate is every 12 minutes Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products amp Symbols Figure 10 10 depicts the symbol for each weather product read from left to right When a weather product is active the product symbol is displayed in the lower right of the screen e NEXRAD e Cloud Top Echo Top e XM Lightning e Cell Movement SIGMETS AIRMETS e METARs
42. TAWS View Arc w Aviation Data Press the FMS CRSR knob to return to base page Figure 10 26 TAWS Page Menu TAWS Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert When TAWS is inhibited only FLTA and PDA alerts are disabled Inhibit TAWS While the TAWS Page is displayed press the INHIBIT Softkey TAWS INHB is annunciated in the lower right of portion of the screen Enable TAWS If TAWS has been inhibited trom the TAWS Page press the INHIBIT Softkey The TAWS INHB annunciation is removed NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 10 HAZARD AVOIDANCE Manual System Test calculated to come within minimum clearance altitudes in the following table Phase of Flight Level Flight Descending A system test is automatically performed at power up After successful completion of the test TAWS System Test OK is heard 700 ft 500 ft The system test may also be initiated manually but 350 ft 300 ft only when the aircraft is on the ground To manually verify Approach 150 ft 100 ft proper operation of the aural and
43. a Flight Plan 8 5 8 9 Load a Departure cscs 8 6 i Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 8 10 Load an Alrival 0 0 cccccccccs cesses 8 6 8 11 Load an Approach essen 8 6 8 12 Remove a Departure Arrival Approach or Airway from a Flight Plan 0 0 cc ce 8 6 8 13 Store a Flight Plamen 8 6 8 14 Edit a Stored Flight Plan 0 0 0 8 7 8 15 Delete a Waypoint from the Flight Plan 8 7 8 16 Invert and Activate a Stored Flight Plan 8 7 8 17 Copy a Flight Plann 8 7 8 18 Delete a Flight Plait cesses 8 8 8 19 Graphical Flight Plan Creation 8 8 8 20 Trip Planning 0 cccccccc cess testeeseesteeseesean 8 8 SECTION 9 PROCEDURES 0 0 9 1 9 1 Arrivals and Departures 0510551111111111112 9 1 Load and Activate a Departure Procedure uu 9 1 Load and Activate An Arrival Procedure 9 1 9 2 Approaches eee 9 2 Load and or Activate an Approach Procedure 9 3 Activate An Approach in the Active Flight Plan 9 4 SECTION 10 HAZARD AVOIDANCE 0000 10 1 10 1 Customizing the Hazard Displays on the Navigation Map 0 0 ccccccsceesteeeesen 10 1 10 2 STORMSCOPE Optional 0 0 0 0 10 1 Displaying Stormscope Lightning Data on the Navigation Map PAGE siscusascssoressasvosonsaadrcistaveresstavouns 10 1 SLONMS COBO PACS ree r a 10 2 10 3
44. adds the procedure to the flight plan without immediately using it for navigation guidance Activate An Approach in the Active Flight Plan 1 2 3 With the Navigation Map Page displayed press the PROC Key Turn the large FMS Knob to highlight ACTIVATE APPROACH Press the ENT Key The approach procedure is now active and a direct to is initiated to the IAF Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE 10 1 CUSTOMIZING THE HAZARD 1 2 3 190 00384 09 Rev A DISPLAYS ON THE NAVIGATION MAP With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select the Weather group Figure 10 2 to customize the display of weather features Select Traffic to customize the display of traffic Press the small FMS Knob to return to the Navigation Map Page PAGE MENU OPTIONS Declutter Measure Bearing Distance Show Chart Figure 10 1 1 Page Menu HAP SETUP k GROUP STRMSCP LTNG STRMSCP MODE Cell STRMSCP SMEL BOONH NEXRAD DATA OFF 2GQQNM NEXRD CELL HOW 4 Cn XM LING Off e 2AOANM Figure 10 2 Map Setup Menu HAP SETUP On Ti raffic Cle Aviatio Land L 150NH parrau con SONH AIl Troffic Figure 10 3 Map Setup Group List T
45. an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircratt NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A RECORD OF REVISIONS Part Number Change Summary 190 00384 03 Rev A Added XM Radio and XM Weather Added ADF capability Added DME capability Added BRG1 BRG2 pointers Added dual audio panel operation Added C172 parameters Changed Airspeed Trend Vector Changed Altitude Trend Vector Added Checklist capability Added Flight ID capability Rev B Updated system software numbers 190 00384 04 Rev A Reformatted manual to new format Added TAS capability Rev B Added DONE Softkey XM INFORMATION Page and XM RADIO Page operation 190 00384 05 Rev A Added explanation of EIS display behavior upon exceedances Added better explanation of Intercom System Isolation Added Stormscope operation upon loss of heading input Added TAWS
46. and charts Obstacle symbols appear in the perspective view with relative height above terrain and distance from the aircraft Unlike the Inset map and MFD moving map display obstacles on the synthetic terrain display do not change colors to warn of potential conflict with the aircrafts flight path until the obstacle is associated with an actual FLTA alert Obstacles greater than 1000 feet below the aircraft altitude are not shown Obstacles are shown behind the airspeed and altitude displays TERRAIN Annunciation wan TBE 117 95 i 15 ARC 136 975 118 088 com neve VEE 45 136 975 118 008 coc man E pary Ei Obstacle POR TOENT TAVAF LNS Potential Impact Caution Point Figure 11 10 Obstacle 190 00384 09 Rev A Field of View Two dashed lines forming a V shape in front of the aircraft symbol on the MFD map represent the forward viewing area shown on the PFD 117 95 l 4 NS 135 975 118 000 con 11 1 95 l _ 138 975 as 1 13 006 cont 136 975 118 009 coe 136 975 118 009 conz TRACK UP TERRAIN 100 1000 Field of View on the MFD Figure 11 11 PFD and MFD Field of View Comparison Configuring field of view 1 While viewing the Navigation Map Page press the MENU Key to display the PAGE MENU 2 3 4 5 6 SECTION 11 ADDITIONAL FEATURES Turn the large FMS Knob to highlight Map Setup and press the ENT Key Turn the FMS Knob to select the Map Group a
47. annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft 4 The autopilot flies the holding pattern after the missed approach is activated Annunciations are displayed in the Navigation Status Box above the AFCS Status Box DIS BRG POIN AVN Sd9 apo VO Y a Figure 6 39 Go Around Missed Approach Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC 6 34 FLIGHT CONTROL 6 6 AFCS ANNUNCIATIONS AND ALERTS AFCS Status Alerts The following annunciations listed in order of increasing priority can appear on the PFD above the Airspeed and Attitude indicators Only one annunciation may occur at a time and messages are prioritized by criticality nav1 148 08 lt 117 95 nav2 108 00 117 95 AFCS Status Annunciation Elevator Mistrim me or stuck MET Switch If AP na move MET switches separately to unstick Ste E Roll axis control Roll axis control failure AP inoperative AP inoperative Pitch Failure PTCH Pitch axis control failure AP inoperative System Failure aim AP and MET are unavailable FD may still be available Performing preflight system test aural alert sounds at completion Do not press the AP DISC Switch during servo power up and preflight system tests as this may cause the pretlight system test to fail or never Preflight Test to sta
48. associated with lateral waypoints to give guidance for vertical navigation These altitudes are depending on the specific instance entered by the pilot or retrieved from the published altitudes in the navigation database The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at then the altitude is not in the database In this case the altitude may be entered manually NOTE All arrival procedure altitudes contained in the navigation database are for turbojet aircraft only Alter or enter altitudes as desired to comply with the ATC clearance When activating or loading an arrival or approach procedure into an active flight plan the VNV ALT fields are populated with any altitudes that can be retrieved from the navigation database Since altitudes loaded with an arrival procedure are published only for turbojet aircraft the altitudes are displayed as white text indicating that the altitudes are displayed for reference only An arrival waypoint altitude may be used or designated as is or changed to a different altitude An altitude is designated by pressing the FMS Knob and turning the large FMS Knob to place the cursor on the desired altitude and pressing the ENT Key or entering a different value and pressing the ENT Key The altitude is now displayed as light blue text indicating that the altitude is now designated to give vertic
49. cause isolated discharge points in the strike display mode However clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The GDU 1040 and GDU 1044B PFD MFD may require a warm up time of up to 30 minutes when exposed to 40 C for an extended period A warm up time of up to 15 minutes may be required when exposed to 30 C for an extended period NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause
50. causing the vertical deviation to go angle error invalid Se The current crosstrack exceeds the limit causing vertical deviation to go invalid crosstrack error ee PAN Aeee A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 The selected waypoint xxxx does not use the WGS 84 datum Cross check waypoint for navigation xxxx position with alternate navigation sources TRAFFIC FAIL Traffic device has The G1000 is no longer receiving data from the traffic system The traffic device failed should be serviced hae pelle Dales A data path connected to the GDU or the GIA 63 W has failed MAG VAR WARN Large magnetic The GDU s internal model cannot determine the exact magnetic variance for variance Verity all course angles geographic locations near the magnetic poles Displayed magnetic course angles may differ trom the actual magnetic heading by more than 2 SVS SVS DISABLED Out of Synthetic Vision is disabled because the aircraft is not within the boundaries of the available terrain region installed terrain database SVS SVS DISABLED Terrain DB Synthetic Vision is disabled because a terrain database of sufficient resolution 9 resolution too low arc second or better is not currently installed SCHEDULER lt message gt Message criteria entered by the user 13 22 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A A
51. data is restored The SVS terrain display shows land contours colors are consistent with those of the topographical map display large water features towers and other obstacles over 200 AGL that are included in the obstacle database Cultural features on the ground such as roads highways railroad tracks cities and state boundaries are not displayed even if those features are found on the MFD map The terrain display also includes a north south east west grid with lines oriented with true north and spaced at one arc minute intervals to assist in orientation relative to the terrain The optional Terrain Awareness and Warning System 190 00384 09 Rev A SECTION 11 ADDITIONAL FEATURES TAWS or standard Terrain SVS is integrated within SVS to provide visual and auditory alerts to indicate the presence of terrain and obstacle threats relevant to the projected flight path Terrain alerts are displayed in red and yellow shading on the PFD The terrain display is intended for situational awareness only It may not provide the accuracy or fidelity on which to base decisions and plan maneuvers to avoid terrain or obstacles Navigation must not be predicated solely upon the use of the Terrain SVS or TAWS terrain or obstacle data displayed by the SVS neve 188 88 117 95 136 975 118 808 com ors 1 wu 188 08 117 95 136 875 118 000 conz Figure 11 1 Synthetic Vision Imagery SVS Operation SVS is activated from the PFD usin
52. displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration deceleration is maintained 190 00384 09 Rev A SECTION 2 FLIGHT INSTRUMENTS Vspeed References Vspeed References are turned on or off in the Timer Reterences Window Press the TMR REF Softkey to display the widow When active ON the Vspeeds are displayed at their respective locations to the right of the airspeed scale To activate the Vspeed References display the Timer Reference Window and turn the large FMS Knob to place the cursor in the ON OFF field Turn the small FMS Knob to select ON or OFF 2 2 ATTITUDE INDICATOR O Roll Pointer Roll Scale G Horizon Line 4 Aircraft Symbol G Land Representation Roll Index Zero 6 Aircraft Wing Tips E Pitch Scale Slip Skid Indicator E Sky Representation Figure 2 6 Attitude Indicator The Slip Skid Indicator is located under the roll pointer and moves laterally away from the pointer to indicate lateral acceleration One Slip Skid indicator displacement is equal to one ball displacement when compared to a traditional slip skid indicator Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 3 SECTION 2 FLIGHT INSTRUMENTS 2 4 2 3 ALTIMETER Altitude Altitude Reference Reference Box Bug Altitude Trend Current Vector Altitude Barometric Altitude Minimums Bug Barometric Setting Box Figure 2 7 Altimeter Selected Alt
53. for details Glidepath Mode GP A NOTE Pressing the CWS Button while Glidepath Mode is active does not cancel the mode The autopilot guides the aircraft back to the glidepath NOTE Glidepath Mode is available only in installations with GIA 63W Integrated Avionics Units and WAAS currently available Glidepath mode is used to track the WAAS based glidepath Arming Glidepath Mode annunciated in white as GP requires e Approach supporting WAAS vertical guidance is loaded into the flight plan e Expected availability of vertical guidance e GPS Approach Mode is armed after acquiring clearance for approach prior to intercepting the WAAS glidepath GPS is the selected navigation source and the APR Key is pressed see GPS upon release of the CWS Button Approach Mode GPS Approach Glidepath Mode Active Mode Active e 7770 es l Vile CN NAN SN A9 GPS is Selected LNAV Navigation a Source ctive Command Bars Indicate Descent on Glidepath 29 921N Glidepath Indicator Figure 6 15 Glidepath Mode Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A _ GPS AP ALTS GP Figure 6 16 Glidepath Mode Armed If vertical guidance becomes or is expected to become SECTION 6 AUTOMATIC FLIGHT CONTROL Glideslope Mode is available for LOC ILS approaches to capture and track the glideslope Glideslope Mode is armed when e A valid localizer frequency is tuned
54. for the airport closest to the aircraft s present position is displayed Select an Airport from the Database 1 2 7 22 With the Airport Intormation Page displayed press the FMS Knob to activate the cursor Enter the desired airport identifier Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Select an Airport from the Active Flight Plan 1 2 3 4 With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the small FMS Knob to the left to display a list of flight plan airports as shown in Figure 7 54 Figure 7 54 Flight Plan Airport List Turn the large FMS Knob to select the desired airport Press the ENT Key Select a Nearest Airport 1 2 3 With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the small FMS Knob to the left Initially a flight plan airport list is displayed as in Figure 7 54 The list is populated only when navigating a flight plan Figure 7 55 Nearest Airport List Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position as shown in Figure 7 55 190 00384 09 Rev A 190 00384 09 Rev A 4 Turn the large FMS Knob to select the desired airport 5 Press the ENT Key Select a Recently Entered Airport Identifier 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Turn the s
55. in the bottom card slot of the PFD 190 00384 09 Rev A 3 4 5 SECTION 1 SYSTEM OVERVIEW The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD Apply power to the G1000 System View the MFD power up splash screen Check that the databases are initialized and displayed on the scrolling window of the splash screen When updating the terrain and FliteCharts databases an in progress message may be seen If this message is present wait for the system to finish loading before veritying the correct databases are initialized then proceed to step 3 DATABASE 7A Checklist File N A Ey Basemap Land 1 01 SafeTaxi Expires 28 SEP 2006 as Terrain 2 04 a Airport Terrain 2 04 x Obstacle Expires 28 SEP 2006 A Aviation Expires 23 NOV 2006 FliteCharts Expires 11 MAY 2006 All map and terrain data provided is only to be used as a general reference to your surrounding und as an aid to situational awareness Press ENT or rightmost softkey to continue Figure 1 13 Power Up Splash Screen Window Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey At the MAP NAVIGATION MAP Page press the MAP Softkey and check to make sure that the TOPO and TERRAIN Softkeys are available not dimmed and other database features are functioning Power down the G1000 Garmin G1000 Cockpit Reference Guide for the Cessna Nav
56. inches of mercury HPA Press to display the BARO setting as hectopacals ARC HSI Press to display the HSI in an arc STD BARO Press to set the barometric pressure format to standard pressure BACK Press to return to the previous level softkeys ALERTS Press to display the Alerts Window OBS Press to select OBS Mode on the CDI when navigating by GPS only available with active leg BRG2 bearing Press to cycle through the following Nav sources making the pointer the indicator for the corresponding source and displaying the appropriate information optional _ Linser T__ _ero_ Loss _cor_J _owe_J _xeor ident irmmvrer _ nest acerrs 190 00384 09 Rev A ME sry f on ar f eno ver Jf cov went J Back J aterrs nnnWnnnnnrnnurninooearnAain w Press the BACK Softkey to return to the top level softkeys a Woe js I bs JE e JE 7 Ji menr JL exse j Back J acerrs nnnnnianarnienrnieannt sw Press the BACK Softkey to return to the previous softkey level Figure 1 5 XPDR Transponder Softkeys Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 1 SYSTEM OVERVIEW CDI Press to change navigation mode on the CDI between GPS VORI and VOR2 DME optional Press to display the DME Tuning Window XPDR Press to display the transponder mode selection softkeys STBY Press to select Standby Mode ON Press to select Mode A ALT Pre
57. navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode Pressing the NAV Key selects Navigation Mode Navigation Mode acquires and tracks the selected navigation source on the HSI GPS VOR LOC The flight director follows GPS roll steering commands when GPS is the selected navigation source SECTION 6 AUTOMATIC FLIGHT CONTROL When the HSI is coupled to VOR or LOC the flight director creates roll steering commands from the Selected Course and deviation Navigation Mode can also be used to fly non precision GPS and LOC approaches where glideslope capture is not required If the Course Deviation Indicator CDI shows greater than one dot when the NAV Key is pressed the selected mode is armed The armed annunciation appears in white to the left of the active roll mode For cases where the projected course is offset a large distance trom the present course for turn anticipation GPS Navigation Mode can be activated with crosstrack error up to 10 nm when the NAV Key is pressed GPS ROL PIT ALTO Figure 6 23 GPS Navigation Mode Armed Selected Altitude GPS Navigation Pitch Mode Capture Mode Mode Active Active Armed o GPS is Selected Selected Navigation Course Source Command Bars Indicate Left Turn to Track GPS Course and Climb to Intercept Selected Altitude Figure 6 22 Navigation Mode 190 00384 09 Rev A Garmin G1000 Cockpit Reference
58. of Descent 7 15 7 16 Tornado 10 5 Traffic advisory 10 7 10 8 10 9 10 22 Traffic map page 10 16 Traffic map page 10 7 10 8 10 9 10 11 10 19 Transponder 4 4 Transponder standby mode 4 4 Transponder Status bar 4 5 Trim adapter 6 22 Tropical storms 10 5 Turbine Inlet Temperature 3 2 3 4 3 7 Turbine Inlet Temperature TIT 3 7 TX 4 3 7 23 U Unable to display chart 11 12 11 15 Unlighted obstacle 10 15 10 20 V Vacuum Pressure 3 2 3 8 VDI 7 16 Vertical Deviation 2 2 2 6 Vertical deviation guidance 1 10 1 11 Vertical Deviation Indicator 7 16 Vertical navigation 1 10 1 11 Vertical Navigation flight control 6 10 6 14 Vertical Path Tracking Mode 6 10 6 11 6 29 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Index 3 INDEX Index 4 Vertical speed 1 4 2 7 Vertical Speed Bug 2 7 vertical speed guidance 1 10 1 11 Vertical Speed Mode 6 7 Vertical Speed Reference 6 7 Vertical track 13 6 VHF 4 1 VNAV 1 11 7 1 7 2 7 3 7 4 VNAV Target Altitude 6 10 6 13 VNAV Target Altitude Capture Mode 6 13 VNV 1 10 1 11 7 15 13 22 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Voltmeter 3 3 3 9 Volume squelch 5 4 VS 1 4 VSI 7 16 Vspeeds 2 3 W WAAS 2 6 6 24 7 5 13 16 WARN 2 11 2 12 WARNING 13 2 Weather data link page 10 4 Weather product symbol 10 5 Weather product symbols 10 6 Weather warnings 10 5 Wind direction 10 5 Wind speed 10 5 Wings level 6 16 6 18
59. performed by the system while flying the holding pattern the display may re size automatically and the aircraft may not precisely track the holding pattern Flying a missed approach 1 Push the GA Switch at the Decision height and apply go around power to execute a missed approach The flight director Command Bars establish a nose up climb to follow If flying an ILS or LOC approach the CDI also switches to GPS as the navigation source Note that when the GA Switch is pushed the missed approach is activated and the autopilot disconnects indicated by the AP annunciation flashing yellow for 5 seconds and the autopilot disconnect aural alert Flashes 5 sec PGA LAP ALT 2 Start the climb to the prescribed altitude in the published Missed Approach Procedure in this case 10 000 ft a After climbing to altitude exceeding the autopilot minimum engage height press the AP Key to re engage the autopilot b Press the NAV Key to have the autopilot fly to the hold GPS AP ALT 3 Use the ALT Knob to set a Selected Altitude to hold To hold the current airspeed during the climb press the FLC Key J GPS AP TE 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL As the aircraft nears the Selected Altitude the flight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds J GPS AP ALT The green ALT
60. service req d memory The G1000 system should be serviced MANIFEST GMA1 software The audio panel has incorrect software installed The G1000 system should be mismatch communication halted serviced GMA1 SERVICE GMA1 needs The audio panel self test has detected a problem in the unit Certain audio service Return unit for repair functions may still be available and the audio panel may still be usable The G1000 system should be serviced when possible GIA 63 Message Advisories Message Comments S O GIA1 CONFIG GIA1 contig error Contig service req d The GIA1 and or GIA2 configuration settings do not match backup configuration GIA2 CONFIG GIA2 config error memory The G1000 system should be serviced Contig service req d GIA1 CONFIG GIA1 audio contig error Contig service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system GIA2 CONFIG GIA2 audio config should be serviced error Contig service req d GIA1 COOLING GIA1 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to GIA2 COOLING GIA2 temperature warm up to operating temperature too low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 GIA2 COOLING GIA2 over system should be serviced temperature GIA1 SERVICE GIA1 needs service Return the unit for repair The GIA1 and or GIA
61. situation should correct itself within a few seconds If there is an actual failure a red X soon appears over the Attitude Indicator Display system is not receiving airspeed input trom air data computer 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 7 SECTION 13 ANNUNCIATIONS amp ALERTS system Annunciation Commet Display is not receiving altitude input from the air data computer Display is not receiving vertical speed input from the air data computer E Display is not receiving valid heading input from AHRS o Display is not receiving valid transponder information Different versions of GDU software are installed in the PFD and MFD This can also indicate different versions of navigation software are installed in the PFD and MFD In some circumstances a cross talk error between the PFD and MFD can cause this annunciation LOI Indicates Loss of Integrity of GPS information GPS information is either not present or is invalid for navigation use DR may also be seen indicating that GPS is in Dead Reckoning Mode Note that AHRS utilizes GPS inputs during normal operation AHRS operation may be degraded if GPS signals are not present see AFMS A red X through any other display field such as engine instrumentation EGON Redes nt fields indicates that the field is not receiving valid data 13 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 0038
62. small FMS Knob to select pages within the group See Figure 1 7 rs A rs A optional optional DCLTR 1 ae A Default softkey ones is dependant on Press the BACK Softkey on this DCLTR 3 the selecti d level to return to the top softkey level A A vy vy options optional optional optional TRAFFIC STRMSCP NEXRAD XMLTNG aN Nw A Press the ENGINE or BACK Softkey to return to the default Engine Page level The DONE Softkey changes to UNDO when the checklist item is already checked mam mw D Press the BACK Softkey to return Press the ENGINE Softkey to to the previous softkey level j the default Engine Page level CRE TE Se er Ger er er Ee a N X airframe specific values a Figure 1 6 MFD Softkeys Nearest Group Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group MAP U U L Figure 1 7 Page Group Icon Selected Page 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 1 SYSTEM OVERVIEW 1 10 1 5 VERTICAL NAVIGATION One of two altitude sources is used by the G1000 when giving vertical navigation guidance WAAS GPS altitude is used when giving guidance for a WAAS approach after the Final Approach Fix Baro corrected altitude is used when vertical guidance is given in all other situations and in non WAAS systems The G1000 system can use altitude constraints
63. small FMS Knob to select the desired backlighting 6 Turn the large FMS Knob to highlight MFD DSPL gt AUTO and repeat steps 3 through 5 PFD DSPL MFD DSPL Figure 1 10 PFD Setup Menu Window 1 7 DATABASE UPDATES The G1000 System uses Secure Digital SD cards to load and store various types of data For basic flight operations SD cards are required for database storage as well as Jeppesen aviation and ChartView database updates Garmin G1000 Cockpit Reference Guide for the Cessna Nav III The following procedures pertain to updating the G1000 system with SD cards as outlined in Appendix B of the G1000 Cessna Nav III Pilots Guide CAUTION Do not load Jeppesen navigation data except ChartView onto Garmin Supplemental Data Cards NOTE Loading a database in the system prior to it s effective date will result in the expiration date on the power up screen and the effective date on the AUX SYSTEM STATUS Page being displayed in yellow Jeppesen Aviation Database NOTE After the aviation database is installed the card may be removed after loading the update to each LRU Updating the Jeppesen aviation database 1 With the G1000 System OFF insert the SD card containing the aviation database update into the top card slot of the PFD to be updated Label of SD card facing left 2 Turn the G1000 System ON A prompt similar to the following is displayed in the upper left corner of the PFD DO YOU WANT
64. the VNAV altitude field Enter the desired altitude Press the ENT Key The option to select MSL or AGL is now displayed Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor now highlights the VNAV offset field Enter the desired offset distance Press the ENT Key SECTION 7 NAVIGATION 9 Turn the large FMS Knob to place the cursor in the COURSE field 10 Enter the desired course 11 Press the ENT Key The cursor now highlights ACTIVATE 12 Press the ENT Key again to begin navigation using the selected destination altitude constraint and course Canceling Direct to Navigation 1 2 3 Press the Direct to 8 Key Press the MENU Key to display the Direct to options menu With Cancel Direct To NAV highlighted press the ENT Key If a flight plan is still active the G1000 resumes navigating the flight plan along the closest leg PAGE HENL OPTIONS Concel Direct To Press the FMS CRSA knob to return to bose poge Figure 7 6 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol DIRECT TO Identifier ae a WPT Location Facility Name SE VNAV Target Altitude jG Saale OFFSET 5NM Offset Distance Bearing to WPT DIS 1074NM Distance from WPT Course to Selected WPT ACTIVATE Figure 7 7 PFD Direct to Window Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3
65. the Navigation Map Page 1 With the Navigation Map Page displayed push the Joystick to activate the panning function The target pointer is displayed at the present aircraft position 2 Move the Joystick to place the pointer at the desired position 3 Press the ENT Key The User Waypoint Information Page is now displayed with the captured position If the pointer is inside an airspace a dialog box will gt appear giving the choice to review the airspace Figure 8 3 Active Flight Plan Page on the MFD information or create a waypoint 8 3 ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page 4 Turn the FMS Knobs to select a waypoint name 5 Press the ENT Key to accept the selected name The first reference waypoint field is highlighted 6 If desired turn the FMS Knobs to enter the identifier of the reference waypoint and the radial and distance to the reference waypoint Press the ENT Key to accept 7 Press the FMS Knob to remove the flashing cursor or press the GO BACK Softkey to return to the map 8 2 VIEWING THE ACTIVE FLIGHT PLAN Press the FPL Key DTK DIS Figure 8 4 Flight Plan Catalog Page Approach ILS 30R iof 2 Press the FMS Knob to activate the cursor Figure 8 2 Active Flight Plan Window on the PFD 3 Turn the large FMS Knob to highlight the desired flight plan and press the ACTIVE Softkey 4 With OK highlighted
66. the Navigation Map AIRWAYS Pressing this softkey displays removes airways information The default is dependent on map setup option selected Pressing cycles through all airways displayed AIRWY ON low altitude airways only AIRWY LO and high altitude airways only AIRWY HI STRMSCP optional Pressing this softkey displays removes Stormscope lightning data on the Navigation Map NEXRAD optional Pressing this softkey displays removes precipitation data on the Navigation Map XM LING optional Pressing this softkey displays removes XM Radio lightning data on the Navigation Map BACK Pressing this softkey displays the ENGINE and MAP top level softkeys DCLTR declutter Pressing this softkey removes map information in three levels SHW CHRT Show Chart optional Pressing this softkey displays optional FliteCharts or ChartView charts CHKLIST checklist optional Pressing the CHKLIST Softkey displays the Checklist Page ENGINE Displays engine softkeys DONE Pressing this softkey checks off a checklist item If an item is already checked an UNDO Softkey is displayed 1 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 1 SYSTEM OVERVIEW EXIT Press to exit the checklist 1 4 MFD PAGE GROUPS EMERGCY Pressing this softkey displays the emergency checklist 1 Turn the large FMS Knob until the desired page group Is selected 2 Turn the
67. the alert message list 1 Annunciation Window GOC1 CONFIG GDC1 confisuration error Config service req AHRS TAS AHRS not receiving airspeed APPR VPROF Approaching VNAV Alerts Window ro j C E ALERTS Softkey F Annunciation Figure 13 1 G1000 Alerting System 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 1 SECTION 13 ANNUNCIATIONS amp ALERTS 13 1 ALERT LEVEL DEFINITIONS WARNING The G1000 Alerting System as installed in Cessna Nav Ill aircraft uses three alert levels Figure 13 2 WARNING Softkey Annunciation e WARNING This level of alert requires immediate pilot attention A warning alert is annunciated in the Annunciation Window and is accompanied by a continuous aural tone Text appearing in the Annunciation Window is RED A warning alert is Figure 13 3 CAUTION Softkey also accompanied by a flashing WARNING Soitkey Annunciation annunciation as shown in Figure 13 2 Pressing the WARNING Softkey acknowledges the presence of the warning alert and stops the aural tone if ADVISORY applicable DYI SORY e CAUTION This level of alert indicates the Figure 13 4 ADVISORY Softkey existence of abnormal conditions on the aircraft panunciaNon that may require pilot intervention A caution alert is annunciated in the Annunciation Window and is accompanied by a single aural tone Text appearing in the Annunciation Window is YELLOW A caution alert is
68. use the large FMS Knob to move the cursor to the next field HRON snes 8 For periodic and one time message use the FMS TRIP STATISTICS mm Knob to enter the timer value HH MM SS from ODOMETER tect ESSAG TRANSPONDER ALTIHITR TRIP ODOMETER CONH y Event TRIP AVERAGE 65 B AKT AT B1 APR 08 which to countdown and press the ENT Key Seats 9 For event based messages a Use the FMS Knob to enter the desired date DD MM YY and press the ENT Key b Press the ENT Key again or use the large FMS Knob to move the cursor to the next field c Use the FMS Knob to enter the desired time HH MM and press the ENT Key 10 Press the ENT Key again or use the large FMS Knob Figure 11 29 Scheduler Utility Page to move the cursor to enter the next message Entering a scheduler message Deleting a scheduler message 1 Select the AUX Utility Page 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the large FMS Knob to highlight the first empty scheduler message naming field 4 Use the FMS Knob to enter the message text to be displayed in the Alerts Window and press the ENT Key 5 Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type 4 Press the CLR Key to clear th
69. with GPS 1 2 3 Press the OBS Softkey to select OBS Mode Turn the CRS Knob to select the desired course to from the waypoint Press the OBS Softkey again to disable OBS Mode NOTE The OBS Softkey is only displayed when navigating an active leg using GPS Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 9 WIND DATA When the window is selected for display but wind information is invalid or unavailable the window shows NO WIND DATA Wind data can be displayed in three different ways e Wind direction arrows with headwind and crosswind components Option 1 e Wind direction arrow and speed Option 2 e Wind direction arrow with direction and speed Option 3 Option 1 Option 2 ya cc No Data NO HIND DATA Option 3 Figure 2 30 Wind Data Window Displaying wind data 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data below the Selected Heading 3 Press one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey 190 00384 09 Rev A 2 10 GENERIC TIMER REFERENCES mt 32 ON 0m OS T ART TIMER 00 25 05 DN TIMER 00 25 13 UP Figure 2 31 Timer Status Prompts Change the Generic Timer 1 190 00384 09 Rev A Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then pres
70. 000 Cockpit Reference Guide for the Cessna Nav III i TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 1 SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the complete system are found in the Garmin G1000 Pilot s Guide for the Cessna Nav III 190 00498 04 SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions for the Primary Flight Display PFD Multi Function Display MFD and the GMA 1347 Audio Panel System A NOTE The pilot should read and thoroughly understand the Cessna Pilot s Operating Handbook POH for limitations procedures and operational information not contained in this Cockpit Reference Guide The Cessna POH always takes precedence over the information found in this guide 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS D O ies EMERG PUSH 1 2 CRS 4 BARO PUSH PUSH HDG SYNC CRS CTR RANGE Ph amr v PUSH PAN MENU PUSH CRSR _ __ MENU PUSH CRSA GFC 700 AFCS Only Figure 1 1 PFD MFD Controls 12 Garmin G1000 Cockpit R
71. 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select the first rectangular page icon 3 The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL Softkey Starting WPT Ending WPT fa ieee Figure 8 21 Trip Planning Page 4 For Direct to planning press the WPTS Softkey and verity that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Turn the FMS Knobs to enter the identitier of the ending waypoint and press the ENT Key to accept the waypoint Or 190 00384 09 Rev A 190 00384 09 Rev A For point to point planning turn the FMS Knobs to enter the identifier of the starting waypoint Once the waypoints identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For flight plan leg planning press the FPL Softkey at the bottom of the display and turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field and turn the small FMS Kno
72. 10 seconds waypoint aoe Selected Altitude of 9 400 MSL ALT Mode VNAV Target Altitude of 9 000 MSL ALT Mode Selected Altitude OPSHN HABUK 3 nm A A Figure 6 36 Non path Descent 6 30 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Approach Flying an ILS approach 1 Transition trom GPS Navigation Mode to Heading Select Mode a Select the Runway 35L ILS approach for KCOS and select VECTORS for the transition Load and activate the approach into the flight plan b Use the HDG Knob to set the Selected Heading after getting vectors from ATC c Press the HDG Key The autopilot turns the aircraft to the desired heading d Use Heading Select Mode to comply with ATC vectors as requested J GPS AP ALT 2 Arm LOC Approach and Glideslope modes a Ensure the appropriate localizer frequency is tuned b Press the APR Key when cleared for approach to arm Approach and Glideslope modes LOC and GS appear in white as armed mode annunciations _ GPS AP ALT c The navigation source automatically switches to LOC After this switch occurs the localizer signal can be captured and the flight directors determine when to begin the turn to intercept the final approach course The flight director now provides guidance to the missed approach point 3 There are two options available at this point as the autopilot flies the ILS approach
73. 1000 Cockpit Reference Guide for the Cessna Nav III Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel that the XM Radio is using The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Channels can be stepped through one at a time or may be selected directly by channel number Selecting a channel from the channel list 1 While on the XM Radio Page press the CHNL Softkey 2 Press the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or 1 Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 2 Press the ENT Key to activate the selected channel Selecting a channel directly 1 While on the XM Radio Page press the CHNL Softkey 2 Press the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Press the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel 190 00384 09 Rev A Category The Category Box of the XM Radio Page displays the currently selected category of audio Categories of channels such as jazz rock or news can be selected to list the available channels for a type of music or other contents One of the optional categories is PRESETS to
74. 1000 Cockpit Reference Guide for the Cessna Nav III NOTE Pressing the CWS Button while in Selected Altitude Capture Mode does not cancel the mode Use of the ALT Knob to change the Selected Altitude while Selected Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode with Selected Altitude Capture Mode armed for the new Selected Altitude Altitude Hold Mode ALT Altitude Hold Mode can be activated by pressing the ALT Key the flight director maintains the current aircraft altitude to the nearest ten feet as the Altitude Reference The flight directors Altitude Reference is shown in the AFCS Status Box and is independent of the Selected Altitude displayed above the Altimeter Altitude Hold Mode active is indicated by a green ALT annunciation in the AFCS Status Box Altitude Hold Mode is automatically armed when the flight director is in Selected Altitude Capture Mode Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude error is less than 50 ft In this case the Selected Altitude becomes the flight director s Altitude Reference Changing the Altitude Reference NOTE Turning the ALT Knob while in Altitude Hold Mode changes the Selected Altitude but not the flight director s Altitude Reference and does not cancel the mode With the CWS Button depressed the aircraft can be hand flown to a new Altitude Reference When the CWS Button is released at
75. 2 self test has detected a problem in the unit The G1000 GIA2 SERVICE GIA2 needs service system should be serviced Return the unit for repair 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 13 SECTION 13 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Message Comments MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should MANIFEST GIA2 software mismatch be serviced communication halted COM1 TEMP COM1 over temp Reducing transmitter power i The system has detected an over temperature condition in COM1 and or COM2 The 3 transmitter is operating at reduced power If the problem persists the G1000 system COMI TEMIR OA OVET demp should be serviced Reducing transmitter power COM1 SERVICE COM1 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may COM2 SERVICE COM2 needs still be usable The G1000 system should be serviced when possible service Return unit for repair COM1 PTT COM1 push to talk ke eie P The COM1 and or COM2 external push to talk switch is stuck in the enable or OM PTT COM ouchtotakk pressed position Press the PTT switch again to cycle its operation a p a ete problem persists the G1000 system should be serviced COM1 RMT XFR COM1 remote transfer key is stuck
76. 3 onan 2700 FFLOW i Cruise Fuel Flow TIT aA FUEL QTY GAL L A 1 _ELECTRICAL H BUS 12 245 vots 245 MH BATT 5 13 8 8 AMPs BA Model T182T SECTION 3 ENGINE INDICATION SYSTEM EIS RPM 2700 i 2000 Maximum FFLOW GPH le Fuel cere OIL PRES Y OIL TEMP CHT ee TIT h FUEL TY GAL A i 5 160 76H SH F ELECTRICAL M BUS E E245 vots 245 BATT 13 i AMPS a0 Model T206H OOOO Figure 3 2 Engine Display Turbocharged Aircraft 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 33 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 4 LEAN DISPLAY NOTE The pilot should follow the engine manu facturer s recommended leaning procedures in the Pilot s Operating Handbook POH Engine Manifold Pressure Gauge MAN IN Models 182T T182T 206H T206H Displays engine power in inches of mercury in Hg Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range A white tick mark is displayed indicating the cruise manifold pressure Model T182 only Tachometer RPM Shows propeller speeds in revolutions per minute rpm Red range indicates propeller overspeed warning a white high rpm range indicates above normal operating speeds Models 172S 206H and T206H Fuel Flow FFLOW GPH Shows the current fuel flow in gallons per hour gph Turbine Inlet Tem
77. 4 09 Rev A SECTION 13 ANNUNCIATIONS amp ALERTS A red X may be the result of an LRU or an LRU function failure The Figure 13 6 illustrates all possible flags and the responsible LRUs GIA 63 63W JSM Integrated Avionics jam Units GEA 71 Engine on pres Airframe Unit Or GIA 63 63W Integrated Avionics Unit OIL TEMP EGT FUEL QTY GAL 0 i0 20 oF ELECTRICAL m VOLS H BATT 5 Tan e Aar z Pada taws IPOR FAIL ENGINE INSET PFO COI DME XPOR IDENT TMR REF GDC 4A Air Data Computer Figure 13 6 G1000 System Failure Annunciations 13 8 G1000 SYSTEM MESSAGE ADVISORIES GIA 63 63W Integrated Avionics Units GDC 4A Air Data Computer Database Mismatch in PFD and MFD GRS 77 AHRS Or GMU 44 Magnetometer GIA 63 63W Integrated Avionics Units i CoR ALERTS GTX 33 Transponder Or GIA 63 63W Integrated Avionics Units This section describes various G1000 system message advisories Certain messages are issued due to an LRU or an LRU function failure Such messages are normally accompanied by a corresponding red X annunciation as shown previously in the G1000 System Annunciation section NOTE This section provides information regarding G1000 message advisories that may be displayed by the system Knowledge of the aircraft systems flight conditions and other existing operational priorities must be considered when responding to a mess
78. 4 Now Active Leg 6 The aircraft continues on heading 290 When the crosstrack distance is less than 2 0 nm the XTK disappears from the HSI and the CDI is positioned on the last dot indicating a 2 0 nm distance from the centerline of the next course Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION 7 As the CDI approaches center the aircraft turns 8 At SLN Victor Airway 244 V244 is intercepted onto the active leg as seen in Figure 7 22 Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 7 23 cs ledkr omeod TRK C65 ere A423 136 975 118 000 com FPL ACTIVE FLIGHT PLAN 136 975 118 000 conz MHORTH UP l 5 136 975 136 975 ACTIVE FLIGHT PLAN KMKC KCOS Enroute TOF Airu V4 5LN ULNA HOPES C ALHAS DRAMA Turn right to 262 now _ CRUMSI IN siren iT ya a al SLN 2 LES mo T W r ne a Airuoy VZ44 LAA 1 y A 158 f Wat 12200 CURRENT ViNV PROFILE dail es Shen ACTIVE VAN WPT WPT a vs Tet FPH FRE ao Figure 7 23 Turn to Intercept V244 VS REG Y DEW 9 As seen in Figure 7 24 V244 is now the active flight plan leg F mB Web om cbr TBE aikee 136 975 118 000 con l _ FPL ACTIVE FLIGHT PLAN 136 975 118 004 cone E i q NORTH UP U OO aA a ACTIVE FLIGHT PLAN al 20 NS KMKC KCOS Enroute CEEE TOF Te Airwoy V4LSLN collapsed SL aa ano W244 AA DUHY
79. 8 15 Airway Entry Point Loaded 6 Turn the small FMS Knob to display the Waypoint Information Window and begin entering the desired airway identifier WAYPOINT INFORMATION IDENT FACILITY CITY 1k Figure 8 13 Airway Insertion Point 4 Turn the small FMS Knob to display the Waypoint Vso ST Information Window and begin entering the desired airways entry point WAYPOINT INF OGRHATION IGENT FACILITY CITY hire HORTH UP Press ENT to occept Figure 8 16 Enter Airway Identifier LET a oe 7 When the desired airway is entered press the LD lt _ lt AIRWY Softkey ERG 063 i DIS 390m Maad Fress ENT to occept Figure 8 14 Load Airway Entry Point 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 9 5 SECTION 8 FLIGHT PLANNING 8 Turn either FMS Knob to scroll through the list of available exit points Figure 8 17 Select Desired Exit Point 9 With the desired exit point highlighted press the ENT Key 10 With LOAD highlighted press the ENT Key Figure 8 18 Airway Added to Flight Plan 8 9 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures 8 10 LOAD AN ARRIVAL See the Procedures section for a discussion on loading and activating arrival procedures Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 8 11 LOAD AN APPROACH See the Procedures section for a discuss
80. 84 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 1 SYSTEM OVERVIEW NEXRAD optional Press to display NEXRAD weather and coverage information on the Inset Map XM LTNG optional Press to display XM lightning information on the Inset Map BACK Press to return to the previous level softkey configuration HRZN HDG Displays compass heading along the Zero Pitch line APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm RS ose arb ere AST AERTS nnnnnmnoaunoerHooaAwinuwti iA Se optional evs oars A a E E ence cron E ano aces BRG1 NAV1 Press the STD BARO or BACK Softkey to return to the top level softkeys Figure 1 4 PFD Configuration Softkeys PFD Press to display the additional softkeys for additional configuration of the PFD DFLTS Press to reset default settings on the PFD SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction WIND Displays softkeys to select wind data parameters OPTN I Wind direction arrows with headwind and crosswind components OPTN 2 Wind direction arrow and
81. A GARMIN G1 01010 Integrated Flight Deck Cockpit Reference Guide Cessna NEWAILL System Software 0563 11 or later SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV COM TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES Copyright 2004 2008 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0563 11 or later for Cessna 172R 1725 1821 11827 206H and T206H aircraft Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 040 ORB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin he
82. ABLE inf a2 Kiih 3000F FALUR 261 SAIH BGDDFT CURRENT VRV PROFILE ACTIVE VNU WPT VS TET ESZFPH FPA 25 ped H TIHE TO TOO 3224 20 FPL Figure 7 35 Loaded Approach 13 Note the altitude constraints associated with each of the approach waypoints as seen in Figure 7 36 These altitudes are loaded from the database and are displayed as light blue text indicating these values are designated for use in computing vertical deviation guidance If it is desirable not to use the displayed altitude for calculating vertical deviation guidance perform the following a Press the FMS Knob to activate the cursor b Turn the small FMS Knob to highlight the desired altitude c Press the CLR Key d Press the FMS Knob to deactivate the cursor After making the altitude non designated it is displayed as white text 190 00384 09 Rev A Altitude constraint values associated with the Final Approach Fix FAF and waypoints beyond the FAF cannot be designated for vertical guidance These altitude values are always displayed as white text as in Figure 7 36 Vertical guidance from the FAF to the Missed Approach Point MAP is given using the WAAS GPS altitude source therefore the displayed altitude values are for reference only ACTIVE FLIGHT PLAN DTK DIS ALT 35 S 8nn 16000FT PYNON 352 11 9Nn 10000FT Approach KCOS RNAY 35RGPs LPY HABUK inf G21 53 FALUR 261 CEGIX fof WJSR aap S368FT CURRENT VNV
83. ANH A CEGIX fof 5 6 0Nn RHSSR aap 351 S INH GIGEFT 46 8 4NNM MOGAL sahp CURRENT VNV PROFILE ACTIVE UNV WPT 9000FT at HABLUK iaf VS TGT 7S5FPH FPA 25 VS REO 6Z7FPH TIME TO TO 00 22 TERRAIN VS REQ Z IME oD 22 I Vv DEV 2O0FT 100Ff1 f 1000F7 V244 f JE A 300 VIEW VNY PROF CNCL VNV VNV Figure 7 45 Approach Leg is Now Active To manually activate the approach procedure perform the following steps a Press the PROC Key b Turn the large FMS Knob to highlight ACTIVATE APPROACH as shown in nge 7 46 PROCEDURES OPTIONS ACTIVATE VECTOR TO FINAL BYACTIVATE APPROACH SELECT APPROACH SELECT ARRIVAL SELECT DEPARTURE Figure 7 46 Activate Missed Approach c Press the ENT Key to activate the approach 190 00384 09 Rev A 190 00384 09 Rev A 22 The IAF is the next waypoint At the TOD establish a descent vertical speed as previously discussed in Step 16 The aircraft altitude will be 9 000 feet upon reaching HABUK FPL ACTIVE FLIGHT PLAN 136 975 118 008 conz 5368FT ames ACTIVE FLIGHT PLAN TFR KMKC KOOS NO DATA OTK DIS OPSHN 3N M OPSHN 2 he FSHER i een PYNON sO a Approoch KOOS RNAV 3SRGPS LPV d HARUK lof 261 INM 93000 FALUR BUI FALUR 26 1 5 ANH 6600 CEGIX fof 351 SONM 7800F RHSSR map 351 SINH vas 63I6EFT 3 O ANH 7 sri 1 MOGAL aahp CURRENT VNV PROFILE ACTIVE UNV WPT S OGeT at HABUK laf VS TGT 7S5FPH FPA 25 O BO 82 20 TERRAIN ve ren
84. ARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe oo WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of accord
85. AXI RWY EXTENSION INT WAYPOINT NDB WAYPOINT VOR WAYPOINT CLASS B TMA CLASS C TCA CLASS D RESTRICTED MOA MILITARY OTHER ADIZ TFR Press the FMS CRSR knob to return to base page Figure 11 15 MAP SETUP Menu Aviation Group 190 00384 09 Rev A ALL A A SECTION 11 ADDITIONAL FEATURES 11 3 CHARTVIEW The optional ChartView feature resembles the paper version of Jeppesen terminal procedures charts The MFD depiction shows the aircraft position on the moving map in the plan view of approach charts and on airport diagrams Airport Hot Spots are outlined in magenta ChartView functions are displayed on three levels of softkeys While on the Navigation Map Page Nearest Airports Page or Flight Plan Page pressing the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys CHRT OPT CHRT INFO DP STAR APR WX NOTAM and GO BACK The chart selection softkeys shown in Figure 11 16 appear on the Airport Information Page Pressing the GO BACK Softkey reverts to the top level soltkeys and previous page Pressing the CHRT OPT Softkey advances to the next level of softkeys ALL HEADER PLAN PROFILE MINIMUMS FIT WDTH FULL SCN and BACK While viewing the CHRT OPT Soitkeys after 45 seconds of softkey inactivity the system reverts to the chart selection softkeys i 0a SO Pressing the GO BACK Softkey returns to the top level softkeys and previous pag
86. Altitude Select is used by the Automatic Flight Control System in certain modes in addition to the standard G1000 Altitude Alerter function The following are only available with the GFC 700 AFCS AP Key Engages disengages the Autopilot and Flight Director Pressing the AP Key activates the Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Flight Director and engages the Autopilot in the default pitch axis and roll axis modes Pressing the AP Key again disengages the autopilot and deactivates the Flight Director HDG Key Selects deselects the Heading Select Mode NAV Key Selects deselects the Navigation Mode 21 APR Key Selects deselects the Approach Mode 22 VS Key Selects deselects the Vertical Speed Mode 23 FLC Key Selects deselects the Flight Level Change Mode FD Key Activates deactivates the Flight Director only Pressing the FD Key turns on the Flight Director in the default pitch axis and roll axis modes Pressing the FD Key again deactivates the Flight Director and removes the command bars unless the Autopilot is engaged If the Autopilot is engaged the FD Key is disabled 25 ALT Key Selects deselects the Altitude Hold Mode VNV Key Selects deselects Vertical Navigation Mode 27 BC Key Selects deselects Back Course Mode NOSE UP NOSE DN Keys Controls the active pitch reference for the Pitch Hold Vertical Speed and Flight Level Cha
87. C 74A has incorrect software installed The G1000 system should be mismatch communication halted serviced Miscellaneous Message Advisories FPL WPT LOCK Flight plan Upon power up the G1000 system detects that a stored flight plan waypoint is waypoint is locked locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved aviation database update Verify that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired DB CHANGE Database changed This occurs when a stored flight plan contains procedures that have been Verity user moditied procedures manually edited This alert is issued only after an aviation database update Verity that the user moditied procedures in stored flight plans are correct and up to date DB CHANGE Database changed This occurs when a stored flight plan contains an airway that is no longer Verity stored airways consistent with the aviation database This alert is
88. CATION BRE 250 prs 101H COURSE 2o ACTIVATE Figure 7 27 Enter VNV Altitude e An altitude of 10 000 feet is entered as requested by ATC Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 11 SECTION 7 NAVIGATION 7 12 f Press the ENT Key The cursor is now displayed in the VNV offset field as shown in Figure 7 28 DIRECT TO IDENT FACILITY CITY OPSHN SW USA NORTH UP L LOCATION ERG 260 DIS 10INM mEIURSE 257 ACTIVATE Figure 7 28 Enter VNV Offset Distance g Enter the offset or distance from the waypoint at which the selected altitude will be reached In this case three miles prior to OPSHN is entered In other words the G1000 gives vertical guidance so the aircraft will arrive at an altitude of 10 000 feet three miles prior to OPSHN h Press the ENT Key twice to activate the direct to Note in Figure 7 29 the magenta arrow in the Active Flight Plan Window indicating the direct to OPSHN after the offset waypoint for OPSHN The preceding offset waypoint indicates the offset distance and altitude that was previously entered The remaining waypoints in the loaded arrival procedure have no database specified altitudes therefore dashes are displayed Keep the CDI centered and maintain a track along the magenta line to OPSHN Note the Direct to waypoint is within the loaded arrival procedure therefore phase of flight scaling for the CDI changes to Term
89. Cessna Nav III Pressing the HEADER Softkey shows the header view approach chart briefing strip on the screen KPDK PDK fy JEPPESEN DEKALB PEACHTREE 7OCT OS ATS LAOS mhin Ter Hii ATLANTA Appetadh F ATLANTA GA ILS Rwy 20L PEACHIMEE Tawar ETAF 120 9 128 4 126 97 Gs TLS DAjH HAMD CONDITIONAL Ap Eley 1005 2652 pea 1241 p50 roze FHT Misse0 APCH Climb to 1400 then climbing RIGHT turn to S000 via 430 hdg and outbound on ATL VOR R 006 to GORST INT D 6 0 ATL and hold Alt Sen INCHES Trans leval Fl 180 Trans alt 16000 1 OME or RADAR required 2 Use local altimeter seitings if not received use Fulton Co Arawn Field abimeiar saning 3 G5 unusable for coupled approach below 1900 d humerous towers 1o heights of 2000 plus in sector south of alrperi 3 Pilot contralled lighting 120 0 PLAN PROFILE MINIMUMS FIT WDTH Figure 11 18 Approach Information Page Header View Pressing the PLAN Softkey shows the approach chart two dimensional plan view ORS jagi y OM ATLA fAF in Lip APPROACH INFORMATION h a iv i LS AAT 26L 3171 E iH fa ia 1435 A B jada AC 4 ry oo A o ih a S Hs oo 203 111 1 IPDK i 1ago y axe ae ATLANTA VOR H10 PROFILE MINIMUMS FIT OTH Figure 11 19 Approach Information Page Plan View 190 00384 09 Rev A SECTION 11 ADDITIONAL FEATURES Pressing the PROFILE Softkey displays the approach If the chart scale has been adju
90. D card contains an invalid checklist file or no checklist the Power up Page messages display Invalid Checklist File or Checklist File Not Present and the CHKLIST Softkey is not available From any page on the MFD press the CHKLIST Softkey Turn the large FMS Knob to select the GROUP field Turn the small FMS Knob to select the desired procedure and press the ENT Key Turn the large FMS Knob to select the Checklist field Turn the FMS Knob to select the desired checklist and press the ENT Key Turn the FMS Knob to scroll through the checklist and highlight the desired checklist item A hollow white box is used for the checkmark The following colors are used for checklist items e Blue Items has not been highlighted e White Item is highlighted for selection e Green Item has been selected e Yellow Warning notes Press the ENT Key or DONE Softkey to check the highlighted checklist item The line item turns green and a checkmark is placed in the box next to it The next line item is automatically highlighted for checking Press the CLR Key to remove a check mark from an item Optional Sse oe CCC CC ones as es es ts ts ts ts ts es es NA oe et eee MNN NNN NNN KN A The DONE Softkey label changes to UNDO when the checklist item is already checked 11 20 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Figure 11 30 Checklist Softkeys 190 00384 09 Rev A Once the last item in a checkli
91. DURES OPT TONS SELECT APPROACH SELECT DEPARTURE LOADED APPROACH ARRIVAL KCOS TBE DBRY IALL DEPARTURE KMKC ALL WLDCT2 SLN Press the PROC key to view the previous page Figure 7 30 Procedures Window c Press the ENT Key A list of available approaches for the destination airport is displayed as in Figure 7 31 AIRPORT KEOS W PUBLIC CITY OF COLORADO SPRINGS COLORADO SPRINGS CO APPRORCH CHANNEL To W354 APPROACH RNAV 35RGps LPY SEQUENCE CEGIX fof LOAD om ACTIVATE Figure 7 31 List of Available Approaches SECTION 7 NAVIGATION d Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 7 31 e Press the ENT Key A list of available transitions for the selected approach is displayed as shown on Figure 7 32 ALRPORT KEOS PUBLIC CITY OF COLORADO SPRINGS COLORADO SPRINGS CO SEQUENCE HABUE lof FALUR 261 S N CEGIX fof BONA RW35R mop 5 1NH b LOAD om ACTIVATE Figure 7 32 List of Available Transitions f Turn either FMS Knob to select the desired transition In this case the Initial Approach Fix IAF at HABUK is used g Press the ENT Key 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 13 SECTION 7 NAVIGATION 7 14 h Turn the small FMS Knob in the direction of the green arrow to select BARO as shown in Figure 7 33 This enables the barometric minimums bug display on the a
92. E 262 is GLIDE 22 aes p A o a MYS abe aT Ti RASO Zl 7 ZAHPO 71 COFFE 258 CURRENT VIN PROFILE ACTIVE VIN WET WWW _FT of WWW YS TGT eee ee V5 REG __ FPH TIME TO TOO BANH FPL Figure 7 24 V244 Now Active Le Figure 7 22 Turn on to Active Leg q 710 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A 10 At Lamar VOR LAA V263 is intercepted See Figure 7 25 136 975 118 000 com 136 975 118 000 corz NORTH UP ACTIVE FLIGHT PLAN n AA J4 7 RANK J repu _ Arrival KCOS TBE DBRY 1 ALL Ox 210 TLIN CURRENT VNV PROFILE ACTIVE VNV WPT T ot VS TGT FPM FPA VS REO FPH TIHE TO TOO V DEV FT V210 Figure 7 25 HYS to LAA Leg Active 11 ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure and issues a crossing altitude restriction of 10 000 feet at OPSHN a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to select OPSHN in the flight plan list c Press the Direct to 8 Key The Direct to Window is now displayed as shown in Figure 7 26 190 00384 09 Rev A SECTION 7 NAVIGATION DIRECT TO IDENT FACILITY CITY EE SH LISA LOCATION ce 26 DIS 10111 COURSE 2o ACTIVATE Figure 7 26 Direct To OPSHN d Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7 27 E IDENT FACILITY CIT r OPSHN a SH USA HINH NORTH UF LO
93. ECTION 7 NAVIGATION e With SLN still highlighted as in Figure 7 15 turn emmy the small FMS Knob to the right The Waypoint er Information Page is displayed and the LD AIRWY eo Softkey is now available ex JEL f Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7 10 Figure 7 17 List of Available Exits for V4 i If necessary turn either FMS Knob to select the desired exit In this case Salina VOR SLN is selected as seen in Figure 7 17 j Press the ENT Key The selected airway and exit haan Ea are displayed the prompt LOAD highlighted Figure 7 16 List of Available Airways for TOP as in Figure 7 18 ENTRY g Turn either FMS Knob to highlight V4 in the list as seen in Figure 7 16 h Press the ENT Key The list of V4 airway exit em points is now displayed as in Figure 7 17 mAIRE Y SEQUENCE TOP kd oy he ait Paap Figure 7 18 Ready to Load V4 k Press the ENT Key 7 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A V4 is now loaded into the flight plan as shown in Figure 7 19 ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS Departure KMKC ALL TIFTO2 TIFTO MCI TIFTO 205 460NH Enroute TOP Airway 4 5LN ULNA 266 14 11M FT HOPPS 255 SINH FT ALHAS 259 Z05HWH ___FT DRAMA 258 A S a CEKIS CURRENT VNV PROFILE ACTIVE WNW WPT VS TGT
94. EOFF ROLL O1 Throttle IDLE pull full out O2 Brakes APPLY O3 Wing Flaps RETRACT O4 Mixture Control DLE CUT OFF pull full out 05 MAGNETOS Switch les O06 STBY BATT Switch O7 MASTER Switch ALT and BAT ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF O1 Airspeed T0 KIAS Flaps UP 65 KIAS Flaps FULL o2 Mixture Control IDLE CUT OFF fpull full out O3 FUEL SHUTOFF Valve OFF pull full out O4 MAGNETOS Switch IE 05 Wing Flaps AS REQUIR O6 SIBT BATT Switch g O7 MASTER Switch ALT and BAT a O8 Cabin Door UNLATC 09 Land STRAIGHT AHEA ENGINE FAILURE DURING FLIGHT RESTART PROCEDURES O1 Airspeed 68 KIAS 2 FUEL SHUTOFF Valve ON push full in JEL SELECTOR Valve BOT UEL PUMP Switch ON vlixture Control RICH if restart has not occurred l MAGNETOS Switch BOTH for START if propeller is stopped O6 FUEL PUMP Switch Figure 11 32 Emergency Checklist Page Example Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 12 ABNORMAL OPERATION 12 1 REVERSIONARY MODE Should a system detected failure occur in either display the G1000 automatically enters Reversionary Mode In Reversionary Mode critical flight instrumentation is combined with engine instrumentation on the remaining display Reduced navigation c
95. Flight level change 1 4 Flight Level Change Mode 6 28 6 30 Flight Level Change Mode FLC 6 8 Flight Plan Catalog 9 1 9 2 FliteCharts 11 14 FliteCharts functions 11 14 FLTA 10 15 10 18 Forward Looking Terrain Avoidance 10 15 10 18 Freezing level 10 5 Frequency toggle key 1 3 4 3 Fuel Calculations 3 7 Flow totalizer 3 7 Remaining 3 9 Used 3 8 Fuel Flow 3 1 3 3 3 4 3 8 Fuel Quantity 3 2 3 4 3 9 G GA Switch Go Around 6 1 Glidepath 2 2 2 6 7 19 Glidepath Mode 6 14 6 20 Glidepath Mode GP 6 32 Glideslope 2 6 7 19 Glideslope Mode 6 15 6 20 Glideslope Mode GS 6 31 GMA 1347 1 1 Go Around Mode GA 6 16 6 33 6 34 Heading indication 2 9 Heading Select 1 3 1 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Heading Select Mode 6 18 Heading Select Mode HDG 6 25 Headset s 5 3 Horizontal situation indicator 2 8 HSI 2 8 Hurricanes 10 5 ID RR 1 1 3 4 2 4 3 4 6 IDENT function 4 5 ILS approach 6 31 Imminent Terrain Impact 10 15 10 18 Impact point 10 15 10 18 Inhibit 10 15 10 17 Interrogations 4 5 IOI 10 13 10 15 10 18 10 21 13 5 ITI 10 15 10 18 K Key s 1 4 L Lean Display 3 5 Leaning 3 Leaning Engine 3 4 Lean Display 3 1 3 4 3 6 Lighted obstacle 10 15 10 20 Lightning 1 5 1 8 10 2 10 3 10 4 LNAV 2 6 7 5 Load approach 8 6 Load a VOR frequency 7 28 Load departure 8 6 Load the frequency for a controlling agency 7 30 Load the nearest A
96. GHT CONTROL Pitch Hold Mode PIT Changing the Pitch Reference When the flight director is activated the FD Key is When operating in Pitch Hold Mode the pitch pressed Pitch Hold Mode is selected by default Pitch reference can be adjusted by Hold Mode is indicated as the active pitch mode by the Using the NOSE UP NOSE DN Keys green annunciation PIT This mode may be used for e Pressing the CWS Button hand flying the aircraft climb or descent to the Selected Altitude shown above to establish a new pitch reference then releasing the Altimeter since Selected Altitude Capture Mode is the CWS Button automatically armed when the mode is activated In Pitch Hold Mode the flight director maintains a constant pitch attitude the pitch reference The pitch reference is set to the aircraft attitude at the moment of mode selection If the aircraft pitch attitude exceeds the flight director pitch command limitations the flight director commands a pitch angle equal to the nose up down limit Pitch Hold Selected Altitude Mode Active Capture Mode Armed Selected Altitude OU b gt 1040 K UDDA Command Bars Maintain Desired Pitch Reference 29 921N Figure 6 5 Pitch Hold Mode 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 5 SECTION 6 AUTOMATIC FLIGHT CONTROL Selected Altitude Capture Mode ALTS Selected Altitude Capture Mode arms automatically when the flight dir
97. I 2 D2 2 Lu gt mn Z 59 ba JU nA Ho Sse Mic 7 TT ee a L lt O lt a4 A FUEL amp TY LA i BNN S T L i BARRANIN M 5 S Hollow Block Peak Represents 2700 ee CE gt EE A A i AN S A i nS EEE E UL FUEL amp TY ANURA MUNNI T tT i ke NIN MUNNI NNI TE L MNI 5 HT g m LLI F MNN MUNIN G MNN MUANI US md ay FUEL QTY GAL Model 206H Model 182T Model 172S Model 172R Figure 3 3 Lean Display Normally aspirated Aircraft 33 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS Cruise Manifold Pressure RPM z fH e 195 FFLOW GPH TIT F 1556 Sr APEAK 9 F 12345 6 12345 G 1455 1565 12345 6 12345 6 C 460 C 435 pa a Model T182T Model T206H Figure 3 4 Lean Display Turbocharged Aircraft The Lean Display is accessed by pressing the ENGINE From the Lean Display the pilot can utilize the CYL Softkey followed by the LEAN Softkey and provides SLCT and ASSIST softkeys to obtain information about specific cylinders Pressing the CYL SLCT Cylinder Select Softkey cycles through the cylinders i e changes the cylinder indicated on the bar graphs in light blue This softkey is disabled when the ASSIST Softkey is pressed or when a cylinder experiences a caution or warning condition the softkey remains
98. ITY H CEN USA Figure 7 4 Nearest Airport List MFD 3 Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position as shown in Figure 7 4 4 Turn the large FMS Knob to select the desired airport 5 Press the ENT Key The cursor is now displayed on ACTIVATE 6 Press the ENT Key again to activate a Direct to Select a Direct to Destination to a Recently Entered Identifier 1 Press the Direct to E Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 3 The list is populated only when navigating a flight plan 190 00384 09 Rev A 3 4 5 6 DIRECT TO IDENT FACILITY CITY kj W CEM USA KSLH a DE T RSH f A Figure 7 5 Recently Entered Waypoints List MFD Turn the small FMS Knob to the right to display the RECENT waypoints as shown in Figure 7 5 Turn the large FMS Knob to select the desired airport Press the ENT Key The cursor is now displayed on ACTIVATE Press ENT again to activate a Direct to Re center the CDI to the Destination Waypoint Press the Direct to Key followed by pressing the ENT Key twice If a missed approach point MAP is the current destination the approach is canceled Manually Define the Active Direct to 1 2 3 4 5 6 1 8 190 00384 09 Rev A Press the Direct to 8 Key Turn the large FMS Knob to highlight
99. It the aircraft altitude is above the specitied altitude after crossing the MAP a direct to is established to the published fix MOGAL to begin the missed approach procedure The altitude constraint value defaults to 400 feet AGL when there is no Course to Altitude defined in the published procedure In some missed approach procedures a Course to Altitude leg may be part of the published procedure For example the procedure dictates a climb to 5 500 feet then turn left and proceed to the Missed Approach Hold Point MAHP The altitude would appear in the list of waypoints as 5500 1 Again if the aircraft altitude is lower than this prescribed altitude a direct to is established on a Course to Altitude leg when the missed approach procedure is activated 25 Upon reaching the MAP it is decided to execute a missed approach Automatic waypoint sequencing is suspended past the MAP Press the SUSP Softkey on the PFD to resume automatic waypoint sequencing through the missed approach procedure 190 00384 09 Rev A A direct to is initiated to MOGAL which is the Missed Approach Hold Point MAHP as seen in Figure 7 50 The aircraft is climbing to 10 000 feet The CDI flight phase now changes from LPV to MAPR as seen on the HSI 136 975 118 000 conz OTK ALT Sate ees ETML Sel eee Approach KDOS RMAY 35Riees LPY SS pee N CURRENT VNV PROFILE ACTIVE UNU WPT _ VS TGT Vo REG Y DEW a y BARO MIN 4 637
100. MS Knob to activate the cursor the FMS Knob to activate the cursor 2 Enter an intersection identifier and press the ENT 2 Turn the large FMS Knob to highlight the desired Key selection field identifier name or closest city 3 Press the FMS Knob to remove the flashing 3 Enter an identifier name or city and press the ENT cursor Key 4 Press the FMS Knob to remove the flashing CUrSOr 134 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Figure 7 59 VOR Information Page Select the VOR Information Page 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the fourth rectangular page icon Access Information on a VOR 1 With the VOR Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the desired selection field identifier name or closest city 3 Enter an identifier name or city and press the ENT Key 4 The FREQUENCY field is now highlighted It desired press the ENT Key to place the frequency in the NAV receiver standby field 5 Press the FMS Knob to remove the flashing cursor 190 00384 09 Rev A SECTION 7 NAVIGATION 7 8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints 7 9 NEAREST AIRPORTS 118 000 conz Figure 7 60 Nearest Airports Page Nearest Airport Informat
101. MYN Anh Mees Gln E I cree Light z Blue Text Approach KDFW RNAV 17LGPS LPV RIVET iof SMEs Oe 2 Small Licht DRAAK 176 3 3NM 2000FT e INWOD 176 3 2NM Small Light rage eo Blue Subdued MENOL faf 176 3 SNM Text RW17L map 176 5 3MM ee Small White SSWFT VIF 4 8NM S Text with f Altitude POLKE Restriction Figure 1 8 VNAV Altitudes Bar 190 00384 09 Rev A Some altitudes retrieved from the database have associated restrictions indicating to stay At At or Above or At or Below a specific altitude These restrictions are indicated using a bar above and or below the appropriate altitude as shown in Figure 1 9 GGT Cross AT or ABOVE 5 000 ft Fae Cross AT 2 300 fi G G Gl am Cross AT or BELOW 3 000 fi Figure 1 9 Altitude Restrictions See Section 7 Navigation for a sample flight plan which further illustrates vertical navigation in more detail Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 1 11 SECTION 1 SYSTEM OVERVIEW 1 12 1 6 BACKLIGHTING Manually adjust the backlight for the PFD and MFD 1 Press the MENU Key on the PFD to display the PFD Setup Menu window 2 Press the small FMS Knob to activate the cursor PFD DSPL gt AUTO is now highlighted 3 Turn the small FMS Knob to display the selection window 4 Turn the small FMS Knob to select MANUAL then press the ENT Key 5 With the intensity value now highlighted turn the
102. PROFILE ACTIVE VNV HPT 1WOBUUFT at OPSHN 3NH VS TGT 7S6FPM FPA VS REQ eee TIHE TO TOD V DEV il Figure 7 36 Vertical Guidance is Active to the FAF 14 As the aircraft approaches OPSHN it may be desirable to adjust how fast or steep the upcoming descent will be The default Flight Path Angle FPA is 2 5 degrees and a required vertical speed is computed to maintain the 2 5 FPA To change the vertical flight path perform the following steps KPUB SECTION 7 NAVIGATION a Press the VNV PROF Softkey to place the cursor in the target vertical speed field VS TGT as shown in Figure 7 37 b At this point the descent vertical speed can be selected or the FPA can be selected Turn the large FMS Knob to select the desired selection field then turn the small FMS Knob to enter the desired value Note the information now displayed in the CURRENT VNV PROFILE box Also note the offset waypoint and a gray circle labeled TOD are now displayed on the map The gray circle marks the Top of Descent TOD In this example after passing the TOD point vertical guidance is provided that results in a 3 0 degree FPA descent to an altitude of 10 000 feet at the offset waypoint TRK ala 136 975 118 608 com FPL ACTIVE FLIGHT PLAN 136 975 118 000 conz NORTH UP a ACTIVE FLIGHT PLAN ktk f KCOS 40 2NH TOCOFT JAH BRARET San 10000FT 11 51 10000FT Approach KOOS RMAW S5RGPS LPW HABUK iof az
103. Path Tracking Mode To proceed with descent path capture if the white VPTH annunciation begins flashing do one of the following Cruise Altitude of 12 000 MSL D ALT Mode 2 tas If the descent is not confirmed by the time of interception Vertical Path Tracking Mode remains armed and the descent is not captured 2 When the top of descent TOD is reached the flight director transitions to Vertical Path Tracking Mode and begins the descent to the VNV Target Altitude Intention to capture the VNV Target Altitude is indicated by the white ALTV annunciation _ GPS AP ALTV 3 As the aircraft nears the VNV Target Altitude the flight director transitions to VNV Target Altitude Capture Mode indicated by the green ALTV annunciation flashing for up to 10 seconds E ALT The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint ALT Mode Selected Altitude set below VNAV Target Altitude Along track Offset 3 nm before OPSHN m A 3 nm Figure 6 35 VPTH Descent Garmin G1000 Cockpit Reference Guide for the Cessna Nav Ill 6 29 SECTION 6 AUTOMATIC FLIGHT CONTROL Non path descent using Flight Level Change SS ALT VPTH Mode mA _ oo The green ALT annunciation flashes for up to 10 1 Command a non path descent usi
104. Press the PATHWAY Softkey The Pathway feature will cycle on or off with the PATHWAY Softkey Activating and deactivating Horizon Headings 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the HRZN HDG Softkey The horizon heading display will cycle on or off with the HRZN HDG Softkey Activating and deactivating Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the APTSIGNS Softkey Display of airport signs will cycle on or off with the APTSIGNS Softkey Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SVS Features Zero Pitch Line ZPL with Flight Compass Airport Path Selected ie be Runway Marker Altitude ww 188 08 117 95 5 ARE newz 108 00 117 95 136 975 136 975 Pathways Airplane lt 5 if Color Matches CDI Symbol oftkeys Indicating NAV Source Figure 11 2 SVS on the Primary Flight Display NOTE Pathways and terrain features are not a substitute for standard course and altitude deviation information provided by the CDI VSI and VDI Pathways Pathways provide a three dimensional perspective view of the selected route of flight shown as colored rectangular boxes representing the horizontal and vertical flight path of the active flight plan The box size represents 700 feet wide by 200 feet tall during enroute oceanic and terminal flight phases During an approach the box width is 700 feet or one half full scale deviation on the
105. RECENT waypoint list 5 Repeat steps 2 through 4 to enter the identifier for each additional flight plan waypoint 3 Repeat step 2 to spell out the rest of the waypoint identifier 4 Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint 5 Turn the large FMS Knob to move the cursor to the next character field Repeat steps 4 and 5 until the 6 Once all waypoints have been entered press the desired identifier has been entered FMS Knob remove the cursor The new flight plan Is now active WAYPOINT INFORHATION IDENT FACILITY CITY y e NORTH UP iT Figure 8 12 Creating Flight Plan on the PFD Figure 8 11 Waypoint Info Window 6 Press the ENT Key 7 Repeat step number 3 4 and 5 to enter the identifier for each additional flight plan waypoint 8 When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list 8 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 8 FLIGHT PLANNING 8 8 ENTER AN AIRWAY IN A FLIGHT 5 When the desired entry point is entered press the PLAN ENT Key 1 Press the FPL Key to display the active flight plan or display a stored flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the waypoint before which the airway is to be entered ACTIVE FLIGHT FLEN Figure
106. RTCC frequency 7 29 LOI 2 11 LOW ALT 2 5 Low Altitude 2 5 LPV 2 6 7 5 7 21 LPV approach 6 24 Manifold Pressure 3 1 3 3 3 4 3 6 3 7 3 9 Manual Electric Trim MET 6 22 MAP 7 1 Map panning 10 5 Marker beacon 2 7 Message advisories 13 2 13 10 13 22 METAR 10 3 10 5 Metric display 2 4 MET Switch Manual Electric Trim 6 1 MFD 1 1 4 4 Minimums 13 6 Missed approach 6 33 MKR MUTE 5 2 5 4 Mode S 4 4 Mode selection softkeys 4 5 Morse code identifier 4 3 Nav Com controls 4 1 NAV1 5 3 NAV2 5 3 Navigation 7 1 Navigation database 1 10 1 11 7 5 Navigation Mode 6 19 6 20 Navigation Mode AFCS 6 26 6 27 Navigation status window 2 2 NAV frequency window 4 1 NCR 10 19 Nearest Airports Page 7 22 7 25 7 27 7 28 7 29 8 1 Nearest ARTCC amp FSS frequencies 7 29 Negative Climb Rate After Takeoff 10 19 NEXRAD 1 8 10 3 10 4 10 5 10 6 Non path descent 6 13 6 30 6 31 190 00384 09 Rev A 0 OBS 2 12 Obstacles 10 10 10 15 10 20 13 12 13 16 Oil Pressure 3 1 3 7 Oil Temperature 3 1 3 8 Operation 5 2 Optional NAV radios 4 3 Overspeed protection autopilot 6 35 P Page group icon 1 9 Passenger address 5 2 PA annunciator 5 2 PA system 5 2 PDA 10 18 Peak Cylinder 3 7 3 8 Peak temperature 3 4 3 7 PFD 1 1 4 1 4 4 Pitch hold 1 4 Pitch Hold Mode PIT 6 5 Pitch modes flight director 6 3 6 9 Pitch Reference 6 5 Power up page 11 20 Premature Desce
107. RVSI appear on the PFD as the flight progresses Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION Turn right to 021 in 7 seconds ACE E ETT ees PTT o 2B FPL ACTIVE FLIGHT PLAN Botts ACTIVE FLIGHT PLAN 20N f LL TFR KMKC KCOS NO DATA DTK DIS TEE oa a Arrival KCOS TBE DBRY 1 ALL OPSHN 3mm EASA eS OPSHN i ae FSHER af pian R PYNON 352 77nn 10000FT Approoch KCOS RNAV SSRors LPV HABUK iaf 821 5 SNN S000 FALUR 261 G NH 8600r CEGIX fof 351 G NH 78 r RH SR map 351 SINH CURRENT UNV PROFILE ACTIVE UNV WPT 9009FT ot HABUK iof VS TOGT 7S5FPH FPA 25 47 1FPM_ TIME TO TOD 0057 VIEH VNV PROF HCL WW VNV VNV Turn right to 021 now f TOD within 1 minute i RASS a EE 20 vE Figure 7 44 Approaching PYNON 7 18 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 21 Upon passing PYNON the approach procedure automatically becomes active The approach may be activated at any point to proceed directly to the IAF In this example the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg activating the approach procedure see Figure 7 45 FPL ACTIVE FLIGHT PLAN 136 975 118 009 conz NORTH UP on ACTIVE FLIGHT PLAN TFR KMKC KCOS NO DATA Vaz OPSHN 3mm OPSHN FSHER HP PYNON 7 pr KCOS RNAV 35R6es LPV HABUK lof 221 5 2N FALUR 261 5
108. System Test OK Aural Message Alert Annunciations S eS Alert Annunciation nan 115 8 117 28 Mee i i DIS za 122 000 121 600 cos ney eT 16 60 114 58 ARG 12 2 308 126 975 cow XPDA IDENT THA REF ET ALERTS 1 Figure 10 33 TAWS Alert Annunciation on the PFD Alert Annunciation Figure 10 32 Alert Annunciation on the TAWS Page 10 22 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 11 ADDITIONAL FEATURES 11 1 SYNTHETIC VISION SYSTEM SVS OPTIONAL NOTE SVS requires a terrain database that has a resolution of nine arc seconds WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic The optional Synthetic Vision System depicts a forward looking attitude display of the topography immediately in front of the aircraft The field of view is 30 degrees to the left and 35 degrees to the right The depicted imagery is derived from the aircraft attitude heading GPS three dimensional position and a nine arc second database of terrain obstacles and other relevant features Loss of any of the required data including temporary loss of the GPS signal will cause SVS to be disabled until the required
109. TO UPDATE THE AVIATION DATABASE FROM TO WORLDWIDE 0604 13 APR 2006 11 MAY 2006 WORLDWIDE 4685 ee ih O42 2 48 JUN 2606 NO WILL BE ASSUMED IN 8 SECONDS Figure 1 11 Database Update Prompt 190 00384 09 Rev A 3 Press the ENT Key to start the database update A prompt similar to the following is displayed DO YOU WANT TO UPDATE THE AVIATION DATABASE FROM TO WORLDWIDE WORLDWIDE 0604 0605 13 APR 2006 TIRNA ZnB 11 MAY 2006 48 JUN 20686 NO WILL BE ASSUMED IN 8 SECONDS UPDATING AVIATION DATABASE PLEASE WAIT UPDATED ea Shy hos Bie Shoe Ey PRESS ANY KEY TO CONTINUE CONTINUING IN 8 SECONDS Figure 1 12 Database Update Confirmation 4 After the update completes the PFD starts in normal mode 5 Turn the G1000 System OFF and remove the SD card 6 Repeat steps 1 through 4 for the MFD The MFD and PFD databases are now updated Remove the SD card when finished 7 Verity that the correct update cycle is loaded during startup of the MFD Garmin Databases Since these databases are not stored internally in the MED or PFD a Supplemental Data Card containing identical database versions must be kept in each display unit NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data 1 Insert one SD card in the bottom card slot of the MFD and one
110. TRIKE RATE HOG UF Sl wee Figure 10 5 Lightning Display Range Annunciation Select cell or strike as the Stormscope lightning mode 1 With the Weather Group selected press the ENT Key The cursor flashes on STRMSCP LING 2 Turn the large FMS Knob to select STRMSCP MODE 3 Turn the small FMS Knob to display the Cell Strike window 4 Turn either FMS Knob to select Cell or Strike Press the ENT Key Figure 10 6 Stormscope Page 5 Push the FMS Knob to return to the Navigation Map Page Change the Stormscope lightning mode between cell and strike Clear Stormscope lightning data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page 2 Press the MODE Softkey The CELL and STRIKE displayed Sottkeys are displayed Press the CELL Softkey to display CELL dat the STRIKE Softkey t 2 Turn either FMS Knob to highlight the Clear ee saa hee arcane en display STRIKE data CELL or STRIKE is displayed Stormscope Lightning field and press the ENT in the mode box located in the upper left corner of 1 Select the Stormscope Page Key the Stormscope Page A NOTE If heading input is lost strikes and or cells NOTE Cell mode uses a clustering program to must be cleared manually after the execution of identify clusters of electrical activity that indicate each turn This is to ensure that the strike and or cells ce
111. Traffic Annunciations e Windows displayed in e AFCS Annunciations the lower right corner e Flight Director of the PFD Command Bars Timer References Inset Map Nearest Airports e Temperatures Flight Plan e DME Information Messages Window Procedures e Wind Data DME Tuning e Selected Heading Box Barometric Minimum e Selected Course Box Descent Altitude Box e Transponder Status e Glideslope Glidepath Box and Vertical Deviation e System Time Indicators e PFD Setup Menu e Altimeter Barometric Setting Selected Altitude e VNV Target Altitude Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Red extreme pitch warning chevrons pointing toward the horizon are displayed starting at 50 degrees above and 30 degrees below the horizon line Figure 12 2 Extreme Pitch Indication 12 4 STORMSCOPE OPERATION WITH LOSS OF HEADING INPUT It heading is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircratt 12 5 HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established The icons in the lower right of the screen indicating the selected functions for display will show an X as shown in Figure 12 3
112. UTOMATIC FLIGHT CONTROL 6 1 6 1 AFCS Controls iccsesiccuintacrncnmsictaceions 6 1 6 2 Flight Director Operation 0 155555551111111 6 2 Activating the Flight Director c ccseesseesceseesesseesseaees 6 2 Command Bais sii ecuat strc ts ates S 6 2 PEGS StalUS BOX o 6 3 6 3 Flight Director Modes 0 0 ccceeeeeen 6 3 PICT Mode maaana e 6 3 ROM VIOGES nornin 6 17 6 4 Autopilot Operation ue 6 22 Fight COMIC adonan 6 22 Engaging the AUtopilot scsssssecessssssesseeseeseen 6 22 Control Wheel Ste ring ccsscesseesssessesseesessesseeaseesees 6 23 Disengaging the Autopilot sceseseeseesecsessesseeen 6 23 6 5 Example Procedures 0 ccccceseeseeseeees 6 24 Diclae iad T ea terre eterna teen terete 6 24 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III TABLE OF CONTENTS Intercepting a VOR Radidl ccscsseseseeseesessesseean 6 26 Flying a Flight Plan GPS COUrS scssessessessesseeen 6 27 BE EEEE ies acted bse T ET 6 28 ADO rsio EO 6 31 Go Around Missed Approach ssssecssessseesseessessees 6 33 6 6 AFCS Annunciations and Alerts 6 34 RECS Sras AICI iaoa nahonaho 6 34 Overspeed Protecti ON izonic 6 35 SECTION 7 NAVIGATION 7 1 7 4 Navigation Map Pag ccccceeseeeen 7 1 7 2 Direct to Navigation 0 0 0c 7 1 Direct to Navigation trom the MFD seseseesecsen 7 1 Direct to Navigation trom the PFD scse
113. VNAV flight plan is active and the VNV Key is pressed Vertical Path Tracking Mode is armed in preparation for descent path capture VPTH or V when Glidepath or Glideslope Mode is concurrently armed is annunciated in white in addition to previously armed modes If applicable the appropriate altitude capture mode is armed for capture of the next VNAV Target Altitude ALTV or the Selected Altitude ALTS whichever is greater GPS VPTH GPS ALTS GP V Figure 6 10 Vertical Path Tracking Armed Annunciations Prior to descent path interception the Selected Altitude must be set below the current aircraft altitude by at least 75 ft For the flight director to transition from Altitude Hold to Vertical Path Tracking Mode acknowledgment is required within five minutes of descent path capture by e Pressing the VNV Key e Adjusting the Selected Altitude If acknowledgment is not received within one minute of descent path interception the white VPTH annunciation and the VNV Key annunciator light start to flash Flashing continues until acknowledged or the descent path is intercepted If the descent is not confirmed by the time of interception Vertical Path Tracking Mode remains armed and the descent is not captured 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL In conjunction with the TOD top of descent within 1 minute annunciation in the Navigation Data Box VNAV indications VNAV Target Altitude verti
114. XM Weather Service Optional 10 3 Displaying METAR and TAF information on the Airport NOLMAUION PACE sassscsaamersmanacinansranauseananarania 10 3 Displaying Weather on the Weather Data Link Page 10 4 Map Panning Information Weather Data Link Page 10 5 Weather Products amp Symbols s s s 10 5 Weather Product AQE ax ccus sasesssssnenesamanesmuemessnaee 10 6 10 4 Traffic Systems 0 c ccccccccesteseesteaseesreaees 10 7 Traffic Information Service TIS 10 7 Traffic Advisory System TAS Optional sesesees 10 8 ADS B Trane QDUGNAl onigaseana 10 9 10 5 Terrain and Obstacle Proximity 10 10 Displaying Terrain and Obstacles on the Terrain Proximity PACE A E tahun A E asa 10 10 Displaying Terrain and Obstacles on the Navigation ILE Sear EA EENAA ANT 10 11 190 00384 09 Rev A TABLE OF CONTENTS 10 6 TERRAIN SVS Display Optional 10 11 SECTION 12 ABNORMAL OPERATION be Displaying Terrain on the TERRAIN SVS Page 10 11 12 1 Reversionary Mode 192 Enable Disable Aviation Data cescsesseseeresren 10 12 12 2 Abnormal COM Operation cccccccssse 12 2 TERRAINS VS ATENO ianareo 10 12 12 3 Unusual Attitudes ccccccccccccscccccccsssscccccssssseee 129 Terrain IN AUN as Bezcacstatsesdecateten cttareaseees duster asentearelec 10 15 12 4 Stormscope Operation with loss of Heading Forward Looking Terrain Avoida
115. a control stick switch rather than the trim wheel Manual trim commands are generated with the MET Switch Trim speeds are scheduled with airspeed to provide more consistent response Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Roll Axis The autopilot roll axis uses roll rate to stabilize aircratt roll attitude during upsets and flight director maneuvers The flight director roll commands are rate and attitude limited combined with roll damper control and sent to the roll servo motor Engaging the Autopilot A NOTE Autopilot engagement disengagement is not equivalent to servo engagement disengage ment Use the CWS Button to disengage the pitch and roll servos while the autopilot remains active When the AP Key is pressed the autopilot and flight director ifnot already engaged are activated Engagement is indicated by a green AP annunciation in the center of the AFCS Status Box The flight director engages in Pitch and Roll Hold modes when initially activated Autopilot Engaged a ROL TAP TEE Figure 6 26 Autopilot Engaged 190 00384 09 Rev A Control Wheel Steering During autopilot operation the aircraft may be hand flown without disengaging the autopilot Pressing and holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the aircraft to be hand flown At the same time the flight director is synchronized to the aircraft attitude during the
116. able when the Synthetic Vision System is installed TAWS will take precedence over TERRAIN SVS when installed Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude S 100 ft Threshold 1000 ft SECTION 10 HAZARD AVOIDANCE Displaying Terrain on the TERRAIN SVS Page 1 Projected Flight Path Unlighted Obstacle Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TERRAIN SVS Page It desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Potential Impact Point Terrain more than 1000 ft below the aircraft altitude Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 11 SECTION 10 HAZARD AVOIDANCE 136 975 136 975 conz Figure 10 18 Terrain SVS Page 360 View 136 975 136 975 conz HOG UP GPS ALT na 368 BACK Figure 10 19 Terrain SVS Page ARC View Enable Disable Aviation Data 1 While the TERRAIN SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide
117. age Always use sound pilot judgment The Cessna aircraft Pilot s Operating Handbook POH takes precedence over any conflicting guidance found in this section 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 9 SECTION 13 ANNUNCIATIONS amp ALERTS MFD amp PFD Message Advisories DATA LOST Pilot stored data was The pilot profile data was lost System reverts to detault pilot profile and lost Recheck settings settings The pilot may reconfigure the MFD amp PFD with preferred settings if desired XTALK ERROR A flight display The MFD and PFD are not communicating with each other The G1000 system crosstalk error has occurred should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The G1000 system MFD1 SERVICE MFD1 needs service should be serviced Return unit for repair MANIFEST PFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The G1000 system should MANIFEST MFD1 software be serviced mismatch communication halted PFD1 CONFIG PFD1 config error The PFD configuration settings do not match backup configuration memory The Contig service req d G1000 system should be serviced MFD1 CONFIG MFD1 contig error The MFD configuration settings do not match backup configuration memory The Contig service req d G1000 system should be servic
118. al speed and Garmin G1000 Cockpit Reference Guide for the Cessna Nav III deviation guidance Approach waypoint altitude constraints are automatically designated when the approach is loaded These altitudes are also displayed as light blue text Waypoint altitude constraints are designated up to but not including the FAF The FAF is always a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this case the FAF altitude can be designated manually Altitudes that have been designated for use in vertical guidance may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude To help interpret the meanings of how the altitudes are presented keep the following points in mind e When the altitude is displayed in light blue the system is using that altitude designated to determine vertical speed and deviation guidance e When the altitude is displayed in white it is not being used by the system non designated to determine the vertical speed and deviation guidance e Analtitude displayed as small text is an altitude that is published in the navigation database e Altitudes displayed as a light blue subdued text cannot be used in the current vertical navigation calcul
119. also accompanied by a flashing CAUTION Softkey annunciation as shown in Figure 13 3 Pressing the CAUTION Softkey acknowledges the presence of the caution alert e MESSAGE ADVISORY This level of alert provides general information to the pilot A message advisory alert does not issue annunciations in the Annunciation Window Instead message advisory alerts only issue a flashing ADVISORY Softkey annunciation as shown in Figure 13 4 Pressing the ADVISORY Softkey acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts Window 13 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 13 ANNUNCIATIONS amp ALERTS 13 2 NAV III AIRCRAFT ALERTS Safe Operating Annunciation T182 T206 and The following alerts are configured specifically for the 206 with Prop De Ice Only Cessna Nav III aircraft See the Cessna Pilots Operating Annunciation Window Text Audio Alert Handbook POH for information regarding pilot responses WARNING Alerts 172R 172S 1827 T1827 206H 133 CO GUARDIAN MESSAGES and T206H Alerts Window Message Comments Annunciation Window Text Audio Alert CO DET SRVC The carbon There is a problem within monoxide detector needs the CO Guardian that service requires services CO DET FAIL The carbon Loss of communication monoxide detector is inopera between the G1000 and tive the CO Guardian
120. ame 3 Turn the large FMS Knob to move the cursor to the next character field 190 00384 09 Rev A 5 6 1 8 SECTION 8 FLIGHT PLANNING Repeat steps 2 and 3 until the desired name is entered Press the ENT Key Press the ENT Key again to accept the new waypoint identifier The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Turn the FMS Knobs to enter the position coordinates or the radial and distance from the reference waypoint Press the FMS Knob to remove the flashing cursor Modify a User Waypoint 1 2 3 4 With the User Waypoint Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the desired field and turn the small FMS Knob to make changes Press the ENT Key to accept the changes Press the FMS Knob to remove the flashing cursor Delete a User Waypoint 1 2 Select the User Waypoint Information Page and press the MENU Key to display the User Waypoint Information Page Options or press the DELETE Softkey Turn the large FMS Knob to select Delete User Waypoint and press the ENT Key The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 8 FLIGHT PLANNING Create User Waypoints from
121. and MFD e Current Track Indicator e All Bearing Pointer Distances e Active Flight Plan distances bearings and ETE values Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 3 SECTION 12 ABNORMAL OPERATION Also while the G1000 is in DR Mode the autopilot will not couple to GPS and Terrain Proximity TERRAIN SVS and TAWS are disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 12 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 13 ANNUNCIATIONS amp ALERTS SECTION 13 ANNUNCIATIONS amp e Softkey Annunciation During certain alerts the ALERTS Softkey may appear as a flashing ALERTS annunciation to accompany an alert The ALERTS Softkey assumes a new label consistent with the alert level WARNING CAUTION or ADVISORY By pressing the softkey annunciation the pilot acknowledges awareness of the alert The softkey then returns to the previous ALERTS label If alerts are still present the ALERTS label is displayed in inverse video white background with black text The pilot can press the ALERTS Softkey a second time to view alert text messages NOTE The Cessna aircraft Pilot s Operating Handbook POH supersedes information found in this document The G1000 Alerting System conveys alerts to the pilot using a combina
122. apability is available on the Reversionary Mode display SECTION 12 ABNORMAL OPERATION Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display problem The Reversionary Mode is activated manually by pressing the red DISPLAY BACKUP Button on the bottom of the audio panel GMA 1347 Pressing the red DISPLAY BACKUP Button again deactivates Reversionary Mode NOTE The Cessna Pilot s Operating Handbook POH always takes precedence over the information found in this section MFD in Reversionary Mode Figure 12 1 G1000 Reversionary Mode Failed PFD 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 SECTION 12 ABNORMAL OPERATION 12 2 12 2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a dual display failure the emergency frequency 121 500 MHz automatically becomes the active frequency to the pilot through the pilot headset 12 3 UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the air craft experiences unusual attitudes
123. arget Altitude is shown as the Altitude Reference beside the ALTV annunciation At 50 ft from the VNAV Target Altitude the flight director automatically transitions from VNAV Target Altitude Capture to Altitude Hold Mode and tracks the level leg As Altitude Hold Mode becomes active the white ALT annunciation moves to the active pitch mode field and flashes green for ten seconds to indicate the automatic transition The flight director automatically arms Vertical Path Tracking allowing upcoming descent legs to be captured and subsequently tracked Altitude Reference In This Case Equal To VNAV Altitude Target GPS ALT VPTH Flash up to 10 sec Indicating Automatic Transition GPS VPTH Figure 6 14 VNAV Altitude Capture Changing the VNAV Target Altitude NOTE Pressing the CWS Button while in VNAV Target Altitude Capture Mode does not cancel the mode Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC FLIGHT CONTROL 6 14 Changing the current VNAV Target Altitude while VNAV Target Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode Vertical Path Tracking and the appropriate altitude capture mode are armed in preparation to capture the new VNAV Target Altitude or the Selected Altitude depending on which altitude is to be intercepted first VNAV target altitudes can be changed while editing the active flight plan see the Navigation section
124. ated receiver audio COMI or COM2 also becomes selected when the COM MIC Key is pressed To prevent deselecting the desired received audio when pressing another COM MIC Key press the already selected COMI or COM2 Key before pressing the other COM MIC Key Figure 5 2 Transceivers 5 2 CABIN SPEAKER Pressing the SPKR Key selects and deselects the cabin speaker All of the radios can be heard over the cabin speaker Speaker audio is muted when the PTT is pressed Certain aural alerts and warnings autopilot traffic altitude are always heard on the speaker even when the speaker is not selected Figure 5 3 Passenger Address and Speaker Keys 5 3 PASSENGER ADDRESS PA SYSTEM T 182T AND T 206H ONLY A passenger address system is available for delivering voice messages over the cabin speaker When the PA Key is selected on the Audio Panel the COM MIC Annunciator is extinguished and the active COM frequency changes to white indicating that there isno COM selected A Push to Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Talk PTT must be pressed to deliver PA announcements The PA Annunciator flashes about once per second while the PTT is depressed 5 4 MARKER BEACON RECEIVER The marker beacon receiver is always on Only the marker beacon audio can be turned off Figure 5 4 shows the marker beacon annunciators on the PFD When the MKR MUTE Key is pressed the key an nunciator is lit and the audio to
125. ations Refer to Figure 1 8 and Table 1 1 for more detail regarding the significance of text size and color 190 00384 09 Rev A SECTION 1 SYSTEM OVERVIEW Whiteext Light Blue Tet Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance Small Text Altitude is not designated to be used in determining vertical speed and deviation guidance Altitude has been retrieved from the navigation database and is provided as a reference Altitude has been entered by the The system cannot use this altitude pilot Altitude is designated for in determining vertical speed and use in giving vertical speed and deviation guidance deviation guidance Altitude does not match the published altitude in navigation database or no published altitude exists Altitude is designated for use in The system cannot use this altitude giving vertical speed and deviation in determining vertical speed and guidance Altitude has been deviation guidance retrieved trom the navigation database or has been entered by the pilot and matches a published altitude in the navigation database Table 1 1 VNV Altitude Text Size and Color ACTIVE FLIGHT PLAN KIXD KDFW KARLA AMMA large White COVIE 221 9 0Nn 124007 oo LE
126. aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as a
127. ays are displayed in green along the localizer and glide slope VOR LOC BC and ADF approach segments that are approved to be flown using GPS are displayed in magenta boxes Segments that are flown using other than GPS or ILS such as heading legs or VOR final approach courses are not displayed Non programmed descents NOT displayed by pathway OD Programmed descent displayed by pathway whichever is higher 2 Je Figure 11 4 SVS Pathways Enroute and Descent Tid Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Missed Approach Upon activating the missed approach pathways lead to the Missed Approach Holding Point MAHP and are displayed as a level path at the published altitude for the MAHP or the selected altitude whichever is the highest If the initial missed approach leg is a Course to Altitude CA leg the pathways boxes will be displayed level at the altitude published for the MAHP If the initial missed approach leg is defined by a course using other than GPS pathways are not displayed for that segment FAF NAP Climbs NOT displayed SECTION 11 ADDITIONAL FEATURES Pathways are displayed along each segment including the path required to track course reversals that are part of a procedure such as holding patterns Pathways boxes will not indicate a turn to a MAHP unless a defined geographical waypoint exists between the MAP and MAHP Descent displaye
128. b to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 displays the active flight plan If the active flight plan is selected REM is an available option to display planning data for the remainder of the flight plan NOTE The Page Mode must be set to MANUAL to perform the following steps 5 Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time 6 Turn the FMS Knobs to enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings SECTION 8 FLIGHT PLANNING Turn the FMS Knobs to enter the fuel flow Press the ENT Key when finished Note that in automatic page mode fuel flow is provided by the system The flashing cursor moves to the fuel on board field Turn the FMS Knobs to modify the fuel on board Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made in GAL REM on the EIS System Page The flashing cursor moves to the calibrated airspeed field Turn the FMS Knobs to enter a calibrated airspeed Press the ENT Key when finished 10 The flashing cursor moves to the indicated altitude field Turn the FMS Knobs to enter ind
129. cal deviation and vertical speed required appears on the PFD in magenta Figure 6 11 Vertical Path Tracking Armed Altitude Hold Flashing Indicates Acknowledg Mode Active ment Required TOD within Selected VNV Target Altitude Below Altitude VNV Target Za Vertical Deviation Indicator Required Vertical Speed Bug GPS is Terminal Selected Phase Navigation of Flight Source Figure 6 11 Vertical Path Capture 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 11 SECTION 6 AUTOMATIC FLIGHT CONTROL When a descent leg is captured Figure 6 12 Vertical e Cannot be computed for a leg type such as a hold Path Tracking becomes active and tracks the descent pro or procedure turn file An altitude capture mode ALTS or ALTV is armed as appropriate Vertical Path VNV Target Altitude Tracking Active Capture Armed VNV Target Altitude Required Vertical Speed Indication Command Bars Indicate Descent to kaci o Maintain Required Vertical Speed Navigation Flight Source Vertical Deviation Indicator Figure 6 12 Vertical Path Tracking Mode Automatic Pitch Hold Reversion Several situations can occur while Vertical Path The following circumstances cause mode reversion Tracking Mode is active which cause the flight director to without arming Vertical Path Tracking Mode revert to Pitch Hold Mode Vertical Path Tracking and the appropriate altitude capture modes are armed for p
130. ch engages the flight director in a wings level 7 pitch up attitude allowing the execution of a missed approach or a go around This mode is a coupled pitch and roll mode and is annunciated as GA in both the pitch and roll active mode fields Go Around Mode disengages the autopilot and arms Altitude Hold Mode automatically Subsequent autopilot engagement is allowed Attempts to modify the aircraft attitude i e with the CWS Button or NOSE UP NOSE DN keys result in reversion to Pitch and Roll Hold modes Go Around Mode Active Autopilot Disconnect Annunciation Flashes Yellow 5 sec Command Bars Indicate Climb Figure 6 19 Go Around Mode 6 16 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Roll Modes e Roll Hold default mode Holds the current aircraft roll attitude or rolls the wings level depending on the commanded bank angle Heading Select Captures and tracks the Selected Heading e Navigation GPS VOR LOC Captures and tracks the selected navigation source e Backcourse Captures and tracks a localizer signal for backcourse approaches Approach GPS VAPP LOC Captures and tracks the selected navigation source with greater sensitivity for approach e Go Around Commands a constant pitch angle and wings level while in the air The following table relates each roll mode to its respective control and annunciation Refer to the pitch modes section for in
131. ct the desired airport 5 Press the ENT Key The cursor is now displayed on ACTIVATE 6 Press the ENT Key again to activate a Direct to Cancelling Direct to Navigation 1 Press the Direct to E8 Key 2 Press the MENU Key to display the Options Window The cursor flashes on Cancel Direct to NAV 3 Press the ENT Key to cancel the direct to 190 00384 09 Rev A SECTION 7 NAVIGATION 7 3 NAVIGATING AN EXAMPLE FLIGHT PLAN A NOTE The following example flight plan is for instructional purposes only All database information depicted should be considered not current The following discussion is an example of navigating a flight plan with the WAAS capable GPS system while the G1000 provides vertical guidance through descents A lateral flight plan LNAV would be navigated in much the same way but would not include vertical guidance when the final approach course is active The example is a flight plan from KMKC to KCOS filed using the TIFTO2 departure various Victor Airways and the DBRY1 arrival with the transition at TBE Enroute altitude will be 12 000 feet An LPV WAAS approach will be selected for runway 35R A missed approach will be executed at the Missed Approach Point MAP A few enroute changes are demonstrated A NOTE If the loaded arrival procedure has published altitudes contained in the navigation database these are for turbojet aircraft only Accept or change these values as desired to
132. d by pathway Selected Altitude or Programmed Altitude whichever is higher oon 1 Turn Segment NOT displayed by pathway Figure 11 5 SVS Pathways Approach Missed Approach and Holding 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 11 ADDITIONAL FEATURES 11 6 Flight Path Marker The Flight Path Marker FPM also known asa Velocity Vector is displayed on the PFD at groundspeeds above 30 knots The FPM depicts the approximate projected path of the aircraft accounting for wind speed and direction relative to the three dimensional terrain display The FPM is always available when the Synthetic Terrain feature is in operation The FPM represents the direction of the flight path as it relates to the terrain and obstacles on the display while the airplane symbol represents the aircraft heading The FPM works in conjunction with the Pathways feature to assist the pilot in maintaining desired altitudes and direction when navigating a flight plan When on course and altitude the FPM is aligned inside the pathway boxes as shown Figure 11 6 Flight Path Wind Marker Vector FPM 5 BBR come 5 888 com wan 108 00 117 95 136 975 waa TAEMA 117 95 136 975 11 11 pii HE Figure 11 6 Flight Path Marker and Pathways Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Zero Pitch Lin
133. d range indicates propeller overspeed warning a white high rpm range indicates above normal operating speeds Models 172S 206 and T206 G Oil Pressure OIL PSI Displays pressure of the oil supplied to the engine in pounds per square inch psi Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3 7 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 8 61 8 59 6 PM i Ha 1980 RPM pj 4 3004 50 0 100 ENG 0085 3 HRS VAC ae FUEL CALC 4 0 4 8 OIL F 210 QIL F 210 58 2 210 ENG HHY 7 HRS FUEL CALC FUEL FFLOW GPH 10 0 4 6 VAC ee FUEL CaLtC FFLOW GPH 12 0 GAL USED 1 1 GAL REM 87 FUEL TY GAL GAL USED A 2 4 6 weet we OOO OO GAL REM FUEL QTY E a A 16 ra F FUEL QTY gap BERF A 16 Pa F FUEL QTY GAL OLD OOOO OLD OOOO en me aaa hea _ELECTRICAL _ELECTRICAL ea E H BUS E H BUS E OE O O MZEE MH BATT S M BATT S M BATT 5 M BATT 5 2 CO O ON Model 172R Model 172S Model 182T Model 206H Figure 3 5 System Display Normally aspirated Aircraft Oil Temperature OIL F Displays the engine T Fuel Flow FFLOW GPH Shows the current oil temperature in degrees Fahrenheit F fuel flow in gallons per hour gph G Engine Hours Tach ENG HRS Models 182 Calculated Fuel Used GAL USED Shows T182 206 T206 A numeric readout gives the quan
134. disabled until the temperature returns to normal information for performing engine leaning 3 6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A The ASSIST Softkey aids in the leaning process by identifying the peak of the first cylinder whose temperature falls If the temperature of the peaked cylinder exceeds the peak value the peak value is not updated Press the ASSIST Softkey to stop peak monitoring Normally aspirated Aircraft For normally aspirated aircraft when a cylinder peaks its peak is represented by a hollow block on the EGT Bar Graph The EGT readout for the peaked cylinder indicat ed on the bar graph in light blue appears directly beneath the bar graph The system automatically switches to the first peak obtained and displays the temperature deviation from peak APEAK in degrees Fahrenheit F below the EGT readout Turbocharged Aircraft Leaning for turbocharged aircraft is done with reter ence to the Turbine Inlet Temperature TIT When the temperature peaks the numeric readout APEAK appears below the TIT Indicator and displays the difference be tween peak and current TITs in degrees Fahrenheit F If a peak is not displayed underscores are shown until one is established 3 3 SYSTEM DISPLAY NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset NOTE The pilot should refer to the Pil
135. e ry Pressing the BACK Softkey returns to the Chart Selection Softkeys Figure 11 16 ChartView Softkeys Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 11 SECTION 11 ADDITIONAL 11 12 FEATURES If a chart is available for the destination airport or the airport selected in the active flight plan the chart appears on the screen When no flight plan is active or when not flying to a direct to destination pressing the SHW CHRT Softkey displays the chart for the nearest airport if available When no terminal procedure chart is available for the nearest airport or the selected airport the banner CHART NOT AVAILABLE appears on the screen The CHART NOT AVAILABLE banner does not refer to the Jeppesen subscription but rather the availability of a particular airport chart selection or procedure for a selected airport If there is a problem in rendering the data such as a data error or a failure of an individual chart the banner UNABLE TO DISPLAY CHART is then displayed Chart Options Pressing the CHRT OPT Softkey displays the next level of softkeys the chart options level Pressing the FULL SCN Softkey displays the chart using the full width of the screen Pressing the ALL Softkey shows the full approach chart on the screen PLAN PROFILE MINIMUMS FIT WOTH Figure 11 17 Approach Information Page ALL View Garmin G1000 Cockpit Reference Guide for the
136. e The Zero Pitch Line is drawn completely across the display and represents the aircraft attitude with respect to the horizon It may not align with the terrain horizon particularly when the terrain is mountainous or when the aircraft is flown at high altitudes Horizon Heading The Horizon Heading is synchronized with the HSI and shows approximately 60 degrees of compass heading in 30 degree increments on the Zero Pitch Line Horizon Heading tick marks and digits appearing on the zero pitch line are not visible behind either the airspeed or altitude display Horizon Heading is used for general heading awareness and is activated and deactivated by pressing the HRZN HDG Softkey Traffic Tratfic symbols are displayed in their approximate locations as determined by the related traffic systems Figure 11 7 Traffic symbols are displayed in three dimensions appearing larger as they are getting closer and smaller when they are further away Traffic symbols and coloring are consistent with that used for traffic displayed in the Inset map or MFD traffic page If the traffic altitude is unknown the traffic will not be displayed on the SVS display For more details refer to the traffic system discussion in the Hazard Avoidance section 190 00384 09 Rev A SECTION 11 ADDITIONAL FEATURES Airport Signs Runways Airport Signs provide a visual representation of eae te pas a asa Gc WARNING Do not use SVS runway depiction as the so
137. e City Forecast e Surface Analysis e Freezing Levels 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 5 SECTION 10 HAZARD AVOIDANCE 10 6 e Winds Aloft e County Warnings e Cyclone Warnings Np w Figure 10 10 Weather Product Symbols The XM Information Page in the AUX Page Group displays the weather products available for the current subscription A green box by the weather product means that it is available From within the AUX XM INFORMATION Page the pilot may switch to the AUX XM RADIO Page by pressing the RADIO Softkey Alternatively the pilot may switch to the AUX XM INFORMATION Page from the AUX XM RADIO Page by pressing the INFO Softkey NOTE The LOCK Softkey on the AUX XM INFORMATION Page is used to save the GDL 69 A activation data when the XM services are initially set up It is not used during normal operation of the GDL 69 A but it should have no adverse effects if inadvertently selected during flight Refer to the GDL 69 69A XM Satellite Radio Activation Instructions 190 00355 04 Rev E or later for further information Weather Product Age The age for each of the enabled products is displayed on the right side of the display Times are based on GMT time when the data was assembled on the ground not the time the data was received by the XM receiver When the age of a weather product has exceeded half of the expiration time the product time change
138. e Push the AP DISC Switch at the decision height and land the aircraft e Use the GA Switch to execute a missed approach SECTION 6 AUTOMATIC FLIGHT CONTROL KCOS apo SD IddV 207 PETEY N PON AVN Sd9 Figure 6 37 ILS Approach to KCOS 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC FLIGHT CONTROL 6 32 Flying a RNAV GPS approach with vertical guidance 1 Arm flight director modes for a RNAV GPS approach with vertical guidance a Make sure the navigation source is set to GPS use CDI Softkey to change navigation source b Select the Runway 35R LPV approach for KCOS Load and activate the approach into the flight plan 2 Press the APR Key once clearance for approach has been received GPS Approach Mode is activated and Glidepath Mode is armed Se GPS AP ALTS GP 3 Once the glidepath is captured Glidepath Mode becomes active The flight director now provides guidance to the missed approach point 4 There are two options available at this point as the autopilot flies the approach e Push the AP DISC Switch at the Decision height and land the aircraft e Use the GA Switch to execute a missed approach KCOS SPO d9 lddV Sd9 SPOIN AVN Sd Figure 6 38 LPV Approach to KCOS Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Go Around Missed Approach NOTE As a result of calculations
139. e TERRAIN Warning Obstacle Obstacle Warning ROC Imminent Obstacle Impact Warning l0 TERRAIN Warning Obstacle Obstacle Reduced Required Terrain Clearance Caution RTC Imminent Terrain Impact Caution ITI O Caution Terrain Terrain Caution Terrain Terrain Reduced Required Obstacle Clearance Caution Obstacle Obstacle Caution ROC mm D Imminent Obstacle Impact Caution IOI a Caution Obstacle Obstacle Table 10 1 TERRAIN SVS Alerts Summary PFD MEFD Alert Alert Type Aural Message System Test Pass Terrain System Test OK Terrain System Test Fail TER FAIL Terrain System Failure Table 10 2 TERRAIN SVS System Test Status Annunciations 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 13 SECTION 10 HAZARD AVOIDANCE Alert Annunciation 136 975 118 009 com HAP NAVIGATI N HAP 136 975 118 688 coz 136 975 118 000 conz NORTH UP TERRAIN ALERT CAUTION TERRAIN Press ENT TERRADN SV6 PAGE Press DLA PREVIOUS PAGE Mi TERRADN SS PAGE previdis to l INHIBIT TERRATH 545 ALT UNIT SID BARO BACK Figure 10 21 TERRAIN SVS Alert Annunciations Abert i 136 975 1 18 000 conz HORTH UP Terrain Display Enabled TERRAIM 100F0 jp Terrain Legend 10000r1 Alert Annunciation Figure 10 22 Navigation Map Page After TERRAIN SVS Pop up Alert Acknowledgment 10 14 Garmin G1000 Cockpi
140. e WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes NORTH UP Se PUBLIC M ee OLIS ST PAUL INTL MINNEAPOLIS MN INNEAPOLIS MN METAR Text GER eT B a ERATURE DS DEW POINT 14 c ALTIMETER 29 721N LIDAF PT KHSP 2619452 2018 23011KT PESH _ TAF Text WX Softkey Figure 10 8 METAR and TAF Text Displayed on the Airport Weather Information Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 10 HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the fourth rectangular page icon Press the available softkeys to select the desired XM weather product Press the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map t SNOW y q ar TvIn 7 0 Gee TAD cr c ICELL MOV SIG AIR METAR LEGEND HORE HX Figure 10 9 Weather Data Link Page NEXRAD Press the NEXRAD Softkey to show 10 4 NEXRAD weather and radar coverage information Areas where radar coverage is not available are shown in grayish purple The display is updated every five minutes Garmin G1000 Cockpit Reference Guide for the Cessna Nav III NEXRAD Limita
141. e does not cancel the mode The autopilot guides the aircraft back to the descent path upon release of the CWS Button NOTE VNAV flight director pitch modes are available only in conjunction with GPS roll modes A NOTE The Selected Altitude takes precedence over any other vertical constraints Vertical Navigation VNAV flight control is available for enroute terminal cruise and descent operations when VNAV has been enabled and a VNAV flight plan with at least one vertical waypoint or direct to with a vertical constraint has been activated Refer to the Navigation section for more information on VNAV flight plans The flight director may be armed for VNAV at any time but no target altitudes are captured during a climb The Command Bars provide vertical profile guidance based on specified altitudes entered manually or loaded from the database at waypoints in the active flight plan or vertical direct to The appropriate VNAV flight control modes are sequenced by the flight director to follow the path defined by the vertical profile Upon reaching the last waypoint in the VNAV flight plan the flight director transitions to Altitude Hold Mode and cancels any armed VNAV modes Vertical Path Tracking Mode VPTH NOTE If another pitch mode key is pressed while Vertical Path Tracking Mode is selected Vertical Path Tracking Mode reverts to armed Garmin G1000 Cockpit Reference Guide for the Cessna Nav III When a vertical profile
142. e location Therefore the exact location of the strike is not displayed 190 00384 09 Rev A CELL MOV Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow pointing in the direction of predicted movement The display is updated every 12 minutes SIG AIR Pressing the SIG AIR Softkey shows SIGMET and AIRMET information The display is updated every 12 minutes METAR Press the METAR Softkey to graphically display METARs METARS are shown as colored flags at airports providing METAR reports The display is updated every 12 minutes MORE WX Press the MORE WX Softkey to display the following group of softkeys for additional weather control SFC Pressing the SFC Softkey for Surface Analysis shows current or forecast conditions Forecasts are available for intervals of Current 12 24 36 and 48 hours Press the softkey corresponding to the desired forecast The closest city forecast information is displayed in the legend The display is updated every 12 minutes FRZ LVL Press the FRZ LVL Softkey to display contour lines for freezing levels The display is updated every 12 minutes WIND Press the WIND Softkey to show wind speed and direction at a selected altitude from the ground up to 42 000 feet in 3 000 foot increments After pressing the WIND Softkey press the softkey corresponding to the desired winds aloft altitude The display is updated every 12 minutes COUNTY Pressing the COUNTY
143. e message text If the CLR Key is pressed again the message is restored 5 Press the ENT Key while the message line is cleared to clear the message time 6 Turn the small FMS Knob to select the message alert type e Event Message issued at the specified date time e One time Message issued when the mes sage timer reaches zero default setting e Periodic Message issued each time the message timer reaches zero 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 19 SECTION 11 ADDITIONAL FEATURES Accessing and navigating checklists 11 7 ELECTRONIC CHECKLISTS 1 O NOTE The checklists presented here are for example only and may not reflect checklists actu 2 ally available for the Cessna NAV III Aircraft This material is not intended to replace the checklist 3 information presented in the AFM or the Pilot Safety and Warning Supplements document NOTE Garmin is not responsible for the content of checklists Cessna NAV III Aircraft checklists 5 are created modified and updated by the aircraft manufacturer The optional checklist functions are displayed on two levels of softkeys that are available on any MFD page The MFD is able to display optional electronic checklists which allow a pilot to quickly find the proper procedure on the ground and during each phase of flight The G1000 accesses the checklists from an SD card inserted into the bezel slot If the S
144. e minimums can be set in the Timer Reterences Window The altitude ranges from 0 to 16 000 feet in 10 foot increments The minimums are reset anytime the power is cycled MINIMUMS 4BARO 1560FT Figure 2 16 Barometric Minimum Descent Altitude Settings The desired barometric minimum descent altitude MDA DA DH can be set in the Timer References Window Visual annunciations alert the pilot when approaching the MDA e When the aircraft altitude descends to within 2500 feet of the MDA setting the Barometric Minimum Box appears with the altitude in light blue text The bug appears on the tape in light blue once in range e When the aircraft passes through 100 feet of the MDA the bug and text turn white e Once the aircraft descends past the MDA the bug and text turn yellow and the aural alert Minimums Minimums is generated Alerting is inhibited while the aircraft is on the ground If the aircraft climbs after having reached the MDA once it reaches 50 feet above the MDA alerting is disabled Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 SECTION 2 FLIGHT INSTRUMENTS Within 2500 ft 21 ral i 0 4 Within 100 ft HSI FRMT Softkey followed by the 360 HSI or the ARC HSI Softkey 2 8 Barometric Minimum Bug lt 2000 Barometric ee BARO MIN Minimum Box 2240 CEUV OMA 2100 Altitude Reached 1980 1800 L 17AA BARO MIN Figure 2 17 Barometr
145. ean Display 00 0 0 3 4 Normally aspirated Aircratt c ssssssssessessecssesssesssen 3 7 Turbocharged Aircraft sccuussicnscss recuse ineredewenlaudcaral 3 7 3 3 System Display 3 7 190 00384 09 Rev A TABLE OF CONTENTS SECTION 4 NAV COM AND TRANSPONDER 4 1 4 1 Radio Status IndicationS 0 cccccseen 4 3 42 Volume sinuain a 4 3 4 3 Automatic Squelch cee 4 3 4 4 Quickly Activating 121 500 MHz 00 0 0 4 3 4 5 Optional NAV Radios 0 0 cceseeeen 4 3 DME Radio OPTOMA siicsssnnvedsixatonneroreistxttevsiacontion 4 3 ADF Radio optional sisin dishasesiclaprasvetuinseichasaamntaneeene 4 4 4 6 Frequency Auto tuning ccceeen 4 4 Auto TUNING onne Pr Deiana 4 4 Autotuning onthe MFD isstcvessexesiossuanentanecisnanxanenioine 4 4 4 7 Transponder 4 4 Mode SOIC CON aano 4 4 aE SEE 0 E E EE tor 4 5 Code selection esan a S 4 5 FIIGNEIDE REDOING nenna 4 6 SECTION 5 AUDIO PANEL 00000 5 1 5 1 COM Radio Selection 5 2 5 2 Cabin Speaker ou cesses 5 2 5 3 Passenger Address PA System T 182T and T 206H Only 5 2 5 4 Marker Beacon Receiver ccccccceeeeen 5 2 Marker Beacon Signal Sensitivity 5 2 5 5 Nav Radio Audio Selection cccccee 5 3 5 6 Intercom System ICS Isolation 5 3 5 7 Intercom Squelch Control 0 cccces 5 4 5 8 Digital Clearance Recorder and Player 5 4 SECTION 6 A
146. ect MSL or AGL 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III fl SECTION 7 NAVIGATION 9 Press the ENT Key The cursor is placed in the VNV offset distance field 10 Enter the desired target altitude offset trom the selected Direct to 11 Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the COURSE field 12 Enter the desired course to the waypoint 13 Press the ENT Key to highlight ACTIVATE 14 Press the ENT Key again to activate the Direct to Select a Direct to Destination to a Flight Plan Waypoint 1 While navigating an active flight plan press the Direct to ES Key 2 Turn the small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7 3 DIRECT To IDENT FACILITY CITY KELN H CEN USA A NORTH UP Figure 7 3 Flight Plan Waypoint List MFD 3 Turn the large FMS Knob to select the desired waypoint 4 Press the ENT Key The cursor is now displayed on ACTIVATE 5 Press the ENT Key again to activate a Direct to Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Select a Direct to Destination to a Nearest Airport 1 Press the Direct to E Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 3 The list is populated only when navigating a flight plan DIRECT TO IDENT FACILITY C
147. ector is in Pitch Hold Vertical Speed Flight Level Change or Go Around Mode This mode is also armed automatically under Vertical Path Tracking Mode when the Selected Altitude is to be captured instead of the VNAV Target Altitude The white ALTS annunciation indicates Selected Altitude Capture Mode is armed see Figure 6 5 for example The ALT Knob is used to set the Selected Altitude shown above the Altimeter As the aircraft nears the Selected Altitude the flight director automatically transitions to Selected Altitude Capture Mode with Altitude Hold Mode armed Figure 6 7 This automatic transition is indicated by the green ALTS annunciation flashing for up to ten seconds and the appearance of the white ALT annunciation The Selected Altitude is shown as the Altitude Reference beside the ALTS annunciation At 50 ft from the Selected Altitude the flight director automatically transitions from Selected Altitude Capture to Altitude Hold Mode and holds the Selected Altitude shown as the Altitude Reference As Altitude Hold Mode becomes active the white ALT annunciation moves to the active pitch mode field and flashes green for ten seconds to indicate the automatic transition Altitude Reference in this case equal to Selected Altitude J GPS LAP ALT Flash up to 10 sec Indicating Automatic Transition Figure 6 6 Automatic Mode Transitions During Altitude Capture Changing the Selected Altitude Garmin G
148. ectors to Final is activated e Navigation source is manually switched e Localizer signal is not captured by the final approach fix FAF Changing the Selected Course The Selected Course on the PFD is controlled using the CRS Knob Pressing the CWS Button and hand ilying the aircraft does not change the Selected Course while in Approach Mode The autopilot guides the aircraft back to the Selected Course or GPS flight plan when the CWS Button is released 190 00384 09 Rev A Backcourse Mode BC NOTE When making a backcourse approach set the Selected Course to the localizer front course Backcourse Mode captures and tracks a localizer signal The mode may be selected by pressing the BC Key Backcourse Mode is armed if the CDI is greater than one dot when the mode is selected The flight director creates steering commands from the Selected Course and deviation when in Backcourse Mode Backcourse Mode Active SECTION 6 AUTOMATIC FLIGHT CONTROL Changing the Selected Course The Selected Course on the PFD is controlled using the CRS Knob Pressing the CWS Button and hand ilying the aircraft does not change course while in Backcourse Mode The autopilot guides the aircraft back to the Selected Course when the CWS Button is released Pitch Hold Mode Active LOC2 is Selected Navigation Source Command Bars Hold Pitch Attitude Figure 6 25 Backcourse Mode 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide fo
149. ed SW MISMATCH GDU software The MFD and PFD have different software versions installed The G1000 system version mismatch Xtalk is off should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by MFD1 COOLING MFD1 has poor dimming the display If problem persists the G1000 system should be serviced cooling Reducing power usage PFD1 KEYSTK PFD1 key name Key A key is stuck on the PFD and or MFD bezel Attempt to tree the stuck key by is stuck ae pressing it several times The G1000 system should be serviced if the problem MFD1 KEYSTK MFD key name Key persists is stuck CNFG MODULE PFD1 configuration The PFD1 configuration module backup memory has failed The G1000 system module is inoperative should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage sini no SDE een The MFD voltage is low The G1000 system should be serviced voltage Reducing power usage 13 10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A The PFD1 voltage is low The G1000 system should be serviced SECTION 13 ANNUNCIATIONS amp ALERTS Database Message Advisories MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basema
150. eference Guide for the Cessna Nav III 190 00384 09 Rev A PFD and MFD controls function the same NAV VOL ID Knob Controls the NAV audio level Press to turn the Morse code identifier ON and OFF Volume level is shown in the field as a percentage NAV Frequency Transfer Key Transfers the standby and active NAV frequencies Dual NAV Knob Tunes the MHz large knob and kHz small knob standby frequencies for the NAV receiver Press to switch the tuning box light blue box between the NAVI and NAV2 fields Heading Knob Turn to manually select a heading on the HSI When pressed it synchronizes the heading bug with the compass lubber line Selected Heading provides the heading reference to the Flight Director while operating in Heading Select Mode G Joystick Changes the map range distance top to 190 00384 09 Rev A bottom of map display when rotated Activates the map pointer when pressed CRS BARO Knob The large knob sets the altimeter barometric pressure and the small knob adjusts the course The course is only adjustable when the HSI is in VORI VOR2 or OBS SUSP Mode Pressing this knob centers the CDI on the currently selected VOR Selected Course provides course reference to the Flight Director when operating in Navigation and Approach Modes Dual COM Knob Tunes the MHz large knob and kHz small knob standby frequencies for the COM transceiver Pressing this k
151. eld 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Traffic a a aircraft is 400 below trafic Uut o Traffic Mode A Mode climbing Range 136 975 118 688 cone Wou SEA NORMAL Non Bearing Traffic system Proximit Traffic is unable to determine bearing 1000 y rap l distance is 8 0 nm 1190 above descending and descending Figure 10 13 Traffic Map Page 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE Displaying Traffic on the Navigation Map 1 Ensure the KTA 870 system is operating With Traffic Advisory with directional information Points in the Navigation Map displayed press the MAP the direction of the intruder aircraft track Softkey Traffic Advisory without directional information 2 Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory out of the selected display range Displayed at outer range range ring at proper bearing a gt Non threat traffic with directional information Points E f in the direction of the aircraft track HR Non threat traffic with no directional information gt Traffic located on the ground with directional information Points in the direction of the aircraft Traffic Advisory track Ground traffic is only displayed when own aircraft is below 1 000 feet AGL or on the ground Ground tratfic without directional information Ground traffic is only displayed w
152. elow the preset barometric minimum descent altitude Aural Message Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic The Traffic Information Service TIS or ADS B traffic system has issued a Traffic Advisory alert Traffic not available The aircraft is outside the Traffic Information Service TIS or ADS B coverage area Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 13 ANNUNCIATIONS 13 7 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails a large red X is typically displayed on areas associated with the failed data Refer to the POH for additional information regarding pilot responses to these annunciations NOTE Upon power up of the G1000 system certain boxes remain invalid as G1000 equipment begins to initialize All boxes should be operational within one minute of power up Should any box continue to remain flagged the G1000 system should be serviced by a Garmin authorized repair facility System Annunciation Comment Attitude and Heading Reterence System is aligning Display system is not receiving attitude information trom the AHRS Indicates a contiguration module failure This annunciation is only seen when the autopilot is engaged The annunciation indicates an AHRS monitor has detected an abnormal flight parameter possibly caused by strong turbulence In this case the
153. em should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still GPS2 SERVICE GPS needs service be available The G1000 system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may stil NAV2 SERVICE NAV2 needs service be available The G1000 system should be serviced Return unit for repair NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck G S1 FAIL G S1 is inoperative The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 G S2 FAIL G S2 is inoperative system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver G S2 SERVICE G S2 needs service may still be available The G1000 system should be serviced when possible Return unit for repair GIA 63W Message Advisories GIA1 CONFIG GIA1 contig error Contig service req d The GIA1 and or GIA2 configuration sett
154. ement Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 23 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 24 6 5 EXAMPLE PROCEDURES NOTE The following example flight plan and diagrams not to be used for navigation in this section are for instructional purposes only and should be considered not current Numbered portions of accompanying diagrams correspond to numbered procedure steps This scenario based set of procedures based on the example flight plan found in the Flight Management Section shows various GFC 700 AFCS modes used during a flight In this scenario the aircraft departs Charles B Wheeler Downtown Airport KMKC enroute to Colorado Springs Airport KCOS After departure the aircraft climbs to 12 000 ft and airway V4 is intercepted following ATC vectors Airway V4 is flown to Salina VOR SLN using VOR navigation then airway V244 is flown using GPS Navigation The ILS approach for runway 35L and LPV WAAS approach for runway 35R are shown and a missed approach is executed KCOS V 244 Departure Climbing to the Selected Altitude and flying an assigned heading 1 Before takeoff set the Selected Altitude to 12 000 feet using the ALT Knob 2 After takeoff hand tly the aircraft to an altitude above the autopilot minimum engage height 3 In this example Vertical Speed Mode is used to capture the Selected Altitude Pitch Hold Vertical Speed or Fli
155. en full the indicator displays to 35 gallons per side 24 gallons for the Models 172R and 17285 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3 9 SECTION 3 ENGINE INDICATION SYSTEM EIS Blank Page 3 10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 4 NAV COM amp TRANSPONDER SECTION 4 NAV COM AND TRANSPONDER The NAV COM controls and frequency boxes share the same locations on the on the Primary Flight Display and the Multi Function Display NAV COM Controls NAV Frequency Box COM Frequency Box Controls tavi 115 88 nav2 116 68 PUSH 1 2 cul CRS 4 gt BARO J 9000 oA onA 8008 Se 6 eee E T A 3 5 one Hooe EE T PUSH FAN GR fe PRAGI WEB Pet ii fleas ete l De MENU FPL PROC AV2 XPOR OOOO ALT RILA 1346 21 IDENT THR REF NRST PUSH CRA Figure 4 1 G1000 VHF NAV COM Interface PFD shown peta 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 4 1 SECTION 4 NAV COM amp TRANSPONDER Standby NAV Selected NAV Selected COM Standby COM Frequency Field Frequency Frequency Frequency Field nav1 189 98 Gs 118 580 con nav2 114 60 110 60 ckv WPT VOR INFORMATION 118 400 121 400 conz Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Fre
156. eparture Turn either FMS Knob to select the desired runway and press the ENT Key A list of available transitions is displayed for the departure Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key SECTION 9 PROCEDURES DEPARTURE CHIEFS RUNWAY ALL TRANSITION CATTS Figure 9 2 Select Departure Transition 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active Load and Activate An Arrival Procedure 1 2 3 4 5 6 NOTE If any portion of an arrival procedure is the active leg of a flight plan the existing arrival procedure must be deleted before changing to a different arrival procedure Press the PROC Key Turn the large FMS Knob to highlight SELECT ARRIVAL Press the ENT Key If a flight plan is active the destination airport is displayed as the default A list of available arrivals is also displayed If no flight plan is active use the FMS Knobs to enter the identifier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Arrival field Turn the small FMS Knob to display a list of available arrivals Turn either FMS Knob to select the desired arrival and press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Nav III g SECTION 9 PROCEDURES 9 2 1 8 9 Figure 9 3 Select Arrival A second window is displayed listin
157. er frequency and selecting that Nav receiver on the CDI The G1000 GPS allows for flying LNAV LNAV VNAV WAAS only and LPV WAAS only approaches accord ing to the published chart The active appoach type is annunciated on the HSI as shown in the following table HSI DESCRIPTION ANNUNCIATION LNAV GPS approach using published LNAV minima LNAV V GPS approach using published LNAV minima Advisory vertical guidance is provided LNAV VNAV minima LPV minima WAAS systems only Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Load and or Activate an Approach Procedure 1 2 3 4 5 6 1 190 00384 09 Rev A Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key If a flight plan is active the destination airport is displayed as the default A list of available approaches is also displayed If no flight plan is active use the FMS Knobs to enter the identifier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Approach field Turn the small FMS Knob to display a list of available approaches ATRAORT PLELIC MIKETA SAN DOSE T U E APPROACM CHANNEL CHANNEL 30106 w Wizk APPRO ADH RNAV t2Rors LPY Figure 9 6 Selecting an Approach Procedure Turn either FMS Knob to highlight the desired approach Press the ENT Key The cursor moves to the TRANSITIONS field Turn the large FMS Kn
158. formation regarding Go Around and Takeoff Modes SECTION 6 AUTOMATIC FLIGHT CONTROL The CWS Button does not change lateral references for Heading Select Navigation Backcourse or Approach modes The autopilot guides the aircraft back to the Selected Heading Course upon release of the CWS Button Roll Hold Mode ROL NOTE If Roll Hold Mode is activated as a result of a mode reversion the flight director rolls the wings level When the flight director is activated the FD or AP Key is pressed Roll Hold Mode is selected by default This mode is annunciated as ROL in the AFCS Status Box The current aircraft bank angle is held subject to the bank angle conditions listed in Table 6 3 Roll Mode Roll Hold default Heading Select HDG Key EE 190 00384 09 Rev A Approach GPS Arm Capture Track Navigation GPS Arm Capture Track aviga VOR Enroute Arm Capture Track NAV Key Navigation LOC Arm Capture Track No Glideslope Backcourse Arm Capture Track BC Key Approach VOR Arm Capture Track Approach ILS Arm Capture Track Glideslope Mode automatically armed APR Key ME LOC Go Around in air GA Switch Table 6 2 Roll Modes Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC FLIGHT CONTROL EROL es EE eae Ae Figure 6 20 Roll Hold Mode Annunciation Bank Angle Flight Director Response Rolls wings level 6 18 6 to 22 Maintai
159. ft nears the Selected Altitude the flight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds ALT The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft Selected Altitude of 10 000 MSL ALT Mode Figure 6 34 FLC Descent 6 28 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL e Turn the ALT Knob to adjust the Selected Altitude e Press the VNV Key Vertical Path Tracking descent to VNV Target Altitude 1 Select VNV flight control 190 00384 09 Rev A a Press the VNV Key to arm Vertical Path Tracking Mode The white annunciation VPTH appears J GPS AP VPTH b Using the ALT Knob set the Selected Altitude at least 75 feet below the flight plan s VNV Target Altitude of 10 000 feet If the Selected Altitude is not adequately adjusted below the VNV Target Altitude the flight director commands descent to the Selected Altitude rather than the VNV Target Altitude once Vertical Path Tracking Mode becomes active ALTS is armed rather than ALTV c If Vertical Path Tracking Mode is armed more than 5 minutes prior to descent path capture acknowledgment is required for the flight director to transition from Altitude Hold to Vertical
160. fuel flow A white tick mark indicates the maximum cruise fuel flow Model T182T only 4 Oil Pressure Indicator OIL PRES Displays pressure of the oil supplied to the engine in pounds per square inch psi G Oil Temperature Indicator OIL TEMP Displays the engine oil temperature in degrees Fahrenheit F 6 Cylinder Head Temperature Indicator CHT Models 182T T1821 206H T206H Shows the head temperature of the hottest cylinder number shown in triangular pointer in degrees Fahrenheit F Garmin G1000 Cockpit Reference Guide for the Cessna Nav III RPM P 1990 2 TOH FFLOW GPH ae a 29 OIL PRES OIL TEMP EGT Lari WI VAC ha FUEL QTY GAL me 5 18 7A F ENG 000 2 HRS ELECTRICAL 0 0000 SECTION 3 ENGINE INDICATION SYSTEM EIS RAM 3000 a 2110 FFLOW GPH Vm i A rai OIL PRES OIL TEMP A EGT Li 1 Wi VAC ee FUEL TY GAL a H 18 7H F ENG 0400 0 HRS ELECTRICAL 0000 J RAM 2700 o 2020 FFLOW GPH A 27 OIL PRES OIL TEMP SS CHT _ EGT Lippi eI FUEL QTY Ko C A 5 16 76 36 F ELECTRICAL OFS FFLOW GPH ee A 30 OIL PRES OIL TEMP h CHT nA EGT UWr ia QTY GAL i 4 A 0 0000 6 10 20 3 F ELECTRICAL MH BUS M BUS E i weg M E
161. g a VOR Radial Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Flying a Flight Plan GPS Course A NOTE Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode wings rolled level As the aircraft closes on Salina VOR GPS is used to navigate the next leg airway V244 The aircraft is currently tracking inbound on Airway V4 Flying a GPS flight plan 1 Transition from VOR to GPS Navigation Mode a Press the CDI Softkey until GPS is the selected navigation source b Press the NAV Key to activate GPS Navigation Mode The autopilot guides the aircraft along the active flight plan leg 2 Following the flight plan the autopilot continues to steer the aircraft under GPS guidance Note that in GPS Navigation Mode course changes defined by the flight plan are automatically made without pilot action required 27 Hays VOR HYS SL Figure 6 33 Transition to GPS Flight Plan 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 27 SECTION 6 AUTOMATIC FLIGHT CONTROL Descent While flying the arrival procedure the aircraft is cleared for descent in preparation for the approach to KCOS Three methods are presented for the descent from 12 000 ft e Flight Level Change descent Flight Level Change Mode can be used to descend to the Selected A
162. g available transitions for the arrival Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key Figure 9 4 Select Arrival Transition A third window is displayed listing the available runways Turn either FMS Knob to select the desired runway and press the ENT Key Figure 9 5 Select Arrival Runway With LOAD highlighted press the ENT Key If a flight plan is active the selected arrival procedure is inserted after the destination airport and becomes part of the active flight plan If no flight plan is active when the arrival is loaded the arrival procedure becomes the active flight plan 9 2 APPROACHES A NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Not all approaches in the database are approved for GPS use When selecting an approach a GPS designation to the right of the procedure name indicates the procedure can be flown using the GPS receiver Some procedures do not have this designation meaning the GPS receiver can be used for supplemental navigation guidance only If the GPS receiver cannot be used for primary guidance the ap propriate navigation receiver must be used for the selected approach e g VOR or ILS The final course segment of ILS approaches for example must be flown by tuning the Nav receiver to the prop
163. g the softkeys located along the bottom edge of the display Pressing the softkeys turns the related function on or off When SVS is enabled the pitch ladder increments are reduced to 10 degrees up and 7 5 degrees down SVS functions are displayed on three levels of softkeys The PFD Softkey leads into the PFD function Softkeys including synthetic vision Pressing the SYN VIS Softkey displays the SVS feature softkeys The softkeys are labeled PATHWAY SYN TERR HRZN HDG and APTSIGNS The BACK Softkey returns to the previous level of Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 1 SECTION 11 ADDITIONAL FEATURES softkeys Synthetic Terrain must be active before any other SVS feature may be activated HRZN HDG APTSIGNS and PATHWAY Softkeys are only available when the SYN TERR Softkey is activated gray with black characters After activating the SYN TERR Soitkey the HRZN HDG APTSIGNS and PATHWAY softkeys may be activated in any combination to display desired features When system power is cycled the last selected state on or off of the SYN TERR HRZN HDG APTSIGNS and PATHWAY soitkeys is remembered by the system Activating and deactivating SVS 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey The SVS display will cycle on or off with the SYN TERR Softkey Activating and deactivating Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3
164. ght Level Change Mode may be used a Press the VS Key to activate Vertical Speed Mode ROL TEE The Vertical Speed Reference may be adjusted after Vertical Soeed Mode is selected using the NOSE UP NOSE DN keys or pushing the CWS Button while hand flying the aircraft to establish a new Vertical Speed Reference b Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode a ROL TAP ALTS 0 Topeka VOR TOP O Salina VOR SLN Figure 6 30 Flight Plan Overview Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A KMKC 4 Use the HDG Knob to set the Selected Heading complying with ATC vectors to intercept Airway V4 SECTION 6 AUTOMATIC FLIGHT CONTROL At 50 feet from the Selected Altitude the green ALT annunciation flashes for up to 10 seconds the autopilot transitions to Altitude Hold Mode and levels the aircraft Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading _ HDG AP ALTS 5 As the aircraft nears the Selected Altitude the flight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds n HDG TAP ALT 4p G Mou Selected Altitude of 12 000 MSL ALT Mode ys mor
165. h wf aT Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the last rectangular page icon 3 If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display Figure 10 17 Terrain Proximity Page Color Indication Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Height is less than Height is less than Height is greater than Height is greater than 1000 AGL 1000 AGL 1000 AGL 1000 AGL Figure 10 16 Obstacle Symbols 10 10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Displaying Terrain and Obstacles on the Navigation Map 1 2 10 6 190 00384 09 Rev A Terrain Obstacle Location With the Navigation Map displayed press the MAP Softkey Press the TERRAIN Softkey Terrain and obstacle proximity is now displayed on the map TERRAIN SVS DISPLAY OPTIONAL NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TERRAIN SVS operation is only avail
166. he ALT field in Figure 7 48 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 19 SECTION 7 NAVIGATION 24 After crossing CEGIX the aircraft continues following the glidepath to maintain the descent to AT or ABOVE 6 370 feet at the Missed Approach Point MAP RW35R as seen in Figure 7 49 Note the BARO MIN bug is now displayed on the altimeter E FLIGHT PLAN WORTH UF j ACTIVE FLIGHT PLAN TFR KMKC KOOS HO DATA FSHER Approach KCOS RMAV HAR IABUK iaf CURRENT VHW PROFILE ACTIVE Wi WPT FT at VS TGT FFH FP es VS REQ FPH HE TO TOD ohne TERRAIN VS REG TIRE T W DEV F j 10 FT Keep Vertical _ Deviation Pointer Centere 59 90IN 637 FT Figure 7 49 Descending to the Missed Approach Point Garmin G1000 Cockpit Reference Guide for the Cessna Nav III In this missed approach procedure the altitude immediately following the MAP in this case 6368FT is not part of the published procedure It is a Course to Altitude CA leg which guides the aircraft along the runway centerline until the altitude required to safely make the first turn toward the MAHP is exceeded In this case if the aircraft altitude is below the specified altitude 6 368 feet after crossing the MAP a direct to is established to provide a course on runway heading until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to is established to the published MAHP MOGAL
167. he NAV1 and or NAV2 receiver The receiver may NAV2 SERVICE NAV2 needs still be available The G1000 system should be serviced service Return unit for repair NAV1 RMT XFR NAV1 remote 4 S E E transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or WAV RMT XFR ET pressed state Press the transfer switch again to cycle its operation If the remou problem persists the G1000 system should be serviced transfer key is stuck G S1 FAIL G S1 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 G S2 FAIL G S2 is inoperative system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The l receiver may still be available The G1000 system should be serviced when G S2 SERVICE G S2 needs service possible Return unit for repair GEA 71 Message Advisories GEA1 CONFIG GEA1 contig error The GEA1 configuration settings do not match those of backup configuration Contig service req d memory The G1000 system should be serviced MANIFEST GEA1 software The 1 GEA 71 has incorrect software installed The G1000 system should be mismatch communication halted serviced GTX 33 Message Advisories XPDR1 CONFIG XPDR1 config The transponder configuration settings do not match those of backup error Contig service req d config
168. he flashing annunciation stops and the flight director enters the default mode for the affected axis Figure 6 4 Loss of VOR Signal 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL If the information required to compute a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis The flight director is automatically disabled if the attitude information required to compute the default flight director modes becomes invalid or unavailable Pitch Modes e Pitch Hold default mode Holds the current aircraft pitch attitude may be used to climb descend to the Selected Altitude Selected Altitude Capture Captures the Selected Altitude Altitude Hold Holds the current Altitude Reference Vertical Speed Maintains the current aircraft vertical speed may be used to climb descend to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed while the aircraft is climbing descending to the Selected Altitude Vertical Path Tracking Follows an active vertical profile for enroute and terminal phases of flight e VNAV Target Altitude Capture Captures the VNAV Target Altitude e Glidepath Intercepts and tracks the WAAS glidepath on approach only available in installations with GIA 63W Integrated Avionics Units and when WAAS is available e Glideslope Intercepts and tracks the ILS glidesl
169. he large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the second rectangular page icon View Information on the Nearest Intersection 1 With the Nearest Intersections Page displayed press the FMS Knob to activate the cursor 2 Turn either FMS Knob to select the desired intersection 3 Press the FMS Knob to remove the flashing cursor 190 00384 09 Rev A SECTION 7 NAVIGATION 7 11 NEAREST NDB Figure 7 63 Nearest NDB Page Select the Nearest NDB Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the third rectangular page icon Access Information on a Specific NDB 1 With the Nearest NDB Page displayed press the FMS Knob to activate the cursor 2 Turn either FMS Knob to select the desired NDB The remaining information on the Nearest NDB Page pertains to the selected NDB 3 Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION MET NORTH UP 136 975 118 000 coe NEAREST VOR OC F THF ORHAT LOM eh Cr woa4 44 27 FREQUENCY Figure 7 64 Nearest VOR Page Select the Nearest VOR Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fourth rectangular page icon View Information on the Nearest VOR 1 With the Nearest VOR Page displayed press the VOR Softkey t
170. he loaded approach is not active Activate active approach when required SLCT FREQ Select appropriate The system notifies the pilot to load the approach frequency for the appropriate frequency for approach NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI approach to the correct NAV receiver EIR ESIE Ealelie act Bad parallel track geometr unavailable bad geometry P J a PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track maen IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach The current vertical waypoint can not be reached within the maximum flight path current vertical waypoint angle and vertical speed constraints The system automatically transitions to the next vertical waypoint 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 21 SECTION 13 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont VNV Unavailable Unsupported The lateral flight plan contains a procedure turn vector or other unsupported leg leg type in flight plan type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track The current track angle error exceeds the limit
171. he small FMS Knob to change the percentage value The percentage value is the day night crossover point based on the percentage of backlighting intensity For example if the value is set to 15 the day night display changes when the display backlight reaches 15 of full brightness The display must be changed in order for the new setting to become active This may be accomplished by selecting another page or changing the display range 6 Press the FMS Knob when finished to remove the Chart Setup Menu Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 11 ADDITIONAL FEATURES 11 16 11 5 XM RADIO ENTERTAINMENT NOTE Refer to the Hazard Avoidance Section for information about XM Weather products The optional XM Radio entertainment feature is available for the pilots and passengers enjoyment throughout the Continental U S Using XM Radio The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled AUK XM RADIO 126 400 134 750 coe ACTIVE CHANNEL CHANNELS CHANNEL Clint Eee Al aspar CATEGORY ALL CATEGORIES Figure 11 25 XM Radio Page Garmin G
172. hen own aircraft is below 1 000 feet AGL or on the ground Non aircraft ground traffic Ground traffic is only displayed when own aircraft is below 1 000 feet AGL or on the ground a PL Non Threat Traffic with directional information but positional ait Bearing u Traffic accuracy is degraded Points in the direction of the aircraft track Figure 10 14 TAS Traffic on Navigation Map n e i i Aircraft ADS B Traffic Optional I en ation a o Em tail number Relative Altitude ADS B is limited to displaying traffic in the G1000 or Flight ID Gin this case 1200 Operation is similar to the TAS system discussed number feet above own previously with the exception of symbology The meray following traffic symbols are used to display traffic with y Altitude Trend up arrow the ADS B system Intruder indicates Aircraft climbing down Ground Track arrow indicates extends in the direction of the aircraft movement descending Figure 10 15 Example ADS B Traffic Advisory 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 9 SECTION 10 HAZARD AVOIDANCE 10 5 TERRAIN AND OBSTACLE PROXIMITY 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area NOTE Terrain data is not displayed when the A P F 5 AP TERRAIN 136 975 118 000 coz aircraft latitude is greater than 75 degrees north T Y EET or 60 degrees sout
173. i SIH 9000 nli 1 5 ANH S600 CURRENT Vit PROFILE ACTIVE VW WET 10O0OFT ot OPSHN 3 WS TGT 553FPH_ FPA VS REG FF TIRE TO TOD 1541 FPL c Press the ENT Key 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 15 SECTION 7 NAVIGATION 15 As seen in Figure 7 38 the aircraft is approaching TOD Note the target vertical speed required to reach the selected altitude The Vertical Deviation Indicator VDI and the Required Vertical Speed Indicator RVSI are now displayed on the PFD as shown in Figure 7 39 Koo ee 5 9 136 975 118 000 com FPL ACTIVE FLIGHT PLAN 136 975 118 004 cone ACTIVE FLIGHT PLAN KHKC KCOS OTK eob TRE OTK GIS ALT Airwor V263 7BE BU ee as MEE re FT Par n FT Arrival KCOS TBE DBRY 1 ALL OPSHH JIH 258 B SeH TOGOUFT OPSHH 258 JONH TOGOOFT FSHER 32 SNH TOGQGFT PYNON Hr 1131H TBECOHFT Approach KOCOS RMAW S5RGrS LPW HABUK inf WER S NA 9000r FALUR 251 S N ge00r erl CURRENT VIN PROFILE ACTIVE VN WPT TEODOFT ot OPSHN JHH Va TOT 55JFPH FPA 25 V5 REG AFPA TIME TO TOO OAZE V DEW 200FT Figure 7 38 Approaching Top of Descent TOD TOD within 1 minute 122 008 EE 122 358 Time target eoo Vertical Deviation Required Indicator Vertical VDI Speed Indicator RVSI 3 Figure 7 39 VDI amp RVSI Upon Reaching Top of Descent TOD 7 16 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
174. ic Minimum Descent Altitude Alerting Visual Annunciations Set the barometric altitude minimums 1 2 3 4 5 2 8 Press the TMR REF Softkey Turn the large FMS Knob to highlight the Minimums field Figure 2 16 Turn the small FMS Knob to select BARO OFF is selected by default Press the ENT Key or turn the large FMS Knob to highlight the next field Use the small FMS Knob to enter the desired altitude from zero to 16 000 feet To remove the window press the CLR Key or the TMR REF Softkey HORIZONTAL SITUATION INDICATOR HSI The HSI compass can be displayed as a 360 rose or 140 arc by pressing the PFD Softkey followed by the Garmin G1000 Cockpit Reference Guide for the Cessna Nav III A Turn Rate Indicator 2 Current Track Indicator G Lateral Deviation Scale Navigation Source Aircraft Symbol 6 Course Deviation Indicator 7 Rotating Compass Rose OBS Mode 9 TO FROM Indicator Heading Bug Course Pointer Flight Phase 13 Turn Rate and Heading Trend Vector Heading 15 Lubber Line Figure 2 18 Horizontal Situation Indicator 190 00384 09 Rev A SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Course Deviation Indicator CDI Tick marks to the left and right of the lubber line denote half standard and standard turn rates A magenta Ta phase of flight as seen in Figure 2 22 Scaling may be turn rate trend vector shows the cu
175. icated altitude Press the ENT Key when finished 11 The flashing cursor moves to the barometric pressure field Turn the FMS Knobs to enter the altimeter barometric pressure setting Press the ENT Key when finished 12 The tlashing cursor moves to the total air temperature field Turn the FMS Knobs to enter the total air temperature Press the ENT Key when finished Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 8 9 SECTION 8 FLIGHT PLANNING Blank Page 8 10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1 2 3 4 5 6 1 8 190 00384 09 Rev A Press the PROC Key Turn the large FMS Knob to highlight SELECT DEPARTURE Press the ENT Key If a flight plan is active the departure airport is displayed as the default A list of available departures is also displayed If no flight plan is active use the FMS Knobs to enter the identitier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Departure field Turn the small FMS Knob to display a list of available departures Turn either FMS Knob to select the desired departure and press the ENT Key AIRPORT PUBLIC NEW CENTURY ATRCENTER 0 L ATH C Ao DEPARTURE CHIEFS Figure 9 1 Select Departure A list of runways may be displayed for the d
176. igure 8 9 Invert Flight Plan Confirmation Figure 8 6 Delete Flight Plan 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 9 3 SECTION 8 FLIGHT PLANNING 8 7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the PFD Create a New Flight Plan Using the MFD NOTE A flight plan cannot be entered using the PFD if another flight plan is active 1 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the NEW Softkey to display a blank flight plan page for the first empty storage location STORED FLIKT PLAN 1 Press the FPL Key then press the FMS Knob to activate the cursor 2 Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large Figure 8 10 Create FPL on MFD FMS Knob to the right to move the cursor to the next character position NOTE After the first leg is entered using the PFD only it is immediately activated 3 Turn the small FMS Knob to display the Waypoint Information Window 4 Turn the small FMS Knob to the right enter the first character of the identifier of the departure waypoint Turning the knob to the left accesses the FPL NRST and
177. inal Mode and is annunciated by displaying TERM on the HSI Garmin G1000 Cockpit Reference Guide for the Cessna Nav III NOTE If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database those altitudes are displayed as white numerals This indicates the altitudes will not be used by the system for vertical guidance until manually accepted by the pilot To accept the displayed altitude place the cursor over the altitude and press the ENT Key The altitude entry then changes to light blue numerals indicating the altitude will now be used by the system for providing vertical guidance TRE 136 975 L ACTIVE FLIGHT PLAN 136 975 NORTH UF ACTIVE FLIGHT PLAN KMKC KDOS KCOS TBE DBRY 1 ALL OPSHN 3mh 20 94 91 10000 CURRENT WNW PROFILE ACTIVE Wy WPT TRGGOeT ot OPSHN 3m VS TGT 051FFH FPA VS REG ee TIHE TO TOO 4204 He V DEV O F 3mh FP Figure 7 29 Direct to Active 12 The aircraft is proceeding to OPSHN The expected approach is the RNAV LPV approach to runway 35R so it is selected a Press the PROC Key to display the Procedures Window If the GPS system is not WAAS capable or WAAS is not available the LPV approach will not be displayed in the list of available approaches Selecting the LNAV approach for runway 35R gives vertical guidance up to the IAF 190 00384 09 Rev A b SELECT APPROACH should be highlighted as shown in Figure 7 30 PROCE
178. ing to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp B WARNING Because of anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING Itis very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III WARNINGS CAUTIONS amp NOTES CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE When using Stormscope there are several atmospheric phenomena in addition to nearby thunderstorms that can
179. ing Source Waypoint Identifier Bearing Pointer Source Icon Figure 2 26 BRG1 Information Window 190 00384 09 Rev A SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source _ 5 Pointer Bearing Icon Source Figure 2 27 BRG2 Information Window DME optional To display the DME Information Window press the PFD Softkey followed by the DME Softkey Navigation Source Change CDI navigation sources 1 Press the CDI Softkey to change from GPS to VOR1 LOC1 2 Press the CDI Softkey again to change from VOR1 LOC1 to VOR2 LOC2 3 Press the CDI Softkey a third time to return to GPS When using GPS as the navigation source the following may appear e LOI GPS position integrity is inadequate for the current procedure being flown If GPS is being used as primary navigation and LOI is annunciated other means of primary navigation is required such as VHE LOI is also displayed during GPS position initialization e WARN GPS detects a position error Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Waypoint Identifier 2 11 SECTION 2 FLIGHT INSTRUMENTS 2 12 OBS Displayed when operating in OBS Mode SUSP Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended DR Navigating using Dead Reckoning due to an error in the GPS solution Figure 2 29 GPS LOI GPS SUSP LOC1 and VOR2 Enable disable OBS Mode while navigating
180. ings do not match backup configuration GIA2 CONFIG GIA2 config error Memory The G1000 system should be serviced Contig service req d 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3215 SECTION 13 ANNUNCIATIONS 13 16 amp ALERTS GIA 63W Message Advisories Cont GIA1 CONFIG GIA1 audio contig error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 GIA2 CONFIG GIA2 audio config system should be serviced error Contig service req d GIA1 COOLING GIA1 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to GIA2 COOLING GIA2 temperature warm up to operating temperature too low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 GIA2 COOLING GIA2 over system should be serviced temperature GIA1 SERVICE GIA1 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 GIA2 SERVICE GIA2 needs service system should be serviced Return the unit for repair HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The
181. ion on loading and activating approach procedures 8 12 REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN 1 With the Active or Stored Flight Plan Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedures waypoints 3 Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure or airway 8 13 STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan Figure 8 19 Store Flight Plan Confirmation 190 00384 09 Rev A 8 14 EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan and press the ENT Key Turn the large FMS Knob to place the cursor in the desired locations for entering changes Turn the FMS Knobs to make the desired changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page 8 15 DELETE A WAYPOINT FROM THE
182. ion on the MFD Select the Nearest Airports Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the first rectangular page icon Initially the closest airport to the aircraft s present position is displayed Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 25 SECTION 7 NAVIGATION Access Information on a Specific Airport 1 2 3 With the Nearest Airports Page displayed press the APT Softkey to place the cursor in the NEAREST AIRPORTS field The first airport in the nearest airports list is highlighted Turn either FMS Knob to highlight the desired airport Press the FMS Knob to remove the flashing cursor Access Runway Information for the Selected Airport 1 2 3 With the Nearest Airports Page displayed press the RNWY Softkey to place the cursor in the RUNWAYS field Turn the small FMS Knob to select the desired runway Press the FMS Knob to remove the flashing cursor Quickly Tune the COM Transceiver to a Nearby Airport Frequency 1 2 7 26 With the Nearest Airports Page displayed press the FREQ Softkey to place the cursor in the FREQUENCIES field Turn either FMS Knob to select the desired frequency Press the ENT Key The selected trequency is placed in the COM standby frequency field Press the Frequency Transfer Key to place the frequency in the active field Press the FMS Kn
183. irspeed The G1000 system should be serviced The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid The 1 AHRS has incorrect software installed The G1000 system should be serviced Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced The GMU 44 has incorrect sottware installed The G1000 system should be serviced SECTION 13 ANNUNCIATIONS 13 20 amp ALERTS GDL 69 69A Message Advisories error Config service req d memory The G1000 system should be serviced system should be serviced mismatch communication halted serviced GDC 74A Message Advisories MANIFEST GDC1 software The GD
184. issued only after an aviation database update Verity use of airways in stored flight plans and reload airways as needed Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 13 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont FPL TRUNC Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete truncated approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate This occurs when the pilot attempts to activate a stored flight plan that contains locked flight plan locked waypoint Remove locked waypoint trom flight plan Update flight plan with current waypoint ME eve tillage Arriving at waypoint xxxx where xxxx is the waypoint name waypoint Xxxx STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead Special use airspace is ahead of aircraft The aircraft will penetrate the airspace less than 10 minutes within 10 minutes a BEA fl a Special use airspace is near and ahead of the aircraft position Bie NEBR rls CE E ea Special use airspace is within 2 nm of the aircraft position than 2 nm APR INACTV Approach is not The system notifies the pilot that t
185. itude Bug The Selected Altitude Bug is displayed at the Selected Altitude or the edge of the tape whichever is closer to the current altitude to provide increased altitude awareness and to set the desired hold altitude for the autopilot Set the Selected Altitude Bug Turn the ALT Knobs to set the Selected Altitude Bug The small ALT Knob sets the hundreds and the large ALT Knob sets the thousands This altitude also appears in the Selected Altitude Box above the Altimeter Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in six seconds if the current rate of vertical speed is maintained Barometric Setting Box Select barometric pressure Turn the BARO Knob to select the desired setting Quickly enter standard pressure 1 Press the PFD Softkey 2 Press the STD BARO Softkey STD BARO will now be displayed in the Barometric Setting Box Altitude Alerting Within 1000 ft Within 200 ft Deviation of 200 ft Figure 2 8 Altitude Alerting Visual Annunciations Visual annunciations appear in the Altitude Reference Box Whenever the setting is changed the Altitude Alerter is reset The Altitude Alerter is independent of the Automatic Flight Control System 190 00384 09 Rev A Metric Display Display altitude in meters and barometric pressure in hectopascals 1 Press the PFD Softkey to display the
186. ivity returns the system to the top level softkeys INFO CNL aw VOL Ey ser st PS2 PSS PSH Figure 11 27 Accessing and Selecting XM Preset Channels BACK Garmin G1000 Cockpit Reference Guide for the Cessna Nav III ey SECTION 11 ADDITIONAL FEATURES 11 18 Volume Radio volume is shown as a percentage Volume level is controlled by pressing the VOL Softkey which brings up the MUTE Softkey and the volume increase and decrease softkeys Adjusting the volume 1 With the XM Radio Page displayed press the VOL Softkey 2 Press the VOL Softkey to reduce volume or press the VOL Softkey to increase volume Once the VOL Softkey is pressed the volume can also be adjusted using the small FMS Knob 3 Press the MUTE Softkey to mute the audio Press the MUTE Softkey again to unmute the audio Boota C OLUILU 23 E TE voL Figure 11 28 Volume Control Automatic Audio Muting XM Radio audio is muted automatically when the aircraft groundspeed exceeds approximately 30 knots and the airspeed is less than approximately 80 knots The audio is not unmuted automatically The audio must be manually unmuted once the aircraft is airborne and outside the applicable speed range Automatic Audio Muting has been implemented to meet regulatory requirements that the aural stall warning be heard When the aircraft is operating within the automute airspeed range the MUTE Softkey and the vo
187. l Selected radios aural alerts OFF alerts pilot copilot alerts pilot copilot _ pilot copilot passengers passengers music passengers music MUSIC Selected radios aural Copilot passengers alerts pilot sage Copilot passengers music Selected radios OFF aural alerts pilot Copilot passengers music Selected radios aural alerts pilot passengers music Selected radios aural Selected radios aural Passengers musi alerts pilot copilot alerts pilot copilot ASSENGETS MUSIC Table 5 1 ICS Isolation Modes 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 5 3 SECTION 5 AUDIO PANEL 5 4 5 7 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator Pressing the small VOL SQ Knob now switches be tween volume and squelch adjustment by lighting VOL or SQ respectively wv wv MAN sQ PLAY w CREW wv PILOT COPLT ICS_ISOLATION PILOT O PASS VOL Figure 5 8 Volume Squelch Control 5 8 DIGITAL CLEARANCE RECORDER AND PLAYER Fach reception of primary active COM audio is automatically recorded ina memory block When the next transmission is received it is recorded in the next memory block and so on Once the 2 5 minutes of recording time has been reached the recorder begins recording over the stored memory blocks starting from the oldest block Powering off the unit auto
188. lay Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 7 SECTION 10 HAZARD AVOIDANCE Traffic Advisory System TAS Optional Refer to the Honeywell KTA 870 Pilots Guide for a detailed discussion of the KTA 870 system System Self Test 1 2 3 4 Set the range to 2 6 nm Press the STANDBY Softkey Press the TEST Softkey Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed as shown in Figure 10 12 and a voice alert TAS System Test OK is heard If the self test fails the system reverts to Standby Mode and a voice alert TAS System Test Fail is heard 136 975 118 888 conz HOG UP Figure 10 12 Self Test OK Display Displaying Traffic on the Traffic Map Page 1 2 10 8 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3 Press the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 5 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode fi
189. le means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing airport location and identification on the synthetic terrain display When activated the signs appear on the display when the aircraft is approximately 15 nm from an airport and disappear at approximately 4 5 nm Airport Runways are depicted at the published field signs are shown without the identifier until the aircraft elevation for the selected airport In some is approximately eight nautical miles from the airport rare cases actual runway elevation differs Airport signs are not shown behind the airspeed or altitude significantly from the airport field elevation display Airport signs are activated and deactivated by causing SVS runways to appear higher or lower pressing the APTSIGNS Softkey than the actual runway Runway data provides improved awareness of runway le lore witht Lente location with respect to the surrounding terrain As Between 8nm Between 4 5 nm runways are displayed those within 45 degrees of the Traffic and 15 nm and 8 nm aircraft heading are displayed in white Other runways anid iros a E Will be gray in color When an approach for a specific runway is active that runway will appear brighter and be outlined with a white box regardless of the runway orientation as related to aircraft heading As the aircraft gets closer to the runway more detail such as runway numbers a
190. ll positions are depicted accurately in relation to the nose of the aircraft 10 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Change the viewing mode between 360 and 120 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data trom the display 10 3 XM WEATHER SERVICE OPTIONAL WARNING XM Weather is not intended to be used for hazardous weather penetration Weather information provided by XM Radio Service is approved only for weather avoidance not penetration 1 From the Navigation Map Page press the MAP Softkey 2 Press the NEXRAD or XM LTNG Softkey to display the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page MAP NAVIGATION MAP 136 975 118 888 com _ WORTH UP TOPO TERRAIN Figure 10 7 Navigation Map Page Displaying NEXRAD Weather 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE NOTE Weather is not displayed on the Navigation Map Page at zoom levels less than 10 nm Displaying METAR and TAF information on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Press th
191. located on the bezels of the PFD and MFD Disengages the autopilot selects flight director Go Around Mode and activates the missed approach The GA Switch is located on the instrument panel above the throttle e MET Switch Manual Electric Trim The MET Switch is located on the pilots control wheel left grip This composite switch is split into left and right sides The left switch is the ARM contact and the right switch controls the DN forward and UP rearward contacts The MET ARM switch can be used to disengage the autopilot and to acknowledge an autopilot disconnect alert and mute the associated aural tone Manual trim commands are generated only when both sides of the switch are operated simultaneously If either side of the switch is active separately for more than e AP DISC Switch Autopilot Disconnect three seconds MET function is disabled and PTRM is displayed as the AFCS Status Annunciation on the PFD The function remains disabled until both sides of the switch are inactivated Figure 6 1 Dedicated AFCS Controls The following AFCS controls are located in the cockpit separately from the MFD Disengages the autopilot and interrupts pitch trim operation The red AP DISC Switch is located forward of the MET Switch on the pilots control wheel left grip This switch may be used to 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL
192. lti tude at a constant airspeed This descent method does not account for flight plan waypoint altitude constraints e Vertical Path Tracking descent Vertical Path Track ing Mode is used to follow the vertical descent path defined in the GPS flight plan Altitude constraints correspond to waypoints in the flight plan Before VNV flight control can provide vertical profile guidance a VNV flight plan must be entered and enabled e Non path descent in a VNV scenario While the flight director is following VNV guidance for descent Pitch Hold Vertical Speed or Flight Level Change Mode can be used to descend to the VNV Target Altitude prior to reaching the planned TOD Flight Level Change Mode is used in the example Flight Level Change descent 1 Select Flight Level Change Mode a Using the ALT Knob set the Selected Altitude to 10 000 feet ALT Mode 2 D Cruise Altitude of 12 000 MSL b Press the FLC Key to activate Flight Level Change Mode The annunciation FLC appears next to the Airspeed Reference which defaults to the current aircraft airspeed Selected Altitude Capture Mode is armed automatically _ GPS AP ALTS 2 Use the NOSE UP NOSE DN keys or push the CWS Button while hand flying the aircraft to adjust the commanded airspeed while maintaining the same power or reduce power to allow descent in Flight Level Change Mode while the autopilot maintains the current airspeed As the aircra
193. ltimeter AIRPORT KEOS W PUBLIC CITY OF COLORADO SPRINGS COLORADO SPRINGS CO APPROACH CHANNEL CHANNEL 37799 To HASA APPROACH AWAY S6RGes LPY TRANSITION HABUK Iof HINTHUHS 7 PRIHARY FREQUENCY p gt SEQUENCE HABUK bof FALUR 267 G N H CEGIX fof 357 G NH RW35R mop 351 5 NA LOAD om ACTIVATE Figure 7 33 Barometric Minimums Enabled i Press the ENT Key Turn the small FMS Knob to enter the published decision altitude for the approach procedure The altitude is entered to the nearest 10 feet Press the ENT Key AIRPORT KEOS W PUBLIC CITY OF COLORADO SPRINGS COLORADO SPRINGS CO JAPPRORCH CHANNEL CHANNEL 97799 To W354 APPROACH RNAY SSRcPs LPW TRANSITION HABLE inf HINTHUAS aau BARO PRIMARY FREQUENCY SEQUENCE HABUK lof FALUR 261 S NN CEGIX fof 357 6 0NH RW3S5R mop 351 5 1MH LOAD og ACTIVATE Figure 7 34 Decision Altitude Entered Garmin G1000 Cockpit Reference Guide for the Cessna Nav III j With LOAD highlighted again press the ENT Key The selected approach is added to the flight plan as seen in Figure 7 35 196 975 118 008 cor OTK TRE ETE FFL ACTIVE FLIGHT PLAN 136 975 118 000 cone NORTH UP ACTIVE FLIGHT FLAN KMEKC KCOS Airway V263 1BE KOHTO Pi WH T TBE ere Arrival KOOS TBEDBRY IALL OPSHN 31H 255 Oh 1000F DPSHH Pas SHH TEBRRFT FSHER i ad Jai TEQARFT PHNOM a57 119W 1BOLUFT Aperooch KCOS RNAY 35R6rs LPW H
194. lume softkeys are subdued and the Unmute selection of the Page Menu is unavailable preventing the audio from being unmuted at this time Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Audio availability conforms to the following three states e Audio is available on the ground until the aircraft exceeds 30 knots e Audio is automatically muted not available from Airborne Status up to 80 knots airspeed e Audio is available when airspeed is over 80 knots Unmuting XM audio 1 With the XM Radio Page displayed press the VOL Softkey 2 Press the MUTE Softkey to restore unmute XM Audio 11 6 SCHEDULER The Scheduler feature can be used to enter and display reminder messages e g Change oil Switch fuel tanks or Altimeter Transponder Check in the Alerts Window on the PFD Messages can be set to display based on a specific date and time event once the message timer reaches zero one time default setting or recurrently whenever the message timer reaches zero periodic Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed When power is cycled all messages are retained until deleted and message timer countdown is resumed crapa mn 3100 3000 MESSAGES SCHEDULER 1kali MEG ba IDENT THMR REF NAST Figure 11 29 PFD Alerts Window 190 00384 09 Rev A SECTION 11 ADDITIONAL FEATURES 7 Press the ENT Key again or
195. mall FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 54 The list is populated only when navigating a flight plan 3 Turn the small FMS Knob to the right to display the RECENT airports as shown in Figure 7 56 Figure 7 56 Recently Entered Airports List 4 Turn the large FMS Knob to select the desired airport 5 Press the ENT Key Select an Airport by Facility Name or City Location 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to the right to select the facility name or location city field 3 Enter the desired facility name or city 5 Press the ENT Key If there are duplicate names in the database a list is displayed trom which to choose the desired location 6 To remove the flashing cursor press the FMS Knob SECTION 7 NAVIGATION Access Runway Information 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to place the cursor on the RUNWAYS identifier field 3 Turn the small FMS Knob in the direction of the green arrow to display the next runway for the selected airport Continue turning the small FMS Knob to select the desired runway 4 To remove the flashing cursor press the FMS Knob Access Frequency Information 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor
196. matically clears all recorded blocks Figure 5 9 Clearance Recorder Play Key Pressing the PLAY Key once plays the latest recorded memory block then returns to normal operation Garmin G1000 Cockpit Reference Guide for the Cessna Nav III e Pressing the MKR MUTE Key while playing a memory block stops play e Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block If a COM input signal is detected while playing play is halted and the new COM input signal is recorded as the latest block 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL SECTION 6 AUTOMATIC FLIGHT hier ie en disconnect and mute the CONTROL e CWS Button Control Wheel Steering A NOTE The Aircraft Flight Manual AFM always Momentarily disengages the autopilot and supersedes the information in this guide This synchronizes the flight directors Command Bars section only applies to the GFC 700 Automatic with the current aircraft pitch if not in Glideslope Flight Control System AFCS Mode and roll if in Roll Hold Mode The CWS Button is located on the top of the pilot s control 6 1 AFCS CONTROLS wheel right grip Upon release of the CWS Button the flight director may establish new reference points depending on the current pitch and roll modes e GA Switch Go Around The following dedicated AFCS keys are
197. mation Window T DME Information Window COI DME KPDR DENT 119 788 158 cons 136 975 BOO conz A 380 1300 f i 1200 e i 4 4h Y Peres HARO MIN 29 92IN T25QFTT KMCI ILS AIL DOTTE fof RWATIL map 1426FT CAMDO mahp ane tha Fa NAV POR R LOL TMR REF NRST rs BRG2 Information Window C Flight Plan Window 10 Barometric Minimums Box Selected Altitude Bug Selected Course Box 13 Barometric Minimums Bug Vertical Deviation Glidepath WAAS en abled systems only Glidesope Indicator 15 Marker Beacon Annunciation Figure 2 2 Additional PFD Information Active Flight Plan Leg Distance to Next Waypoint Bearing to Next Waypoint Figure 2 3 PFD Navigation Status Box 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A 2 1 AIRSPEED INDICATOR Vspeed References Speed Ranges Airspeed Trend ector Figure 2 4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer The pointer becomes red upon reaching Vne Figure 2 5 Red Pointer at Vne Speed Ranges The color coded speed range strip denotes flaps operating range normal operating range and never exceed speed Vne A red range is also present for low speed awareness Refer to the Pilots Operating Handbook POH for airspeed limitations and indicator markings Airspeed Trend Vector The end of the trend vector
198. meet the requirements of the clearance 1 Prior to departure the TIFTO2 departure the airways and the DBRY 1 arrival at KCOS are loaded See the Procedures section for loading departures and arrivals Note the magenta arrow in Figure 7 11 indicating the active departure leg After takeoff ATC assigns a heading of 240 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III PD SECTION 7 NAVIGATION 2 Figure 7 11 shows the aircraft on the assigned heading of 240 TERM Terminal is the current CDI flight phase displayed on the HSI indicating 1 0 nm CDI scaling TRK co ACTIVE FLIGHT PLAN omK 28 TRK 2 ETE 136 975 118 000 com FPL 136 975 118 000 corz ACTIVE FLIGHT PLAN KMKC NORTH UP KLOS DTK E ALT Departure KMKC ALL TIFTOZ TIFTO Airway V244 LA8 DUMYE HYS RANS ZAMPE CURRENT VNV PROFILE q ACTIVE VNV WPT VS TGT VS REO s PH TIHE TO TOO e2649 136 975 ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS Departure KMKC ALL TIFTO2 TIFTO Airway V244 LAA DUMYE 2AMPC CURRENT VNV PROFILE ACTIVE VNV WPT VS TGT VS REO Figure 7 12 Assigned Heading of 290 Figure 7 11 Assigned Heading of 240 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 136 975 11 3 ATC now assigns routing to join V4 A heading of 290 is assigned to intercept V4 The aircraft turns to heading 290 as seen in Figure 7 12 8 888 com 8 000 c
199. mum 2 8 Base reflectivity 10 4 BRG1 2 11 BRG2 2 11 C CAUTION 13 2 CDI 2 9 2 11 7 3 7 6 7 12 7 17 7 21 9 2 13 21 Cell 10 2 Cell mode 10 2 Cell movement 10 5 Chart Not Available 11 12 11 15 Chart options 11 12 11 15 ChartView 11 11 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III INDEX ChartView functions 11 11 ChartView plan view 11 12 ChartView softkeys 11 11 Checklists 11 20 11 21 Checklist softkeys 11 20 Cloud Tops 10 4 CLR 1 3 3 9 Coast mode 10 7 Code selection 4 5 Command Bars flight director 6 2 COM frequency window 4 1 COM Knob 4 3 Controls 1 2 Control Wheel Steering CWS 6 23 Create a new user waypoint 8 1 CWS Button 6 1 6 5 6 10 6 13 6 18 6 20 6 23 Cyclones 10 5 Cylinder Head Temperature 3 1 3 4 D Databases 1 12 Day Night views 11 13 11 15 Day view 11 13 11 15 Dead Reckoning 2 12 12 3 13 8 Departures 9 1 Direct to 7 1 7 5 7 11 7 12 8 8 DME 1 8 DR 2 12 DR mode 12 3 12 4 Dual CDU failure 12 2 E ECHO TOPS 10 4 Edit a flight plan 8 7 EDR 10 19 Electronic checklists 11 20 11 21 Emergency checklist 11 22 Engine Hours 3 3 3 8 Engine Leaning 3 6 Engine Page 3 1 Excessive Descent Rate 10 19 Exhaust Gas Temperature 3 2 3 4 Index 1 INDEX Index 2 F FD 1 4 Five Hundred Aural Alert 10 15 10 19 FLC 1 4 Flight director 6 2 6 3 Pitch modes 6 3 6 9 Roll modes 6 17 6 19 Flight ID 4 5
200. n aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration WARNING GDL 69 Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69 is approved only for weather avoidance not penetration WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A WARNINGS CAUTIONS amp NOTES WARNING The Garmin G1000 as installed in Cessna Nav III aircraft has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit B W
201. nce FLTA 10 15 LL et sneer aes ere er ee ene ent ar en ree 12 2 Displaying Terrain and Obstacles on the Navigation Map 12 5 Hazard Displays with Loss of GPS Position 12 2 10 16 12 6 Dead Reckoning 0 ccccccsesesee eee 12 3 10 7 Terrain Awareness amp Warning System SECTION 13 ANNUNCIATIONS amp ALERTS 13 1 TAWS Display Optional sae ee va KOAA Aoa 10 16 13 1 Alert Level Definitions fehcdccconcles ccc EZ Displaying Terrain on the TAWS Page 10 16 1 37 NAV Ill Aircraft Alerts 133 ENS sae COO ieee aia ae WARNING Alerts 172R 1725 182 11827 206H TAY TAMD uar a 10 17 and T206H 13 3 Manua rE TE ptt egui Pe CAUTION Alerts 172R 1725 1821 T1827 206H Forward Looking Terrain Avoidance FLTA 10 18 and T206H 13 3 PSST De eee ee CAUTION Alerts T182 1206 and 206 with Prop Excessive Descent Rate Alert EDR uc 10 19 Ae 13 3 Negative Climb Rate After TakeotfAlert NCR 10 19 Safe 0 a a E T 89 T20 6 and 206 Five Hundred Aural Alennus 10 19 ui z S Only pre 13 3 Displaying Terrain and Obstacles on the Navigation 13 3 CO pee dian P E ee ae 133 ne 13 4 APCS Alerts 13 4 TAWS Alerts SUMMANY onnsurennenrenenneen 10 21 eee Pe Se ee aie ONES soca nn AO G ae ies 13 6 Other G1000 Aural Alerts occu 13 6 SECTION 11 ADDITIONAL FEATUREG ie 13 7 G1000 System Annunciations 13 7 11 1 Synthetic Vision System SVS O
202. nce is shown on the indicator Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC FLIGHT CONTROL Selected Altitude Vertical Speed Vertical Speed Capture Mode Mode Active Reference Armed Selected Vertical Altitude Speed ane Vertical Speed ae Bug Command Bars Indicate Climb to Attain Vertical Speed Reference aan 29 921N 92IN Figure 6 8 Vertical Speed Mode Changing the Vertical Ref anging the Vertical Speed Reference Flight Level Change Mode is selected by pressing the The Vertical Speed Reference shown both in the AFCS FLC Key When Flight Level Change Mode is active the Status Box and above below the Vertical Speed Indicator flight director continuously monitors Selected Altitude B be changed by airspeed and altitude This mode acquires and maintains Using the NOSE UP NOSE DN Keys the Airspeed Reference while climbing or descending to e By pressing the CWS Button hand flying the the Selected Altitude shown above the Altimeter The aircralt to attain a new Vertical Speed Relerence Airspeed Reference is set to the current airspeed upon then releasing the CWS Button mode activation Flight Level Change Mode is indicated by an FLC annunciation beside the Airspeed Reference Flight Level Change Mode FLC in the AFCS Status Box The Airspeed Reference is also displayed directly above the Airspeed Indicator along NOTE The Selected Altitude should be set before Wi
203. nd press the ENT Key PAGE MENU OPTIONS Declutter Measure Bearing Distance Show Chart Press the FMS CRSR knob to return to base page Navigation Map Page OPTIONS Menu HAF SETUP GROUP Map ORIENTATION Trock up AUTO 200H All On H LOOK FWD HIN LOOK FWD TIHE OUT LAND DATA On TRACK VECTOR OFF WIND VECTOR OFF NAW RANGE RING OFF TOPO DATA On gt 1500m TOPO SCALE OFF TERRAIN DATA On OBSTACLE DATA OFF ZONH FUEL RNG RSW OFF 045 FIELD OF VIEW HEM Press the FMS CRSR knob to return to bose poge Map Setup Menu Map Group Field of View Option Figure 11 12 Enabling SVS Field of View Turn the large FMS Knob to scroll to FIELD OF VIEW Turn the small FMS Knob to select On or Off Press the FMS Knob to return to the Navigation Map Page 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 9 SECTION 11 ADDITIONAL FEATURES 11 2 SAFETAXI When viewing at ranges close enough to show the airport detail the map reveals taxiways with identifying letters numbers airport Hot Spots and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges Airport Hot Spots are outlined to caution pilots of areas on an airport surface where positional awareness confusion or runway incursions happen most often Hot Spots are defined with a magenta circle or outline around the region of possible conf
204. nd centerlines will be displayed Other Runway Runway on Selected for Airport Approach wn 108 08 117 95 JIBIS RWI7R nop ms 2 6m ems 171 136 975 118 000 con wae tO8 00 117 95 136 975 118 008 coe cor DME POR IDENT THREF NRST Figure 11 7 Airport Signs SPER we see amp T RA hil OBS CHI DHE KPOR IDENT THRREF NAST Figure 11 8 Airport Runways 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III hey SECTION 11 ADDITIONAL FEATURES Terrain SVS and TAWS Alerting Terrain alerting on the synthetic terrain display is triggered by Forward looking Terrain Avoidance FLTA alerts and corresponds to the red and yellow X symbols on the Inset Map and MFD map displays For more detailed information regarding Terrain SVS and TAWS refer to the Hazard Avoidance Section In some instances a terrain or obstacle alert may be issued with no conflict shading displayed on the synthetic terrain In these cases the contlict is outside the SVS field of view to the left or right of the aircraft TERRAIN Annunciation ew 183 08 136 975 118 888 com naz 198 88 11 136 975 8 088 cow Potential Terrain Impact Caution Points Figure 11 9 Terrain Alert Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Obstacles are represented on the synthetic terrain display by standard two dimensional tower symbols found on the Inset map and MFD maps
205. ne can be heard over the speaker or headsets during marker beacon reception When the tone is active pressing the MKR MUTE Key once mutes the audio but does not affect the marker an nunciator The audio returns when the next marker signal is received To turn off the marker beacon audio press the MKR MUTE Key once when there is no marker indication pres ent or press twice when an indication is present The key annunciator extinguishes when the marker beacon audio is turned off Inner Marker Figure 5 4 Marker Beacon Annunciators on the PFD Outer Marker Middle Marker Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity 190 00384 09 Rev A SECTION 5 AUDIO PANEL v v 5 6 INTERCOM SYSTEM ICS ISOLATION MKR HI MUTE SENS Press the PILOT and or COPLT Key to select who is isolated from hearing the Nav Com radios and music Figure 5 5 Marker Beacon Selection scenarios are addressed in Table 5 1 5 5 NAV RADIO AUDIO SELECTION Pressing DME ADF NAVI or NAV2 selects and o deselects the audio source and activates the annunciator Figure 5 7 ICS Isolation Selected audio can be heard over the headset and the speakers These four keys can be selected individually or together il Figure 5 6 Navigation Radios PILOT KEY COPLT KEY Pilot Hears Copilot Hears Passenger Hears Annunciator Annunciator Selected radios aural Selected radios aura
206. ng Flight Level seconds upon reaching 50 feet from the Selected Change Mode Altitude the autopilot transitions to Altitude Hold a Using the ALT Knob set the Selected Altitude Mode and levels the aircraft below the current aircraft altitude to an altitude in this case 9 400 feet at which to level off GPS AP VPTH between VNV flight plan altitudes 4 When the next TOD is reached Vertical Path Tracking b Press the FLC Key before the planned TOD becomes active may require acknowledgment to during an altitude hold while VPTH is armed allow descent path capture The Airspeed Reference defaults to the current aircraft airspeed Vertical Path Tracking and GPS AP AL TY Selected Altitude Capture Mode are armed 5 As the aircraft nears the VNV Target Altitude the automatically flight director transitions to VNV Target Altitude _ GPS LAP ALTS VPTH Capture Mode indicated by the green ALTV annunciation flashing for up to 10 seconds 2 Reduce power to allow descent in Flight Level Change Mode The autopilot maintains the es Fn ALT Airspeed Reference The green ALT annunciation flashes for up to 3 As the aircraft nears the Selected Altitude the flight 10 seconds upon reaching 50 feet from the VNV director transitions to Selected Altitude Capture Target Altitude the autopilot transitions to Altitude Mode indicated by the green ALTS annunciation Hold Mode and levels the aircraft at the vertical flashing for up to
207. nge Modes 190 00384 09 Rev A SECTION 1 SYSTEM OVERVIEW 1 2 PFD SOFTKEYS TERRAIN Softkey ON Softkey OFF optional SS e CN A TE VOR1 on HS VOR2 on HSI GPS on HSI SENDO A Figure 1 2 PFD Top Level Softkeys ji nn ry A A gt a m A iar op optional optional optional Emma breveod rex prone ano aes Press the BACK or OFF Softkey to return to the top level softkeys Figure 1 3 INSET Softkeys INSET Press to display the Inset Map in the lower left corner of the PFD OFF Press to remove the Inset Map DCLTR 3 Press momentarily to select the desired amount of map detail The declutter level appears adjacent to the DCLTR Softkey No declutter All map features are visible Declutter 1 Declutters land data Declutter 2 Declutters land and SUA data Declutter 3 Declutters large NAV data remaining removes everything except the active flight plan TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Press to display topographical data Q e coastlines terrain rivers lakes etc and elevation scale on the Inset Map TERRAIN Press to display terrain information on the Inset Map STRMSCP optional Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft 190 003
208. nob switches the tuning box light blue box between the COM1 and COM2 fields SECTION 1 SYSTEM OVERVIEW COM Frequency Transfer Key Transfers the standby and active COM frequencies Pressing and holding this key for two seconds automatically tunes the emergency frequency 121 5 MHz in the active frequency field COM VOL SQ Knob Controls COM audio level Pressing this knob turns the COM automatic squelch ON and OFF Audio volume level is shown in the field as a percentage Direct to Key Allows the user to enter a destination waypoint and establish a direct course to the selected destination specified by the identifier chosen from the active route or taken from the map pointer position FPL Key Displays the active Flight Plan Page for creating and editing the active flight plan or for accessing stored flight plans CLR Key DFLT MAP Erases information cancels an entry or removes page menus To display the Navigation Map Page immediately press and hold CLR MFD only Dual FMS Knob Used to select the page to be viewed only on the MFD The large knob selects a page group MAP WPT AUX NRST while the small knob selects a specific page within the page group Pressing the small knob turns the selection cursor ON and OFE When the cursor is ON data may be entered in the different fields using the small and large knobs The large knob is used to move the cursor on the page while the small knob is u
209. ns current aircraft roll attitude Limits bank to 22 Table 6 3 Roll Hold Mode Responses Changing the Roll Reference The roll reference can be changed by pressing the CWS Button establishing the desired bank angle then releasing the CWS Button Heading Select Mode Active Heading Select Mode HDG Heading Select Mode is activated by pressing HDG Key Heading Select Mode acquires and maintains the Selected Heading The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper left of the HSI Changing the Selected Heading NOTE Pressing the HDG Knob synchronizes the Selected Heading to the current heading The Selected Heading is adjusted using the HDG Knob on either display Pressing the CWS Button and hand flying the aircraft does not change the Selected Heading The autopilot guides the aircraft back to the Selected Heading upon release of the CWS Button Pitch Mode Active Selected Selected Heading Heading Bug Command Bars Track Selected Heading Figure 6 21 Heading Select Mode Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Turns are commanded in the same direction as Selected Heading Bug movement even if the bug is turned more than 180 from the present heading e g a 270 turn to the right However Selected Heading changes of more than 330 at a time result in turn reversals Navigation Mode GPS VOR LOC NOTE The selected
210. nt Alert 10 18 Presets 11 17 Procedure examples AFCS 6 24 6 31 Red pointer 2 3 Remove departure arrival or approach 8 6 Replies 4 5 Required Vertical Speed 2 6 7 16 Required Vertical Speed Indicator 7 16 Reversionary mode 5 1 12 1 ROC 10 13 10 15 10 18 10 21 13 5 Roll Hold Mode ROL 6 17 Roll modes flight director 6 17 6 20 Roll Reference 6 18 190 00384 09 Rev A RTC 10 15 10 18 RVSI 7 16 RX indicator 4 3 R indication 4 5 S Scheduler 11 18 Secure Digital SD card 1 12 11 20 Selected Altitude 6 6 6 10 6 13 Selected Altitude Capture Mode 6 6 6 10 6 13 Selected Course 6 20 6 21 Selected Heading 6 18 Selected vertical speed 2 7 Servos 6 22 Severe thunderstorm 10 5 SIGMET 10 5 Slip Skid indicator 2 3 Softkey function MFD 1 5 1 8 Speaker 5 2 Speed ranges 2 3 SQ 1 3 4 2 4 3 5 1 5 4 Squelch 5 4 STBY Softkey 4 4 Store Flight Plan 8 6 Stormscope lightning data 1 5 1 8 10 1 10 2 10 3 Strike 10 2 Strike mode 10 2 SVS 13 22 System annunciations 13 1 System message advisories 13 9 T TA 10 7 Tachometer 3 1 3 4 3 7 TAF 10 3 TAS 10 7 10 8 10 9 13 19 TAWS 10 11 10 16 10 17 10 18 10 20 10 21 10 22 13 5 13 6 TAWS B 10 16 INDEX TAWS system test 10 18 Temperature Peak Cylinder 3 7 Turbine Inlet 3 7 Terrain 10 11 12 2 Terrain 10 10 10 11 10 16 10 20 10 22 13 12 Timer 13 20 TIS 10 7 TNA Mute 10 7 TOD 7 15 7 16 7 19 Top
211. o place the cursor in the NEAREST VOR box 2 Turn either FMS Knob to select a VOR 3 Press the FMS Knob to remove the flashing cursor Select and Load a VOR Frequency 1 With the Nearest VOR Page displayed press the FREQ Softkey to highlight the VOR frequency in the FREQUENCY field 2 Press the ENT Key The selected VOR frequency is placed in the NAV standby frequency field 3 Press the FMS Knob to remove the flashing cursor 7 13 NEAREST USER WAYPOINT Figure 7 65 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fifth rectangular page icon Select a Nearest User Waypoint 1 With the Nearest User Waypoint Page displayed press the FMS Knob to activate the cursor If any previously entered User Waypoints are within 200 nm they are displayed with the closest listed first 2 Turn either FMS Knob to select the desired waypoint The remaining information on the Nearest User 1728 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Waypoint Page pertains to the selected Nearest User Waypoint 3 Press the FMS Knob to remove the flashing cursor 7 14 NEAREST FREQUENCIES 136 975 118 000 con NEAREST ARTCC Figure 7 66 Nearest Frequencies Page Select the Nearest Frequencies Page 1 Turn the large FMS Knob to select the NRST page
212. ob to highlight the desired transition waypoint and press the ENT Key The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 8 SECTION 9 PROCEDURES APPROACH CHANNEL CHANEL 90708 Figure 9 7 Selecting an Approach Transition The cursor moves to the MINIMUMS field If desired the decision altitude for the selected approach procedure may be entered and displayed on the PFD as described in the Barometric Altitude Minimums discussion in the Flight Instruments section Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO Press the ENT Key APPROGCH TRYSITION MINIMUMS PRIMARY FREQUENCY SEQUENCE A NMAN of Figure 9 8 Selecting Barometric Altitude Minimums Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 9 3 SECTION 9 PROCEDURES 9 4 9 The cursor moves to the altitude field Turn the small FMS Knob to enter the published decision altitude for the selected approach procedure Press the ENT Key SOFT PRIMARY FREQUENCY SEQUENCE ACMAN iof Figure 9 9 Entering Minimum Altitude 10 Turn the large FMS Knob to highlight Activate and press the ENT Key to activate the approach Activating the approach initiates a direct to for IAF and the G1000 immediately begins navigating to the IAF Selecting Load
213. ob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Nearest Airports Information on the PFD Bearing TO Distanc Airport Symbol NEAREST AIRPORTS U56 EE Er 9 3NM VFR MULTICOM 122 906 RNWY 35 FT KIDA amp 267 9 5NM ILS TOWER 118 500 RNWY 9001FT 20 11NM YOR 122 800 RNWY 42 FT Identifier Runway Length VDE ocac KRXE 4 352 UNICOM Primary COM Frequency Figure 7 61 Nearest Airports Window Press the NRST Softkey to display the PFD Nearest Air ports Window View Information on a Specific Airport in the List 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport identifier 2 Press the ENT Key to display airport information 3 Press the ENT Key again cursor is on BACK to return to the list Load an Airport COM Frequency into the Active COM 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport frequency shown in the window 2 Press the ENT Key and the selected frequency is placed in the COM standby frequency field 3 Press the Frequency Transfer Key to make the frequency the active trequency 190 00384 09 Rev A 7 10 NEAREST INTERSECTIONS 136 975 HEAREST DHT METT 4 1 NEAREST INTERSECTIONS NORTH UF Sa EERIE Ci MA Figure 7 62 Nearest Intersections Page Select the Nearest Intersections Page 1 Turn t
214. oo 10 2 SECTION 10 HAZARD AVOIDANCE STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 2 Press the MAP Softkey Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page 136 975 118 BRB com P NORTH ur rt LINING HODE CELL RATES TERRAIN Figure 10 4 In sae iain Map Page TE Stormscope Lightning Data Lightning Age Symbol Strike is less than 6 seconds old Q Strike is between 6 and 60 seconds old g Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Oos Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 1 SECTION 10 HAZARD AVOIDANCE At a map range of less than 25 nm Stormscope Stormscope Page lightning data is not displayed but can still be present The presence of Stormscope lightning data is indicated 1 Turn the large FMS Knob until the Map Page group by the annunciation LING lt 25 nm in the upper right is selected corner 2 Turn the small FMS Knob until the Stormscope NORTH UP Page is selected This is the third rectangular page icon STRMSCP MODE CELL 136 975 118 088 con a S
215. ope on approach e Go Around Automatically disengages the autopilot and commands a constant pitch angle and wings level while in the air Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 3 SECTION 6 AUTOMATIC FLIGHT CONTROL Table 6 1 lists the pitch modes with their corresponding controls and annunciations The mode reference shown with default measurement units is displayed next to the active mode annunciation for Altitude Hold Vertical Speed and Flight Level Change modes The NOSE UP NOSE DN Keys can be used to change the pitch mode reference while operating under Pitch Hold Vertical Speed or Flight Level Change Mode Reference Pitch Mode Control Annunciation Reference Range Change Increment Pitch Hold default Selected Altitude Capture j ALTS Altitude Hold ALT Key Vertical Speed VS Key 3000 to 1500 fpm 100 tom FLC P Vertical Path Tracking VNV Key VPTH VNAV Target Altitude m NITV Capture cepa APR Key Glideslope Go Around in air GA Switch ALTS is armed automatically when PIT VS FLC or GA is active and under VPTH when the Selected Altitude is to be captured instead of the VNAV Target Altitude ALTV is armed automatically under VPTH when the VNAV Target Altitude is to be captured instead of the Selected Altitude Table 6 1 Flight Director Pitch Modes 6 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 6 AUTOMATIC FLI
216. orz ALT 190 00384 09 Rev A SECTION 7 NAVIGATION 4 V4 is now entered into the flight plan c Turn the small FMS Knob to display the Waypoint a Press the FMS Knob to activate the cursor Information Window Enter the desired beginning int for V4 leg in thi le Topeka VOR b The desired entry point for V4 TOP must now be TOP o f nown in Figure 7 14 a entered Turn the large FMS Knob to highlight i the desired flight plan insertion point as shown eae in Figure 7 13 The V4 entry point TOP is placed Mi a immediately above the highlighted waypoint es SLN EE ACTIVE FLIGHT PLAN 4 46 MKC KCOS DTK DIS Departure KMKC ALL TIFTO2 1IFTO KOR i CEN KEI OPEKA TIFTO Enroute Airway V244 LAA DUMYE i 15ih LOCATION ERG 020 N CEN USA ssa N 3908 23 DIS 22 9NH M0953295 Press ENT to occept ORBE MN PROPTLE Figure 7 14 Entering V4 Entry Point d Press the ENT Key TOP is now inserted into the flight plan as in Figure 7 15 Figure 7 13 Begin Adding V4 to the Flight Plan ACTIVE FLIGHT PLAN KMKC KCOS OTK DIS ALT Departure KMKC ALL TIFTO2 TIFTO pigi Enroute TOP a Airway V244 LAA DUMYE GLIDE HYS So ARDC RANSO CURRENT VNU PROFILE ACTIVE VNV WPT FT aot YS TGT SS Fw VS REQ _ FPH TIME TO TOD Figure 7 15 TOP Inserted into the Flight Plan 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III i S
217. ossible descent profile recapture if the vertical deviation e Navigation source manually changed from GPS e CNCL VNV Softkey selected on the Active Flight oes B Plan Page MFD i Exceeds 200 it during ay overspeed condition e All remaining vertical waypoints deleted from the e Experiences a discontinuity exceeding 200 ft due to flight plan a flight plan change e Becomes invalid due to excessive cross track error track angle error e Displays entering Reversionary Mode 6 12 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A Non Path Descents Pitch Hold Vertical Speed and Flight Level Change modes can also be used to fly non path descents while VNAV flight control is selected If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to allow profile re capture GPs ALTS VPTH Figure 6 13 Flight Level Change VNV Non Path Descent To prevent immediate profile re capture the following must be satished e Atleast ten seconds have passed since the non path transition was initiated e Vertical deviation from the profile has exceeded 250 ft but is now less than 200 ft Pressing the VNV Key twice re arms Vertical Path Tracking for immediate profile re capture VNAV Target Altitude Capture Mode ALTV NOTE Armed VNAV Target Altitude and Selected Altitude capture modes are mutually excl
218. ot s Operating Handbook POH for fuel values and limitations The displayed fuel remaining can be adjusted up to 53 gal Models 172R 172S or 87 gal Models 182T T1827 206H T206H 190 00384 09 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS The System Display is accessed by pressing the ENGINE Softkey followed by the SYSTEM Softkey and shows critical engine fuel and electrical parameters Fuel calculations are based on the fuel flow totalizer and the displayed fuel remaining adjusted by the pilot using the following softkeys RST FUEL Resets totalizer based fuel remaining GAL REM to zero and the fuel used GAL USED to zero e GAL REM Gives access to softkeys for adjusting the amount of fuel remaining for purposes of fuel calculations Fuel remaining can be adjusted in one or ten gallon increments using the appropriate softkeys Softkeys also allow entering the full tank quantity for the aircraft or the tab quantity which is 35 gallons Models 172R and 172S or 64 gallons Models 182T T182T 206H and T206H Engine Manifold Pressure Gauge MAN IN Models 182 T182 206 T206 Displays engine power in inches of mercury in Hg Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range A white tick mark is displayed indicating the cruise manifold pressure Model T182 only 2 Tachometer RPM Shows propeller speeds in revolutions per minute rpm Re
219. oystick clockwise to display a larger area or rotate counter clockwise to display a smaller area If data is not received fora period longer than 6 seconds the age of the present data is displayed in the lower lett of the screen along with the annunciation that the system 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE has entered Coast Mode The system maintains the traffic display up to 60 seconds until the next data reception If no data is received after 60 seconds traffic is removed from the display Traffic Advisory aircraft is 1200 TNA Mute above amp climbing moving in the Traffic out of Traffic Mode Status direction of the line range THA HUTE STANDI r f P ER ATE Last data update Traffic at same altitude Proximity Traffic 1200 above is older than 6 level flight amp moving in the amp descending moving in the sec resulting in irection of the line direction of the line Coast Mode Figure 10 11 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is now displayed on the map TIS Voice Alert When a Traffic Advisory TA is displayed a voice alert Traffic is given Traffic Not Available is heard whenever TIS service becomes unavailable This alert can be muted by pressing the TNA MUTE Softkey TNA MUTE ON is displayed in the upper left of the disp
220. p database error exists MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists MFD1 DB ERR MFD1 terrain database missing The terrain database is present on another LRU but is missing on the specified PFD1 DB ERR PFD1 terrain database LRU missing MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced The MFD and or PFD detected a failure in the basemap database The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card It problem persists The G1000 system should be serviced Database Message Advisories Cont MFD1 DB ERR MFD1 obstacle database missing The obstacle database is present on another LRU but is missing on the specified PFD1 DB ERR PFD1 obstacle LRU database missing MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain da
221. p and preflight system tests as this may cause the preflight system test to fail or never to start if Preflight Test servos fail their power up tests Power must be cycled to the servos to remedy the situation Preflight system test failed aural alert sounds at failure 13 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A 13 5 TAWS ALERTS SECTION 13 ANNUNCIATIONS amp ALERTS The following table shows the possible TAWS alert types with corresponding annunciations and aural messages Alert Type Reduced Required Terrain Clearance Warn ing RTC Imminent Terrain Impact Warning ITI Reduced Required Obstacle Clearance Warning ROC Imminent Obstacle Impact Warning IO Reduced Required Terrain Clearance Caution RTC Imminent Terrain Impact Caution ITI Reduced Required Obstacle Clearance Caution ROC Imminent Obstacle Impact Caution IOI PFD MFD TAWS Page Annunciation Excessive Descent Rate Warning EDR PULL UP ue PULL UP PULL UP PUL UI PULL _UP MFD Pop Up Alert TERRAIN PULL UP Or TERRAIN AHEAD PULL UP TERRAIN AHEAD PULL UP or TERRAIN PULL UP OBSTACLE PULL UP or OBSTACLE AHEAD PULL UP OBSTACLE AHEAD PULL UP or OBSTACLE PULL UP Aural Message Pull Up Terrain Terrain Pull Up Pull Up or Terrain Ahead Pull Up Terrain Ahead Pull Up Terrain Ahead Pull Up Terrain Ahead P
222. perature Indicator TIT Models T182T and T206H Displays the temperature at the turbine inlet in degrees Fahrenheit F When the ASSIST Softkey is pressed the TIT deviation from peak APEAK is displayed below the indicator Exhaust Gas Temperature Bar Graph EGT F Displays the exhaust gas temperature of all cylinders in degrees Fahrenheit F a readout for the selected cylinder by default the hottest cylinder is shown below the bar graph The selected cylinder is indicated in light blue Cylinders whose EGTs are in the normal range appear in white For normally aspirated models pressing the ASSIST Softkey causes the EGT Garmin G1000 Cockpit Reference Guide for the Cessna Nav III deviation from peak APEAK for the selected cylinder to be displayed below the indicator Cylinder Head Temperature Indicator CHT Shows the head temperatures of all cylinders in degrees Fahrenheit F a readout for the selected cylinder by detault the hottest cylinder is shown below the bar graph The selected cylinder is indicated in light blue Cylinders whose CHTs are in the normal range appear in white Cylinders whose CHTs enter the warning ranges appear in red Fuel Quantity Indicator FUEL QTY GAL Shows the quantity of fuel in the left and right fuel tanks left L and right R When full the indicator displays to 35 gallons per side 26 gallons for the Models 172R and 172S 190 00384 09 Rev A A LLJ LL
223. play and can be displayed after viewing other EIS displays by pressing the ENGINE Softkey The EIS automatically defaults back to the Engine Display from the Lean or System Display when certain parameters are exceeded Fluctuations in engine speed and fuel quantity above certain levels depending on the airframe also cause reversion back to the Engine Display C Engine Manifold Pressure Gauge MAN IN Models 182T T182T 206H T206H Displays engine power in inches of mercury in Hg Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure 190 00384 09 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS range A white tick mark is displayed indicating the cruise manifold pressure Model T182T only Tachometer RPM Shows propeller speeds in revolutions per minute rpm Red range indicates propeller overspeed warning a white high rpm range indicates above normal operating speeds Models 172S 206H and T206H Model 172S When ascending through 5300 ft the upper end of the green arc displays 2600 rpm and ascending through 10 300 displays 2700 rpm When descending below 9700 ft the upper end of the green arc reutrns to 2600 rpm and descending below 4700 ft reutrns to 2500 rpm 3 Fuel Flow Indicator FFLOW GPH Shows the current fuel flow in gallons per hour gph For turbocharged aircraft the indicator displays a small stand alone green band indicating maximum takeoff
224. press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key 8 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 8 FLIGHT PLANNING 8 4 ACTIVATE A FLIGHT PLAN LEG Delete all vaya in Flight 1 From the Active Flight Plan Page press the FMS m E Knob to activate the cursor and turn the large Figure 8 7 Delete Flight Plan Confirmation FMS Knob to highlight the desired destination waypoint 8 6 INVERT ACTIVE FLIGHT PLAN 2 Press the ACT LEG Softkey using MFD only Or 1 From the Active Flight Plan Page press the MENU Key to display the Page Menu 2 Turn the large FMS Knob to highlight Invert Flight Plan and press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD 3 With Activate highlighted press the ENT Key 3 PAGE HEN OPT TONS ACTIVATE Shoes Flight Ply i Invert Flight Pion Figure 8 5 Activate Flight Plan Leg Confirmation 8 5 STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu window F
225. ptional 11 1 13 8 G1000 System Message Advisories 13 9 SV SO MCL STON surat credited el tates tareuuuia 11 1 MFD amp PFD Message AdVISOTICS cscessecseeseeseesen 13 10 OVS ROGUES sense caret coat aac liana aceasta uy 11 2 Database Message AdVISOFES c sscsceseeseseeseesen 13 11 PeO ON ceteentea niet ob ceeds oat ashe amt 11 9 GMA 1347 Message Advisories s s s 13 13 T2 Satela annann EA 11 10 GIA 63 Message Advisories ssssssiiirssrsssssssrersrrrrrers 13 13 11 3 ChartView 0 0 ccna 11 11 GIA 63W Message Advisories cescccscesecseesteeseeseen 13 15 Chat OOUOMS oeie narasesunsemanacaneumern 11 12 GEA 71 Message Advisories scesscesceseessesteeseeseen 13 18 Day Night VEW sgannan 11 13 GTX 33 Message Advisories 13 18 11 4 FliteCharts 0 11 14 GRS 77 Message AQVISOLOS sixidsscasinvessenveteaseiunnaeesein 13 19 Chat ODIS cenean 11 15 GMU 44 Message Advisories cesccscesecseesteeseeseen 13 19 DAVNO VW esan anan aa 11 15 GDL 69 69A Message Advisories cescecscesceeseeseeen 13 20 11 5 XM Radio Entertainment 11 16 GDC 74A Message Advisories 13 20 Usina X M RadiOsnasosinnnamacaen na 11 16 Miscellaneous Message AdVISOTI S c csceseeseeses 13 20 Automatic Audio MUtING cesceescestesstestesseestesseeseeaees 11 18 11 6 SCHOQUICN 5055 ts aseiiecrenindnmrrneaciimanicrsalnn 11 18 Da eae are rere eee nce 11 7 Electronic Checklists oo eee 11 20 190 00384 09 Rev A Garmin G1
226. quency Field Frequency Field 135 100 126 050 com 12 1 988 conz Frequency Transfer Arrow Tuning Box Figure 4 3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL PUSH VOL PUSH ID Knob SQ Knob vo_LPUsH E Fre Transfer K quency Transfer Key Dual NAV Dual COM Knob Knob Turn to tune in desired frequencies Press to change tuning box positions Figure 4 4 NAV COM Controls 4 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A 4 1 RADIO STATUS INDICATIONS RX When a COM signal is received a white RX appears by the active COM frequency during signal reception e TX When a COM radio is transmitting a white TX indication appears to the right of the corresponding COM frequency ID When the Morse code identifier is ON for a NAV radio a white ID indication appears to the left of the corresponding active NAV frequency The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel 121 900 118 600 com TX 118 400 conz Figure 4 5 Radio Status Indications 4 2 VOLUME VOLUME is displayed in place of the associated radio name i e COMI or NAV2 for two seconds after the volume level is last changed The percentage of maximum volume is displayed in place of the standby frequency selected by the tuning box 124 158 com VOLUME 135 675 357 Figure 4 6
227. r a TAWS B installation Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude 100 ft Threshold 1000 ft 10 16 Projected Flight Path Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Displaying Terrain on the TAWS Page 1 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS Page It desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 2 3 Potential Impact Point Unlighted Obstacle Terrain more than 1000 ft below the aircraft altitude 190 00384 09 Rev A 124 000 118 000 conz HDG UP Se view Figure 10 24 TAWS Page 360 View 124 000 118 000 conz HDG UP GPS ALT HSL 110 Figure 10 25 TAWS Page ARC View Enable Disable Aviation Data 1 While the TAWS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE 3 Press the ENT Key PAGE MENU Inhibit
228. r the Cessna Nav III SECTION 6 AUTOMATIC FLIGHT CONTROL 6 22 6 4 AUTOPILOT OPERATION NOTE Refer to the AFM for specific instructions regarding emergency procedures Cessna Nav IIIs autopilot operates flight control surface servos to provide automatic flight control The autopilot controls the aircraft pitch and roll attitudes following commands received from the flight director Pitch autotrim provides trim commands to the pitch trim adapter to relieve any sustained effort required by the pitch servo Flight Control Pitch and roll commands are provided to the servos based on the active flight director modes Servo motor control limits the maximum servo speed and torque The servo gearboxes are equipped with slip clutches set to certain values This allows the servos to be overridden in case of an emergency Pitch Axis and Pitch Trim The autopilot pitch axis uses pitch rate to stabilize the aircraft pitch attitude during upsets and flight director maneuvers Flight director pitch commands are rate and attitude limited combined with pitch damper control and sent to the pitch servo motor The pitch servo measures the output effort torque and provides this signal to the pitch trim servo The pitch trim servo commands the motor to reduce the average pitch servo effort When the autopilot is not engaged the pitch trim servo may be used to provide manual electric trim This allows the aircraft to be trimmed using
229. rammed Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 3 SECTION 11 ADDITIONAL FEATURES Descent and Approach Pathways are shown descending only for a programmed descent Figures 11 4 and 11 5 When the flight plan includes programmed descent segments pathways are displayed along the descent path provided that the selected altitude is lower than the programmed altitude During a Vectors to Final VTF approach transition pathways are displayed along the final approach course inbound to the Missed Approach Point MAP Pathways are shown level at the selected altitude or at the next programmed crossing altitude whichever is higher up to the point along the final approach course where the altitude intercepts the extended vertical descent path glidepath or glideslope Selected Altitude set for Enroute Selected Altitude set for Departure limbs NOT displayed by pathway Selected Altitude for Step Down Selected Altitude or Programmed Altitude From the vertical path descent glidepath or glideslope intercept point the pathways are shown inbound to the Missed Approach Point MAP along the published lateral and vertical descent path During an ILS approach the initial approach segment is displayed in magenta at the segment altitudes if GPS is selected as the navigation source on the CDI When switching to localizer inbound with LOC selected as the navigation source on the CDI pathw
230. reby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc Honeywell and Bendix King are registered trademarks of Honeywell International Inc CO Guardian is a trademark of CO Guardian Inc September 2008 190 00384 09 Rev A Printed in the U S A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III WARNINGS CAUTIONS amp NOTES B O O O WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being
231. rrent turn rate The end of the trend vector gives the heading predicted in six selected manually trom the MFD System Setup Page Za seconds based on the present turn rate At rates greater Flight Phase Automatic CDI Full scale than 4 deg sec an arrowhead appears at the end of the Deflection magenta trend vector and the prediction is no longer Departure DRPT sm Terminal TERM Jee Tek Mare E TEE Enroute ENR 2 0 nm Standard Turn R FE Trend Vector Oceanic OCN I 33 j Rate Tick Mark rate gt 4 The CDI scale automatically adjusts to the current deg sec Approach LNAV 1 0 nm decreasing to 350 feet Approach LNAV V depending on variables see Figure 2 19 Turn Rate Indicator and Trend Vector WAAS systems only Figure 2 23 Approach LNAV 1 0 nm decreasing to a specitied Turn Bate VNAV WAAS only course width then 0 3 nm Trend Vector Approach depending on variables see LPV WAAS only Figure 2 24 Missed Approach standard rate Figure 2 20 Standard Rate Turn Indication Course Pointer The course pointer is a single line arrow GPS VORI and LOC1 or double line arrow VOR2 and LOC2 which points in the direction of the set course Figure 2 21 Course Pointer 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 9 SECTION 2 FLIGHT INSTRUMENTS 2 O D 5 E 5 E r 2 q o E T O N a T z Refer to accompanying roe
232. rt if servos fail their power up tests Power must be cycled to the servos to remedy the situation Preflight system test failed aural alert sounds at failure Table 6 4 AFCS Status Field Alerts Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Overspeed Protection Overspeed protection is provided in situations where the flight director cannot acquire and maintain the vertical Mode Reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed When an autopilot overspeed condition occurs the Airspeed Reference appears in a box above the Airspeed Indicator flashing a yellow MAXSPD annunciation Engine power should be reduced and or the pitch reference adjusted to slow the aircraft The annunciation disappears when the overspeed condition is resolved Airspeed Indicator Figure 6 41 Overspeed Annunciation 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 35 SECTION 6 AUTOMATIC FLIGHT CONTROL Blank Page 6 36 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 7 NAVIGATION The majority of the following discussions pertain to the Multi Function Display In discussions pertaining to the PFD the controls are located on the PFD 7 4 NAVIGATION MAP PAGE WARNING The map display should only be used for situational awareness
233. s displayed on the TERRAIN SVS Page as a yellow or red X Imminent Terrain Impact ITI and Imminent Obstacle Impact IOI This provides alerts when the aircraft is below the elevation of terrain in the aircrafts projected path ITI and IOI alerts are accompanied by a potential impact point displayed on the TERRAIN SVS Page as a yellow or red X The alert is given when the projected vertical flight path is calculated to come within minimum clearance altitudes in the following table Descending During the final approach phase of flight RTC ROC ITIIOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0 5 nm of the approach runway or is below 125 feet AGL while within 1 nm of the runway Lighted Obstacle Height is greater than 1000 AGL Potential Impact Points Figure 10 23 Terrain SVS Symbols 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 10 HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP Softkey Press the TERRAIN Softkey Terrain and obstacle proximity are now displayed on the map 2 TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured fo
234. s from light blue to amber in color Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Echo Top Cloud Top and Echo Top Mutually Exclusive st e UE minutes SIGMETSIAIRMETs oo City Forecasts w CountyWarnings f 6 CydoneWarmings f 6 Freezing Leves fo oo r Surface Analysis fo oo mes Cid WindsAloft wo ms CT o Oo O Clouds Tops 190 00384 09 Rev A 10 4 TRAFFIC SYSTEMS e If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Softkey are displayed e Ifa Traffic Advisory System TAS is configured a STANDBY NORMAL TEST and ALT MODE Softkey are displayed e If an ADS B traffic system is configured only the ALT MODE Softkey is displayed Traffic Information Service TIS A NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site A NOTE If the G1000 is configured to use a Traffic Advisory System TAS TIS is not available for use Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the second rectangular page icon 3 Press the OPERATE Softkey to begin displaying traffic OPERATIING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the J
235. s the ENT Key The UP DOWN field is now highlighted Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it must be reset manually Press the CLR Key or the TMR REF Softkey to remove the window SECTION 2 FLIGHT INSTRUMENTS Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 13 SECTION 2 FLIGHT INSTRUMENTS Blank Page Ja Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS NOTE Refer to the Pilot s Operating Handbook POH for limitations EIS information is presented in three displays accessed using the ENGINE Softkey on the MFD The 172R 172S 182T 206H T182T and T206H dis play the following Engine Display Default display shows all critical engine fuel and electrical indicators Lean Display Provides engine leaning information System Display Shows numeric readouts of critical engine fuel and electrical indicators Green and white bands indicate normal ranges of operation yellow and red bands indicate caution and warning respectively If sensory data to an instrument becomes invalid or unavailable a red X is shown across the instrument 3 1 ENGINE DISPLAY The Engine Display is the detault EIS dis
236. scheck NERO I SE With other NAVS GPS integrity is insufficient for the current phase of flight The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced ai oe nme A DIG Loss of GPS navigation due to insufficient satellites navigation Insufficient satellites ae a D 7 ehh Loss of GPS navigation due to position error navigation Position error at ae ee a da Loss of GPS navigation due to GPS failure navigation GPS fail AP OAN ORA DE EROA Vertical guidance generated by WAAS is unavailable use LNAV only minimums downgraded TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav Change HDG reference to TRUE angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may GPS2 SERVICE GPS2 needs service still be available The G1000 system should be serviced Return unit for repair ASORTATA A Abort approach due to loss of GPS navigation navigation Abort approach 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 17 SECTION 13 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories Cont NAV1 SERVICE NAV1 needs service Return unit for repair A failure has been detected in t
237. second level softkeys 2 Press the ALT UNIT Softkey 3 Press the METERS Softkey to display altitude in meters 4 Press the HPA Softkey to display the barometric setting in hectopascals Press the IN Softkey to display the barometric setting in inches of mercury 5 Press the BACK Softkey to return to the previous level softkeys Figure 2 9 Altimeter Metric SECTION 2 FLIGHT INSTRUMENTS Low Altitude Annunciation A NOTE The LOWALT annunciation is only available in G1000 systems configured with WAAS capable GPS Also the LOW ALT annunciation is not available when the G1000 is configured with TAWS Terrain Awareness amp Warning System unless TAWS is inhibited When the Final Approach Fix FAF is the active waypoint in a GPS WAAS approach using vertical guidance a LOW ALT Low Altitude annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed altitude at the FAE The annunciation initially flashes After a few seconds the flashing stops and the annunciation is displayed as shown in Figure 2 10 Low Altitude Annunciation 29 921N Figure 2 10 Low Altitude on GPS Approach 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 5 SECTION 2 FLIGHT INSTRUMENTS 2 6 2 4 VERTICAL DEVIATION GLIDEPATH GLIDESLOPE INDICATOR The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior
238. sed to select individual characters for the highlighted cursor location When the G1000 displays a list that is too long for the display screen a scroll bar appears along the right Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 1 SYSTEM OVERVIEW side of the display indicating the availability of additional items within the selected category Press the small FMS Knob to activate the cursor and turn the large FMS Knob to scroll through the list MENU Key Displays a context sensitive list of options This list allows the user to access additional features or to make setting changes that relate to certain pages 15 PROC Key Selects approaches departures and arrivals from the flight plan If a flight plan is used available procedures for the departure and or arrival airport are automatically suggested If a flight plan is not used the desired airport and the desired procedure may be selected This key selects IFR departure procedures DPs arrival procedures STARs and approaches IAPs from the database and loads them into the active flight plan ENT Key Accepts a menu selection or data entry This key is used to approve an operation or complete data entry It is also used to confirm selections and information entries 17 Dual ALT Knob Sets the selected altitude in the box located above the Altimeter The large knob selects the thousands while the small knob selects the hundreds
239. ses the selected navigation receiver deviation and desired course inputs to fly the approach Approach Mode provides greater sensitivity for signal tracking than Navigation Mode Pressing the APR Key when the CDI is greater than one dot arms the selected approach mode annunciated Garmin G1000 Cockpit Reference Guide for the Cessna Nav III in white to the lett of the active roll mode If the selected navigation receiver is GPS pressing the APR Key arms GPS Approach Mode provided that a GPS approach has been loaded into the flight plan If the loaded approach provides WAAS based vertical guidance Glidepath Mode is also armed Figure 6 16 If GPS Approach Mode is selected while in GPS Navigation Mode capture can occur with crosstrack error of up to 2 nm GPS ROL ALT Figure 6 24 Navigation Approach Mode Armed LOC Approach Mode allows the autopilot to tly a LOC ILS approach with a glideslope LOC Approach Mode is armed along with Glideslope Mode see Figure 6 17 when the APR Key is pressed and either of the following have been done e Navigation source is set to LOC e A LOCALS approach is loaded into the flight plan and the corresponding localizer frequency tuned even if the selected navigation source is GPS Localizer capture is suppressed until the navigation source is changed to LOC If Approach Mode is active and either of the following occur the flight director reverts to Roll Hold Mode wings rolled level e V
240. sessesseesen 7 3 7 3 Navigating an Example Flight Plan 7 5 7 4 Airport Information 0 0 eee 7 22 7 5 Intersection Information 0 0 0 cccee 7 24 7 6 NDB Information 0 ccccccsee eee 7 24 7 7 VOR Information 0 c seen 7 25 7 8 User Waypoint Information Page 7 25 7 9 Nearest Airports 0 0 ccs 7 25 Nearest Airport Information on the MFD cssesee 7 25 Nearest Airports Information on the PFD 1 26 7 10 Nearest Intersections ccccsesssesen 1 21 7 11 Nearest NDB cesses 1 21 7 12 Nearest VOR 1 28 7 13 Nearest User Waypoint 0 cccceeeen 7 28 7 14 Nearest Frequencies 0 c cccsssseeeseeen 1 29 7 15 Nearest Airspace ccc 7 29 SECTION 8 FLIGHT PLANNING 0000000000 8 1 8 1 User Defined Waypoints 0 cc cess 8 1 Select the User WPT Information Page scseseseeen 8 1 Create User Waypoints from the Navigation Map Page 8 2 8 2 Viewing the Active Flight Plan 8 2 8 3 Activate a Stored Flight Plan 8 2 8 4 Activate a Flight Plan Leg 0 0 8 3 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan ee 8 3 8 7 Create a New Flight Plan 8 4 Create a New Flight Plan Using the MFD sss 8 4 Create a New Flight Plan Using the PFD uo 8 4 8 8 Enter an Airway in
241. speed OPTN 3 Wind direction arrow with direction and speed OFF Information not displayed DME optional Press to display the DME Information Window 1 6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A BRG bearing Press to cycle through the following Nav sources making the pointer the indicator for the corresponding source and displaying the appropriate information NAVI Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 Information Window GPS Displays GPS waypoint identifier and GPS distance information in the BRG1 Information Window ADF Displays ADF in the BRGI Information Window when an otional ADF is installed OFF Removes the BRG1 Information Window HSI FRMT Press to display the HSI formatting softkeys 360 HSI Press to display the HSI in a 360 degree format SECTION 1 SYSTEM OVERVIEW NAV2 Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window GPS Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window ADF Displays ADF in the BRG2 Information Window when an otional ADF is installed OFF Removes the BRG2 Information Window ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled displays altimeter in meters IN Press to display the BARO setting as
242. ss to select Altitude Reporting Mode GND Press to select Ground Mode VFR Press to automatically squawk 1200 only in the U S A refer to ICAO standards for VFR codes in other countries CODE Press to display transponder code selection softkeys 0 7 0 through 7 Press numbers to enter code IDENT Press to provide special aircraft position identification to Air Traffic Control ATC BKSP Press to remove numbers entered one at a time BACK Press to return to the previous level softkeys IDENT Press to provide special aircraft position identification to Air Traffic Control ATC BACK Press to return to the previous level softkeys ALERTS Press to display the Alerts Window IDENT Press to provide special aircraft position identification to Air Traffic Control ATC TMR REF Press to display the Timer References Window NRST Press to display the Nearest Airports Window ALERTS Press to display the Alerts Window 1 3 MFD SOFTKEYS ENGINE Pressing this softkey makes available the LEAN and SYSTEM Soitkeys which in turn access the Lean Page and the System Page respectively MAP Pressing this softkey enables the following softkeys TRAFFIC Pressing this softkey displays removes Traffic on the Navigation Map TOPO Pressing this softkey displays or removes topographic information on the Navigation Map TERRAIN Pressing this softkey displays removes terrain and obstacle data on
243. st is checked the next highlighted item is Go to the next checklist Press the ENT Key to advance to the next checklist displayed Press the EXIT Softkey or hold down the CLR Key momentarily to exit the Checklist Page and return to the page last viewed SECTION 11 ADDITIONAL FEATURES GRouP TAKEOFF CHECKLIST TAKEOFF NORMAL TAKEOFF Wing Flaps 2 Throttle Control Mixture Control 4 Elevator Contro 2 FULL RICH Above 3000 fe EH ENG e e 6 Wing Flaps SHORT FIELD TAKEOFF Wing Flaps 2 Brakes Throttle Contro l gt Brakes ture Control FULL RICH Above 3000 fe i Elevator Contro ele ara 2 el eE jel el eB 2 AC lans C 56 KIAS funtil all obstacles a SLOWLY v 10 degrees 10 degrees preferred FULL et elevation lean for maximum RPM LIFT NOSE WHE EL at 55 KIAS f0 80 KIAS ETRACT at safe altitude mum RPM RELEAS SLIGHT TAIL LOVY et elevation lean for max e cleared yhen airspeed is more than 60 KIAS Figure 11 31 Sample Checklist 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 11 ADDITIONAL FEATURES Immediately accessing emergency procedures 1 From any page press the CHKLIST Softkey 2 Press the EMERGCY Softkey GRouP EMERGENCY PROCEDURES 172S CHECKLIST ENGINE FAILURE ENGINE FAILURE DURING TAK
244. sted Airspace With the Nearest Airspace Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to scroll through the list highlighting the desired airspace Press the ALERTS Softkey to place the cursor in the AIRSPACE ALERTS field Turn either FMS Knob to select the desired airspace Press the FMS Knob to remove the flashing cursor View and Quickly Load the Frequency for a Controlling Agency 1 With the Nearest Airspace Page displayed press the FREQ Softkey to place the cursor in FREQUENCIES field Turn either FMS Knob to select the desired frequency Press the ENT Key to load the frequency into the COM frequency standby field Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 8 FLIGHT PLANNING The following discussions pertain to the Multi Function Display unless otherwise indicated 8 1 USER DEFINED WAYPOINTS 136 975 118 000 cwe ee Figure 8 1 User WPT Information Page Select the User WPT Information Page 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the fifth rectangular page icon Create a New User Waypoint 1 With the User Waypoint Information Page displayed press the NEW Softkey A waypoint is created at the current aircraft position 2 Turn the small FMS Knob to enter first character of the waypoint n
245. sted to view a small area chart descent profile strip of the chart pressing the FIT WIDTH Softkey changes the chart size to fit the available screen width WPT APPROACH INFORHAT TON E KPOK APPROACH ILS RWY 20L 51 1 Day Night View ChartView can be displayed on a white or black background for day or night viewing The Day View offers a better presentation in a bright environment Selecting Day Night or Automatic View roxe 991 a 1 While viewing a terminal chart press the MENU ipee Eie aes fete es 7 eg Tasot A Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to move to the COLOR SCHEME Option MINIMUMS FIT WOTH a PAGE MENU Figure 11 20 Approach Information Page Profile View OPTIONS Show Info Page Pressing the MINIMUMS Softkey displays the She Doare Piae minimum descent altitude visibility strip at the bottom of Show Approach Page the approach chart Show Weather Puge WPT APPROACH INFORMATION AIRPORT KPDOK APPROACH ILS RWY 28L 51 1 Chart Mode OFF Chart Setup Go Back To Previous Page Press the FMS CRSR knob to return to base page STRAIGHT TN LANDING RW ZOL CIRCLE TO LAND ns LOE IG CHART SETUP FULL SCREEN lt On COLOR SCHEME DA 15 307 CHAMISE 5 tharted chairections Press the FMS CRSR knob to return to base page Figure 11 21 Approach Information Page
246. t Reference Guide for the Cessna Nav III 190 00384 09 Rev A Terrain Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert Inhibit TERRAIN SVS While the TERRAIN SVS Page is displayed press the INHIBIT Softkey TER INHB is annunciated in the lower right of portion of the screen Enable TERRAIN SVS If TERRAIN SVS has been inhibited from the TERRAIN SVS Page press the INHIBIT Softkey The TER INHB annunciation is removed NOTE If TERRAIN SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Forward Looking Terrain Avoidance FLTA The Forward Looking Terrain Avoidance alert is composed of two sub functions Reduced Required Terrain Clearance RTC and Reduced Required Obstacle Clearance ROC This provides alerts when the aircraft flight path is above terrain and or obstacles yet is projected to come within minimum clearance values outlined in the following table Unlighted Obstacle Height is less than 1000 AGL Lighted Obstacle Height is less than 1000 AGL 1000 AGL Unlighted Obstacle Height is greater than SECTION 10 HAZARD AVOIDANCE When an RTC or ROC alert is issued a potential impact point i
247. tabase Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 11 SECTION 13 ANNUNCIATIONS amp ALERTS Database Message Advisories Cont MFD1 DB ERR MFD1 airport terrain database missing The airport terrain database is present on another LRU but is missing on the PFD1 DB ERR PFD1 airport terrain specified LRU database missing MFD1 DB ERR MFD1 Sate Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists MFD1 DB ERR MFD1 Chartview The MFD and or PFD detected a failure in the ChartView database optional database error exists feature Ensure that the data card is properly inserted Replace data card It problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts The MFD and or PFD detected a failure in the FliteCharts database optional database error exists feature Ensure that the data card is properly inserted Replace data card It problem persists The G1000 system should be serviced The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced DB MISMATCH Aviation database The PFD and MFD have different aviation database versions installed Crossfill is
248. th a bug corresponding to the Airspeed Reference along selecting Flight Level Change Mode the tape a Engine power must be adjusted to allow the autopilot to fly the aircraft at a pitch attitude corresponding to the 6 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Airspeed Reference and the desired flight profile climb or descent The flight director maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not allow the aircraft to climb or descend away from the Selected Altitude Changing the Airspeed Reference The Airspeed Reference shown in both the AFCS Status Box and above the Airspeed Indicator may be adjusted e Using the NOSE UP NOSE DN Keys By pressing the CWS Button hand tlying the aircraft to a new airspeed then releasing the CWS Button to establish the new Airspeed Reference Selected Altitude Flight Level Change Airspeed Capture Mode Mode Active Reference Armed Airspeed Airspeed Reference Reference Airspeed Reference Bug Command Bars Indicate Climb to Attain Selected Altitude Figure 6 9 Flight Level Change Mode 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 9 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Navigation Modes VPTH ALTV NOTE Pressing the CWS Button while Vertical Path Tracking Mode is activ
249. the TMR REF Softkey to display the Timer Reterences Window 2 Turn the large FMS Knob to place the cursor in the Flight ID field 3 Turn the small FMS Knob to enter the desired first character 4 Turn the large FMS Knob to place the cursor in the next desired field 5 Turn the small FMS Knob to enter the next desired character 6 Repeat steps 4 and 5 until the desired Flight ID is entered 7 Press the ENT Key updating is displayed as the Flight ID is loaded into the system 4 6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 5 AUDIO PANEL SECTION 5 AUDIO PANEL oM com ae Receiver Audio Disabled Passenger Address Disabled on 72R S TD Cabin Speaker Marker Beacon Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio Optional disabled if ADF and or DME Aircraft Navigation Radio Audio are not installed Disabled Manual Squelch T Digital Clearance Recorder Play Key w CREW wv PILOT COPLT ICS Isolation ICS ISOLATION PILOT O PASS VOL SQ VOL Annunciation SQ Annunciation Reversionary Mode DISPLAY BACKUP Figure 5 1 Front Panel Controls 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 5 1 SECTION 5 AUDIO PANEL Jz 5 1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter i e microphone The associ
250. the aircraft symbol on the CDI as shown in Figure 12 4 Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD 190 00384 09 Rev A SECTION 12 ABNORMAL OPERATION Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of accurately tracking your estimated position and consequently the system may display a path that is different than the actual movement of the aircratt Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Figure 12 4 Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following e Navigation Status Box fields except Active Leg TAS and DTK e GPS Bearing Pointer e Wind data and pointers in the Wind Data Box on the PFD
251. the desired altitude the new altitude is established as the Altitude Reference 190 00384 09 Rev A If the Selected Altitude is reached during CWS maneuvering the Altitude Reference is not changed To adjust the Altitude Reference in this case the CWS Button must be pressed again after the Selected Altitude is reached Altitude Hold Mode Active SECTION 6 AUTOMATIC FLIGHT CONTROL Altitude Reference BRG Command Bars Hold Pitch Attitude to Maintain Altitude Reference Selected Altitude Figure 6 7 Altitude Hold Mode Vertical Speed Mode VS In Vertical Speed Mode the flight director acquires and maintains a Vertical Speed Reference Current aircraft vertical speed to the nearest 100 fpm becomes the Vertical Speed Reference at the moment of Vertical Speed Mode activation Vertical Speed Mode does not consider the relative position of the Selected Altitude in relation to the current aircraft altitude at the time of mode activation so it is possible to use Vertical Speed Mode while not climbing descending to the Selected Altitude 190 00384 09 Rev A Vertical Speed Mode is activated by pressing the VS Key the VS annunciation appears in the AFCS Status Box to indicate the active pitch mode along with the Vertical Speed Reference to the right The Vertical Speed Reference is also displayed above the Vertical Speed Indicator A Vertical Speed Reference Bug corresponding to the Vertical Speed Refere
252. tion of the following items Annunciation Window The Annunciation Window displays abbreviated annunciation text Text color is based on alert levels described later in the Alert Levels Definitions section The Annunciation Window e System Annunciations Typically a large red X appears in windows when a failure is detected in the is located to the right of the Altimeter and Vertical LRU providing the information to the window see Speed Indicator on the display All Cessna Nav III the G1000 System Annunciations section for more annunciations can be displayed simultaneously in information the Annunciation Window A white horizontal line e Audio Alerting System The G1000 system issues separates annunciations that are acknowledged from audio alert tones when specific system conditions are annunciations that are not yet acknowledged Higher met See the Alert Levels Definitions section for more priority annunciations are displayed towards the top information of the window Lower priority annunciations are displayed towards the bottom of the window Alerts Window The Alerts Window displays alert text messages Up to 64 prioritized alert messages can be displayed in the Alerts Window Pressing System ESS the ALERTS Softkey displays the Alerts Window Eo Pressing the ALERTS Softkey a second time removes the Alerts Window from the display When the Alerts Window is displayed the pilot can use the large FMS Knob to scroll through
253. tions Certain limitations exist regarding the NEXRAD radar displays Some but not all are listed here NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics hail vs rain etc An individual NEXRAD site cannot depict high altitude storms at close ranges and has no information about storms directly over the site The resolution of displayed NEXRAD data is 4 square kilometers Therefore when zoomed in on the display each square block is 2 kilometers on each side The intensity level reflected by the square is the highest level sampled within the square area ECHO TOP Press the ECHO TOP Softkey to show the location elevation and direction the highest radar echo This may not indicate the top of a storm or clouds only the highest radar return echo ECHO TOPS cannot be displayed along with NEXRAD and CLOUD TOPS When ECHO TOPS is activated NEXRAD and CLOUD TOPS are removed Refer to the Legend for a description of the ECHO TOPS coding The display is updated every 7 5 minutes CLD TOP Press the CLD TOP Softkey to show the cloud top altitude determined from satellite imagery The display is updated every 15 minutes LING Pressing the LING Softkey shows the location of cloud to ground lightning strikes The display is updated every five minutes NOTE Strikes depicted represent cloud to ground strikes within a 2 kilometer radius of the actual strik
254. tity of fuel used in gallons based on fuel flow time in hours the engine has been in service since last reset 6 Vacuum Pressure Indicator VAC Models 182 T182 206 T206 Displays vacuum pressure Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS Cruise Manifold N HAN IN w 15 0 Pressure PH R 2 fHE o 2000 50 0 100 OIL PSI 57 4 OIL F 200 ENG AHAH HRS VAC N FUEL CALC FFLOW GPH 6 0 GAL USED 0 8 GAL REM A FUEL TY GAL me Y Hh 16 76 30 F ELECTRICAL M BUS OLD OOOOH ENG 4085 3 HRS VAC C FUEL CALC FFLOW GPH 4 8 GAL USED 4 6 GAL REM FUEL QTY GAL A a 6 16 76 30 F ELECTRICAL ee OCOD OOOO 11 2 5 VOLTS 2 6 11 24 5 VOLTS 24 5 M BATT 5 M BATT S 12 4 0 AMPS AO 12 6 6 AMPS AO Model T182T Model T206H Figure 3 6 System Display Turbocharged Aircraft Set Fuel Remaining GAL REM Shows 11 Voltmeter M E BUS VOLTS Displays the current fuel remaining in gallons as set by the main and essential bus voltages pilot and adjusted for fuel burn since last set 12 Ammeter M S BATT AMPS Shows the Fuel Quantity Indicator FUEL QTY GAL main and standby battery load in amperes Shows the quantity of fuel in the tanks in gallons ranging from zero to full F for each fuel tank left L and right R Wh
255. to executing an approach see Figure 2 11 In systems that are WAAS enabled the Glidepath Indicator appears at a point prior to the FAF when executing an LPV LNAV VNAYV or LNAV V approach see Figure 2 12 VNAV Target Altitude Vertical Deviation Indicator a Required Vertical Speed 29 9 51N Figure 2 11 Vertical Deviation Indications Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Glidepath Indicator Figure 2 12 Glidepath Indicator The Glideslope Indicator appears when an ILS is tuned in the active NAV receiver field selected for display on the HSI and the aircraft heading is within 105 of the approach course see Figure 2 13 Marker Beacon Annunciation Glideslope Indicator Figure 2 13 Glideslope Indicator 190 00384 09 Rev A 2 5 MARKER BEACON ANNUNCIATIONS Outer Marker Middle Marker Inner Marker p 0 Altimeter 1800 Figure 2 14 Marker Beacon Annunciations 2 6 VERTICAL SPEED INDICATOR Selected Vertical Speed Vertical Speed Bug Vertical Speed Pointer Figure 2 15 Vertical Speed Indicator The actual vertical speed is displayed inside the pointer When the Flight Director is placed in Vertical Speed Mode by pressing the VS Key the Vertical Speed Bug is displayed Press the NOSE UP or NOSE DN Key to adjust 190 00384 09 Rev A SECTION 2 FLIGHT INSTRUMENTS 2 7 BAROMETRIC ALTITUDE MINIMUMS The desired barometric altitud
256. uational awareness and should not be used independent of the CDI VDI glide path indicator and glide slope indicator They are removed from the display when the selected navigation information is not available Pathways are not displayed beyond the active leg when leg sequencing is suspended and are not displayed on any portion of the flight plan leg that would lead to intercepting a leg in the wrong direction Departure and Enroute Prior to intercepting an active flight plan leg pathways are displayed as a series of boxes with pointers at each corner that point in the direction of the active waypoint Pathways are not displayed for the first leg of the flight plan if that segment is a Heading to Altitude leg The first segment displaying pathways is the first active GPS leg or active leg with a GPS overlay If this leg of the flight plan route is outside the SVS field of view pathways will not be visible until the aircraft has turned toward this leg While approaching the center of the active leg and prescribed altitude the number of pathway boxes decreases to a minimum of four Pathways are displayed along the flight plan route at the highest of either the selected altitude or the programmed altitude for the leg Climb profiles cannot be displayed due to the variables associated with aircraft performance Flight plan legs requiring a climb are indicated by pathways displayed at a level above the aircraft at the altitude selected or prog
257. uide for the Cessna Nav III 10 19 SECTION 10 HAZARD AVOIDANCE Pop up Alerts When a terrain or obstacle alert is issued a pop up window is displayed on the MFD with the appropriate alert 118 808 118 000 conz NORTH UP Figure 10 30 TAWS Alert Pop Up Press the ENT Key to display the TAWS Page or press the CLR Key to remain on the existing page Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Potential Impact Points Height is less than Height is less than Height is greater than Height is greater than 1000 AGL 1000 AGL 1000 AGL 1000 AGL Figure 10 31 TAWS Symbols 10 20 Garmin G1000 Cockpit Reference Guide for the Cessna Nav Ill 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert Excessive Descent Rate Warning EDR PULL UP Pull Up Reduced Required Terrain Clearance PULL UP Terrain Terrain Pull Up Pull Up Warning RTC or or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact Warning ITI PULL UP Terrain Ahead Pull Up Terrain Ahead Pull Up or or TERRAIN PULL UP Terrain Terrain Pull Up Pull Up Reduced Required Obstacle Clearance PULL UP Obstacle Obstacle Pull Up Pull Up Warning ROC or OF Obstacle
258. ull Up or Terrain Terrain Pull Up Pull Up Obstacle Obstacle Pull Up Pull Up or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Obstacle Ahead Pull Up Obstacle Ahead Pull Up or Obstacle Obstacle Pull Up Pull Up Caution Terrain Caution Terrain or Terrain Ahead Terrain Ahead Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Caution Obstacle Caution Obstacle or Obstacle Ahead Obstacle Ahead Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Altitude Callout 500 Excessive Descent Rate Caution EDR TERRAIN see DOTSIK eae melons TOO LOW TERRAIN Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 13 5 Negative Climb Rate Caution NCR 190 00384 09 Rev A None None Five Hundred Sink Rate Don t Sink or Too Low Terrain SECTION 13 ANNUNCIATIONS amp ALERTS The following system status annunciations may also be issued PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert TAWS System Test Fail TAWS FAIL TAWS System Failure No GPS position or excessively degraded TAWS N A None TAWS Not Available GPS signal TAWS Available will be heard when sufficient GPS signal is re established System Test pass TAWS System Test OK 13 6 OTHER G1000 AURAL ALERTS Aural Alert The aircraft has descended b
259. unavailable and the approach downgrades Glidepath Mode is disarmed When vertical guidance becomes available again Glidepath Mode is automatically re armed under GPS Approach Mode Glideslope Mode GS e LOC Approach Mode is armed the APR Key is pressed and either LOC is the selected navigation source or a LOC ILS approach is loaded into the flight plan see LOC Approach Mode LOC HDG AP ALT 10000r7 GS Geeta oss hn oni FE ee ek Figure 6 18 Glideslope Mode Armed NOTE Pressing the CWS Button while Glideslope Mode is active does not cancel the mode The autopilot guides the aircraft back to the glides lope upon release of the CWS Button Once the localizer has been set as the navigation source the localizer and glideslope can be captured Upon reaching the glideslope the flight director transitions to Glideslope Mode and begins to intercept and track the glideslope Active ILS Approach Mode Glideslope Frequency Tuned Active Mode Active navid12 18 116 9HIIXD DUS faf RW36 mdp DIS 4 6nm BRG 356 gt ah aa a nav2 1 14 95 357 A a F l 7 Suan a ec A Command Bars Indicate Descent on Localizer Glideslope Path NAV2 localizer is Selected Navigation Source Glideslope l l Indicator Figure 6 17 Glideslope Mode 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 15 SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around GA Mode Pushing the GA Swit
260. unway or is below 125 feet AGL while within 1 nm of the runway Premature Descent Alert PDA A Premature Descent Alert is issued when the system detects that the aircraft is significantly below the normal approach path to a runway The PDA alert mode functions only during descent to land PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0 5 nm from the runway threshold OR is at an alti tude of 125 feet AGL while within 1 nm of the threshold During the final descent algorithms set a threshold for alerting based on speed distance and other parameters Height Above Terrain Feet Runwa 1 2 3 4 5 6 7 8 9 10 11 h z A k Distance From Destination Airport nm 12 13 14 15 Figure 10 27 PDA Alerting 190 00384 09 Rev A SECTION 10 HAZARD AVOIDANCE Excessive Descent Rate Alert EDR The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing descending upon terrain at an excessive speed Figure 10 28 displays the correlation between height above terrain and descent rate resulting in the two EDR alerts EDR alerts have two levels of severity caution sink rate and warning pull up DON T SINK Height Above Terrain Feet E a 0 20 40 60 80 100 120 140 Altitude Loss Feet 6000
261. uration memory The G1000 system should be serviced MANIFEST GTX1 software The transponder has incorrect software installed The G1000 system should be mismatch communication halted serviced XPDR1 SRVC g ane needs service The 1 transponder should be serviced when possible Return unit for repair XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A GRS 77 Message Advisories SECTION 13 ANNUNCIATIONS amp ALERTS AHRS1 TAS AHRS1 not receiving valid airspeed AHRS1 GPS AHRS1 using backup GPS source AHRS1 GPS AHRS1 not receiving any GPS information AHRS1 GPS AHRS1 not receiving backup GPS information AHRS1 GPS AHRS1 operating exclusively in no GPS mode AHRS1 SRVC AHRS1 Magnetic field model needs update GEO LIMITS AHRS1 too far North South no magnetic compass MANIFEST GRS1 software mismatch communication halted GMU 44 Message Advisories Message HDG FAULT AHRS1 magnetometer fault has occurred HDG FAULT AHRS2 magnetometer fault has occurred MANIFEST GMU1 software mismatch communication halted 190 00384 09 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III The 1 AHRS is not receiving true airspeed trom the air data computer The AHRS relies on GPS information to augment the lack of a
262. usion Any map page that displays the navigation view can also show the SateTaxi airport layout within the maximum configured range During ground operations the aircrafts position is displayed in reference to taxiways runways and airport features When panning over the airport features such as runway holding lines and taxiways are shown at the cursor 8 80 a5 TK TRK E 118 200 con 19 80 sro HAP NAVIGATION HAP a HAP T DCLIR SHW CHRT Figure 11 13 SafeTaxi Depiction on the Navigation Map Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Configuring SafeTaxi range 1 2 3 4 5 6 1 8 While viewing the Navigation Map Page press the MENU Key to display the PAGE MENU Turn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Key PAGE MENU OPTIONS Press the FMS CRSR knob to return to base page Figure 11 14 Navigation Map PAGE MENU Turn the FMS Knob to select the Aviation Group and press the ENT Key Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI Turn the small FMS Knob to display the range of distances Turn either FMS Knob to select the desired distance for maximum SafeTaxi display range Press the ENT Key to complete the selection Press the FMS Knob to return to the Navigation Map Page 190 00384 09 Rev A MAP SETUP GROUP ACTIVE FPL ACTIVE FPL WPT LARGE APT MEDIUM APT SMALL APT SAFET
263. usive However Selected Altitude Capture Mode is armed implicitly not annunciated whenever VNAV Target Altitude Capture Mode is armed This ensures the Selected Altitude is not violated during a change from VNAV Target Altitude Capture to Selected Altitude Capture Mode close to Selected Altitude interception VNAV Target Altitude Capture is analogous to Selected Altitude Capture Mode and is armed automatically after the VNV Key is pressed and the next VNAV Target Altitude is to be intercepted before the Selected Altitude The annunciation ALTV indicates that the VNAV Target Altitude is to be captured VNAV Target Altitudes are shown in the active flight plan or vertical direct to and can be entered manually 190 00384 09 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL or loaded from a database see the Navigation section for details At the same time as TOD within 1 minute is annunciated in the Navigation Data Box the VNAV Target Altitude is displayed above the Vertical Speed Indicator see Figure 6 12 VNAV Target Altitudes can be modified until VNAV Target Altitude Capture Mode becomes active As the aircraft nears the VNAV Target Altitude the flight director automatically transitions to VNAV Target Altitude Capture Mode with Altitude Hold Mode armed This automatic transition is indicated by the green ALTV annunciation flashing for up to ten seconds and the appearance of the white ALT annunciation The VNAV T
264. version mismatch Xtalk is off off Install correct aviation database version in all displays DB MISMATCH Aviation database The PFD and MFD have different aviation database types installed Americas type mismatch Xtalk is off European etc Crosstill is off Install correct aviation database type in all displays DB MISMATCH Terrain database The PFD and MFD have different terrain database versions installed Install version mismatch correct terrain database version in all displays DB MISMATCH Terrain database The PFD and MFD have different terrain database types installed Install correct type mismatch terrain database type in all displays DB MISMATCH Obstacle database The PFD and MFD have different obstacle database versions installed Install version mismatch correct obstacle database version in all displays DB MISMATCH Airport Terrain The PFD and MFD have different airport terrrain databases installed Install database mismatch correct airport terrain database in all displays 13 12 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 09 Rev A SECTION 13 ANNUNCIATIONS amp ALERTS GMA 1347 Message Advisories GMA1 FAIL GMA1 is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA1 CONFIG GMA1 contig error The audio panel configuration settings do not match backup configuration Contig
265. visual annunciations 100 ft 100 ft of the system perform the following steps 1 While the TAWS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS Page When all is in working order TAWS System Test OK is heard Forward Looking Terrain Avoidance FLTA The Forward Looking Terrain Avoidance alert is composed of two sub functions Reduced Required Terrain Clearance RTC and Reduced Required Obstacle Clearance ROC This provides alerts when the aircraft flight path is above terrain and or obstacles yet is projected to come within minimum clearance values outlined in the following table When an RTC or ROC alert is issued a potential impact point is displayed on the TAWS Page as a yellow or red X Imminent Terrain Impact ITI and Imminent Obstacle Impact IOI This provides alerts when the aircraft is below the elevation of terrain in the aircrafts projected path ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS Page as a yellow or red X The alert is given when the projected vertical flight path is Garmin G1000 Cockpit Reference Guide for the Cessna Nav III During the final approach phase of flight RTC ROC ITI IOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0 5 nm of the approach r

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