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Garmin Software Version 0563.05 Cockpit Reference Guide

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1. 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III RR 1 RECORD OF REVISIONS Revision Date of Revision affected Pages RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 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 cece 1 10 1 6 Backlighting 0 0 0 ccc cscs ees 1 12 1 7 XM Radio Automatic Muting 0 1 12 1 8 Database Updates seen 1 12 Jeppesen Aviation Database cccesessesesereesen 12 Garmin Data aSCS icsactaseht d atcnanssenohvestenenaarahasticns 1 13 SECTION 2 FLIGHT INSTRUMENTS 00000 2 1 2 1 Airspeed Indicator 2 3 Speed NACAs A 2 3 Speed RM Eanan e O 2 3 Airspeed Trend VeCtOr v sssssessessecsesseesseesecsesseeaseesees 2 3 Vspeed Referentes corinae 2 3 2 2 Attitude Indicator 0 0 0 2 3 23 AIIM CD eetesiicscscncirccanecmienonnnenunnewn 2 4 Selected Altitude BUG c scssssssessessecsessessnesseesean 2 4 Altitude Trend Vector susene 2 4 Barometric Setting BOX ssssccsssectariensusvedsneesnevedehsensdtubirecds 2 4 Altitude Alei aaien a 2 4 Metric Display iarna 2 5 Low Altitude ANNUNClatiOn cesccssceseesseseesseseeseeseen 2 5 2 4 Vertical Deviation Glidepath Glideslope I
2. 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 C OM1 PTT COM1 push to talk ke eia P The COM1 and or COM2 external push to talk switch is stuck in the enable or gt PTT COM push kk pressed position Press the PTT switch again to cycle its operation a g PUSA IORASKEN iffe problem persists the G1000 system should be serviced C OM1 RMT XFR COM1 remote J P eed ia transfer key is stuck The COM1 and or COM2 transfer switch is stuck in the enabled or pressed posi tion Press the transter 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 with other NAVS i sa Pol J o POEME Loss of GPS navigation due to insufficient satellites tion Insufficient satellites Loss of GPS integrity monitoring T AAY eae a Ee oe Loss of GPS navigation due to position error navigation Position error ae ae eel B A Loss of GPS navigation due to GPS failure navigation GPS fail 12 1
3. TERM Terminal is the current CDI flight phase displayed on the HSI indicating 1 0 nm CDI scaling ACTIVE FLIGHT PLAN 136 975 118 688 conz NORTH UP X TFR KMKC KCOS NO DATA DTK DE ALT Deporture KMKC ALL TIFTO2 TIFTO MCI TIFTO 287 66 9NH aa Enroute SLN Airvoy Y HYS Airwoy V263 TBE TRE Arrivol KCOS TBE DBRY1 ALL CURRENT VNV PROFILE ACTIVE VNV WPT VS TOGT __ PH FPA i Q F 0 TO TERRAIN VS REQ PH TIME T y V DEV SESA j 100r1 i 1000r1 yee 30nn Figure 7 11 Assigned Heading of 240 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 FPL ACTIVE FLIGHT PLAN 136 975 118 000 conz Eisa ilai pt ACTIVE FLIGHT PLAN TFR KMKC KOS HI DATA OTK DIS Deporture KHKC ALL TIFTOATIFTO MCI TIFTO 2a S75NH Enroute SLN is Airwoy W2e44JLAd HYS r TLI F j LAA 251 es F ao f a Airway 263 1BE Li TBE 210 sn g Arrival KCOS TBE DBRY1 ALL TARE Kansas CITY CURRENT WW PROFILE ACTIVE Wi WPT FT at VS TGT TERAATH 10pFT Figure 7 12 Assigned Heading of 290 7 6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 4 V4 is now entered into the flight plan a Press the FMS Knob to activate the cursor b The desired entry point for V4 TOP must now be entered Turn the large FMS Knob to highlight the desired flight plan insertio
4. The HSI compass can be displayed as a 360 rose or 140 arc by pressing the PFD Softkey followed by the 2 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III HSI FRMT Soitkey followed by the 360 HSI or the ARC HSI Softkey A Turn Rate Indicator 2 Ground Track Bug G Lateral Deviation Scale Navigation Source G 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 08 Rev A Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote halt standard and standard turn rates A magenta turn rate trend vector shows the current turn rate The end of the trend vector gives the heading predicted in six seconds based on the present turn rate At rates greater than 4 deg sec an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid Half Standard Turn Rate Tick Mark Tra Rae Standard Turn Me Tend Vector Rate Tick Mark rate gt 4 deg sec Turn Rate Trend Vector 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
5. Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION 7 22 Select an Airport from the Active Flight Plan 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Turn the small FMS Knob to the left to display a list of flight plan airports as shown in Figure 7 52 AIRPORT EMCI Figure 7 52 Flight Plan Airport List 3 Turn the large FMS Knob to select the desired airport 4 Press the ENT Key Select a Nearest Airport 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Turn the small FMS Knob to the left Initially a flight plan airport list is displayed as in Figure 7 52 The list is populated only when navigating a flight plan AIRPORT Figure 7 53 Nearest Airport List 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 53 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 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 small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 52 The list is populated only when navigating a flight plan 3 Turn the small FMS Knob to the right to dis
6. KCOS FPL ACTIVE FLIGHT PLAN NORTH UP TFR NO DATA 118 888 conz IQOBET DTK DIS FSHER PYNON aT pE autt tT Approach KCOS RNAV 35Rees LPV HABUK iof FALUR CEGIX fof RH SR aap 6368F1 MOGAL mahp CURRENT VNV PROFILE ACTIVE VV WPT __ VS TGT VS REO V DEV TERRAIN 100Ff1 Lack po 1000F I A 15m CNCL VNV Figure 7 49 Establishing the Holding Pattern 27 The aircraft maintains 10 000 feet while following the magenta line through the hold as in Figure 7 50 FPL ACTIVE FLIGHT PLAN 136 975 118 688 conz asiluk ACTIVE FLIGHT PLAN i TER KMKC KOOS NO DATA WILS DIS FSHER py RESET PYNON yaya hee Approach KCOS RNAV 35Rees LPV HABUK jaf FALUR CEGIX fof RHSSR aap 6368FT MOGAL sahp CURRENT VNV PROFILE aA oy TERRAIN 1009F 1000F7 i A 15nn Figure 7 50 Hold Established 190 00384 08 Rev A RUNWAYS BIL 19R gt HARD SURFACE FULL TIME FREQUENCIES Figure 7 51 Airport Information Page Select 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 first rectangular page icon Initially information for the airport closest to the aircraft s present position is displayed Select an Airport from the Database 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Enter the desired airport identifier
7. 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 Trattic Mode field 5 Rotate the Joystick 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 08 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 G climbing moving in the Traffic out of Traffic Mode Status direction of the line range 17185 HAP TRAFFIC HAP 136 975 118000 cone OPERATING me aren a ae HOG UP TNA MUTE OFF RAP T SCTE i OPERATE Ee Last data update wili at same altitude Proximity Traffic 1200 above TREC COAST AGE DOT 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 Traffi
8. 813 STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MED 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 JAFRE pa 2 a a KOH O re orl Figure 8 18 Airway Added to Flight Plan 8 9 LOAD A DEPARTURE Figure 8 19 Store Flight Plan Confirmation 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 8 6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 8 14 EDIT A STORED FLIGHT PLAN 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 190 00384 08 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
9. CANCEL and press the ENT Key 8 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 8 FLIGHT PLANNING 8 4 ACTIVATE A FLIGHT PLAN LEG Knob to activate the cursor and turn the large Figure 8 7 Delete Flight Plan Confirmation 1 From the Active Flight Plan Page press the FMS FMS Knob to highlight the desired destination waypoint 8 6 INVERT ACTIVE FLIGHT PLAN 2 Press the ACT LEG Softkey using MFD only 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 Or 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 Als KIAH Course 236 from KOJC to KIAB ACTIVATE or CANCEL 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 Figure 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 t
10. FSHER Hz JSHH 10CAOFT PY NOM 352 11 51 TRQERET Agprooch KOOS RNAY 35Riaes LPY Bt HABUK iaf S Si soad FALUR 251 S 0NH 8600r1 CURRENT WHV PROFILE ACTIVE UNU WET TOOOOFT ot OPSHH Jr VS TGT 7S5FPH FPA 30 VS REG Figure 7 35 Adjusting the Descent c Press the ENT Key SECTION 7 NAVIGATION 15 As seen in Figure 7 36 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 37 FPL ACTIVE FLIGHT PLAN 136 975 118 000 conz Biisit ri ACTIVE FLIGHT PLAH TFR KEKE KEOS HO DATA v WES TBE TBE AE P Arrival ECOS TBE DBRY1 ALL OPSHH 3MM fol BRANA TEREFT OPSHN 253 JONA TOCAOFT FSHER a2 JENA TOCOOFT PYHNOH 352 11 5mm BGRRFT Approoch KOOS RNAY 35Rigrs LPY HABUK iaf BT S SN 30001 FALUR 251 S NM 8600r1 CURRENT VNV PROFILE ACTIVE VA WPT TOOOGOFT at OPSHN Jhh VS TGT BSRFPH FPA 25 TERRAIN VS REO iDDFT pl 1000Ft aN j 30m i D VIEH AW PROF CHOL VV YHV fe SHW CHRT Figure 7 36 Approaching Top of Descent TOD 136 975 136 975 E Target Altitude Vertical J Deviation Devt Required da ma Vertical Speed Indicator RVSI Figure 7 37 VDI amp RVSI Upon Reaching Top of Descent TOD 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Ces
11. Figure 2 21 Course Pointer 190 00384 08 Rev A SECTION 2 FLIGHT INSTRUMENTS Course Deviation Indicator CDI The CDI scale automatically adjusts to the current phase of flight as seen in Figure 2 22 Scaling may be selected manually from the MFD System Setup Page Flight Phase Automatic CDI Full scale Deflection Approach LNAV Approach LNAV V WAAS systems only Approach LNAV VNAV WAAS only 1 0 nm decreasing to 350 feet depending on variables see Figure 2 23 1 0 nm decreasing to a specitied course width then 0 3 nm Approach depending on variables see LPV WAAS only Figure 2 24 Missed Approach Garmin G1000 Cockpit Reference Guide for the Cessna Nav Ill 2 9 SECTION 2 FLIGHT INSTRUMENTS xe O D 2 E E E oO z 2 qA o E T O mN Te T Refer to accompanying N P 2 approach CDI scaling figures 3 F LL Aas O 4 J i Enroute Missed o Departure Terminal Oceanic if gt 200 nm Terminal Approach l AACR from nearest airport p pp O Drawing not to scale Figure 2 22 Phases of Flight CDI Scaling O 5 CDI scale is set to the smaller of 0 3 nm S E or an angle set by the system _ dD D E 2 x c T O 5 2 2 angle based S m pe angle set 3 5 a on database 9 a by system ol I information z 4 C j A LO e e iT FAF Jo FAF Landing Threshold d O CDI scale varies if Vectors To Final is activated CDI sca
12. MANUAL then press the ENT Key 5 With the intensity value now highlighted turn the 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 SETUP MENU AUTO 23 477 e f PFD DSPL MFD DSPL Figure 1 10 PFD Setup Menu Window 1 7 XM RADIO AUTOMATIC MUTING XM Radio audio is automatically muted when the aircraft groundspeed exceeds approximately 30 kts and the airspeed is less than approximately 80 kts The audio must be manually unmuted once the aircraft is outside the applicable speed range Refer to the G1000 Optional Equipment section of the pilots guide Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 1 8 DATABASE UPDATES The G1000 System uses Secure Digital SD cards to load and store various types of data For basic flight op erations SD cards are required for database storage as well as Jeppesen aviation and ChartView database updates 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 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
13. 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 08 Rev A Load and or Activate an Approach Procedure 1 2 3 4 5 6 190 00384 08 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 Figure 9 6 Selecting an Approach Procedure Turn either FMS Knob to highlight the desired approach Press the ENT Key 1 8 SECTION 9 PROCEDURES The cursor moves to the TRANSITIONS field Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key The Vectors option assumes vectors
14. 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 SECTION 2 FLIGHT INSTRUMENTS Within 2500 ft Within 100 ft Barometric Minimum Bug Barometric Minimum Box BARO MIN 3U 041N Figure 2 17 Barometric Minimum Descent Altitude Alerting Visual Annunciations Set the barometric altitude minimums 1 Press the TMRIREF Softkey 2 Turn the large FMS Knob to highlight the Minimums field Figure 2 16 3 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 4 Use the small FMS Knob to enter the desired altitude from zero to 16 000 feet 5 To remove the window press the CLR Key or the TMRIREF Softkey 2 8 HORIZONTAL SITUATION INDICATOR HSI
15. 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III the altitude is now designated to give vertical speed and 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 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 deviatio
16. 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 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 08 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
17. the FMS Knob to activate the cursor 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 We Press the ENT Key to view the information The Figure 7 55 Intersection Information Page following may be displayed with the frequency Access Information on an Intersection e TX transmit only e RX receive only PT part time frequency 1 With the Intersection Information Page displayed press the FMS Knob to activate the cursor 4 Press the ENT Key to place the selected frequency 2 Enter an intersection identifier and press the ENT in the standby field of the COM or NAV box Key 5 To remove the cursor press the FMS Knob 3 a FMS Knob to remove the flashing 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 793 SECTION 7 NAVIGATION 7 6 7 24 NDB INFORMATION HOATH UP s ITKE Hre Mg Fa Fa i LEI Figure 7 56 NDB Information Page Select the NDB Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the third rectangular page icon View Information on a Specific NDB 1 2 3 4 With the NDB Information Page displayed press the FMS
18. the autopilot will not couple to GPS and both TAWS and Terrain Proximity 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 11 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 190 00384 08 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS 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 combination of the following items e 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 is located to the right of the Altimeter and Vertical Speed Indicator on the display All Cessna Nav III annunciations can be displayed simultaneously in the Annunciation Window A white horizontal line separates annunciations that are acknowledged from annunciations that are not yet acknowledged Higher priority annunciations are displayed towards the top 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 the ALERTS Softkey displays
19. 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 ns Ey is 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 sate XPOR 6943 SITBY ENT BACK I ALERTS A 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 o LET Figure 4 13 ON Mode 190 00384 08 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 sai Sa T 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 th
20. 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 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 9 10 1 10 2 10 3 Strike 10 2 Strike mode 10 2 System annunciations 12 1 System message advisories 12 9 190 00384 08 Rev A T TA 10 7 Tachometer 3 1 3 4 3 8 TAF 10 3 TAS 10 7 10 8 10 9 12 19 TAWS 10 11 10 13 10 15 10 17 12 5 12 6 TAWS B 10 11 TAWS system test 10 13 Temperature Peak Cylinder 3 7 Turbine Inlet 3 7 Terrain 10 10 10 11 10 15 10 17 11 2 12 12 TIS 10 7 TNA Mute 10 7 TOD 7 15 7 18 Top of Descent 7 15 Tornado 10 5 Trattic advisory 10 7 10 8 10 9 10 17 Traffic map page 10 7 10 8 10 9 10 11 10 14 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 1 3 4 3 7 Turbine Inlet Temperature TIT 3 7 TX 4 3 7 23 U Unlighted obstacle 10 15 V Vacuum Pressure 3 1 3 8 VDI 7 15 7 16 Vertical Descent Indicator 7 15 Vertical Deviation 2 2 2 6 Vertical deviation guidance 1 10 1 11 Vertical navigation 1 10 1 11 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III INDEX Vertical Navigation flight control 6 10 6 14 Vertical Path Tracking Mode 6 10 6 11 6
21. 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 Flight Level Change Airspeed Altitude Hold Mode Active Reference Mode Armed mavi 115 50 113 80 ane de ee 133 888 con nav2 188 08 117 95 123 800 135 325 conz Airspeed Reference stoner SNA ri L Gang Airspeed Reference Bug Fi ae m 4400 z 4300 4g 41270 4000 E 39A Figure 6 9 Flight Level Change Mode 190 00384 08 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 active 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 se
22. Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 1 SYSTEM OVERVIEW GPS Displays GPS waypoint identifier and GPS XPDR Press to display the transponder mode distance information in the BRG2 Information selection softkeys Window STBY Press to select Standby Mode ADF Displays ADF in the BRG2 Information ON Press to select Mode A Window when an otional ADF is installed ALT Press to select Altitude Reporting Mode OFF Removes the BRG2 Information GND Press to select Ground Mode Window VFR Press to automatically squawk 1200 only ALT UNIT Displays softkeys for setting the in the U S A refer to ICAO standards for VFR altimeter and BARO settings to metric units codes in other countries METERS When enabled displays altimeter in CODE Press to display transponder code selection meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals soltkeys 0 7 0 through 7 Press numbers to enter code IDENT Press to provide special aircraft position identification to Air Traffic Control STD BARO Press to set the barometric pressure ATC to standard pressure BKSP Press to remove numbers entered one BACK Press to return to the previous level softkeys ala NE ALERTS Press to display the Alerts Window BACK Press to return to the previous level softkeys OBS Press to select OBS
23. DME ee Reece ALERTS A Traffic Annunciation BRG2 Information Window 2 Vspeed References ee anaes Barometric Minimums Box G Selected Heading Box Selected Altitude Bug Wind Data Window G Inset Map 6 BRGI Information Window Selected Course Box Barometric Minimums Bug Vertical Deviation Glidepath WAAS en 7 DME Information Window abled systems only Glidesope Indicator Marker Beacon Annunciation O OOOO0O Figure 2 2 Additional PFD Information an Distance to Next Active Flight Plan Leg Waypoint Bearing to Next Waypoint DIS BRG Figure 2 3 PFD Navigation Status Box 1I Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 2 1 AIRSPEED INDICATOR Vspeed References Actual Airspeed 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 displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration deceleration is mai
24. 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 206 and T206 G Oil Pressure OIL PSI Displays pressure of the oil supplied to the engine in pounds per square inch psi 4 Oil Temperature OIL F Displays the engine oil temperature in degrees Fahrenheit F 5 Engine Hours Tach ENG HRS Models 182 T182 206 T206 A numeric readout gives the time in hours the engine has been in service 6 Vacuum Pressure Indicator VAC Models 182 T182 206 T206 Displays vacuum pressure T Fuel Flow FFLOW GPH Shows the current fuel flow in gallons per hour gph Calculated Fuel Used GAL USED Shows quantity of fuel used in gallons based on fuel flow since last reset 9 Set Fuel Remaining GAL REM Shows current fuel remaining in gallons as set by the pilot and adjusted for fuel burn since last set Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Fuel Quantity Indicator FUEL QTY GAL Shows the quantity of fuel in the tanks in gallons ranging from zero to full F for each fue
25. Knob to activate the cursor Turn the large FMS Knob to highlight the desired selection field identifier name or closest city Enter an identifier name or city and press the ENT Key Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Figure 7 57 VOR Information Page Select the VOR Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the fourth rectangular page icon Access Information on a VOR 1 2 3 4 5 With the VOR Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired selection field identifier name or closest city Enter an identifier name or city and press the ENT Key The FREQUENCY field is now highlighted If desired press the ENT Key to place the frequency in the NAV receiver standby field Press the FMS Knob to remove the flashing cursor 190 00384 08 Rev A 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 136 975 118 000 con EAREST AIRPORTS Figure 7 58 Nearest Airports Page Nearest Airport Information 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 fir
26. 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 TO UPDATE THE AVIATION DATABASE FROM TO WORLDWIDE WORLDWIDE 0584 0605 13 APR 2006 11 MAY 2006 11 MAY 2006 48 JUN 2006 NO WILL BE ASSUMED IN 8 SECONDS Figure 1 11 Database Update Prompt 3 Press the ENT Key to start the database update A prompt similar to the following is displayed 190 00384 08 Rev A DO YOU WANT TO UPDATE THE AVIATION DATABASE FROM TO REGION WORLDWIDE WORLDWIDE EYELE 0584 0605 EFFECTIVE 13 APR 2006 11 MAY 2006 EXPIRES 11 MAY 2006 48 JUN 2006 NO WILL BE ASSUMED IN 8 SECONDS UPDATING AVIATION DATABASE PLEASE WAIT UPDATED TRIVES SULCESSEURL YT 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 Verify 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 iden tical database versions must be kept in each display unit A NOTE The data contained in the terrain and obstacle databases comes from government agencies G
27. Map ADS B Traffic Optional ADS B is limited to displaying traffic in the G1000 Operation is similar to the TAS system discussed previously with the exception of symbology The following traffic symbols are used to display traffic with the ADS B system 190 00384 08 Rev A SECTION 10 HAZARD AVOIDANCE Traffic Advisory with directional information Points in the direction of the intruder aircraft track Traffic Advisory without directional information Traffic Advisory out of the selected display range Displayed at outer range range ring at proper bearing Non threat traffic with directional information Points in the direction of the aircraft track Non threat traffic with no directional information Traffic located on the ground with directional information Points in the direction of the aircraft 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 when 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 Traffic with directional information but positional accuracy is degraded Points in the direction of the aircraft track Aircraft Identification tail number Relative Altitude or Flight ID in this case 1200 number e feet a
28. Mode on the CDI when navigating by GPS only available with active leg CDI Press to change navigation mode on the CDI between GPS VORI and VOR2 DME optional Press to display the DME Tuning Window 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 optional RE 0 ve E TRE S J ALERTS Mnononnnn w nae A L Ii sy f on acr_ _eno_J _ver_J cope went Back Jfarerrs nonnnoniarnenieniaAnk iw Press the BACK Softkey to return to the top level softkeys Lo Woe es Wos ies IE e JL 7 Jf mer JL ekse back J acerrs SnNnonNnNnnNAMAAnAnNnNAnNNA DND Press the BACK Softkey to return to the top level softkeys Figure 1 5 XPDR Transponder Softkeys 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III ey SECTION 1 SYSTEM OVERVIEW IDENT Press to provide special aircraft position MAP Pressing this softkey enables the following identification to Air Traffic Control ATC softkeys TMR REF Press to display the Timer References TRAFFIC Pressing this softkey displays removes Window Traffic on the Navigation Map NRST Press to display the Nearest Airports TOPO Pressing this softkey displays or removes Window topographic information on the Navigation Map ALERTS Press to display the Alerts Window TERRAIN
29. PROF CHOL VV YNV fe SHH CHRT Figure 7 33 Loaded Approach 13 Note the altitude constraints associated with each of the approach waypoints as seen in Figure 7 33 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 7 14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 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 34 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 r ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS ALT FSHER 352 9 8mm 10000FT PYNON 352 11 9mm 10000FT Approach KCOS RNAV 35RGPs LPV HABUK iof 821 5 9M 9000F1 FALUR 261 5 0NH 8600 CEGIX fof 351 GON 7800F1 RW3S5R aap 351 5 1NH 6368FT 348 B 4NH 6370r
30. Waypoint an Information Page is displayed and the LD AIRWY Po Softkey is now available f Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7 16 ENTRY TOR AIRWAY J60 O77 Ne 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 are displayed the prompt LOAD highlighted as in Figure 7 18 LOAD Figure 7 16 List of Available Airways for TOP ENTRY TOF 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 pem points is now displayed as in Figure 7 17 I TOP m EIER Vy fal SLN 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 08 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 R TIFTO Enroute TOP 196 32 3NM __FT Airway V4 SLN SLN 260 97 7NH Airway 244 LAA HYS 22 TIN LAA 251 Airway 263 TBE CURRENT VNV PROFILE ACTIVE VUNU WPT VS TGT VS REQ 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 ac
31. 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 Flash up to 10 sec Indicating Automatic Transition GPS EY 3000Fr 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 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 for details Glidepath Mode GP NOTE Pressing the CWS Button while Glidepath Mode is active does not cancel the mode The autopilot guides the aircraft back to the glidepath upon release of the CWS Button GPS Approach Mode Active naval 18 98 114 10 Suc nav2 113 88
32. airport and ends when the aircraft is Reduced Required Terrain Clearance RTC and either 0 5 nm from the runway threshold OR is at an alti Reduced Required Obstacle Clearance ROC tude of 125 feet AGL while within 1 nm of the threshold This provides alerts when the aircraft flight path During the final descent algorithms set a threshold for is above terrain and or obstacles yet is projected to alerting based on speed distance and other parameters come within minimum clearance values outlined in the following table When an RTC or ROC alert is issued a The Forward Looking Terrain Avoidance alert is composed of two sub functions potential impact point is displayed on the TAWS Page as a yellow or red X S E Imminent Terrain Impact ITI and Imminent S Obstacle Impact IOI This provides alerts when the aircraft is below the elevation of terrain in the aircrafts projected path ITI and et cnn Destinnton Aint Istance From Destination IOI alerts are accompanied by a potential impact point displayed on the TAWS Page as a yellow or red X The Figure 10 21 PDA Alerting alert is given when the projected vertical flight path is 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 13 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
33. and above below the Vertical Speed Indicator flight director continuously monitors Selected Altitude may 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 By pressing the CWS Button hand flying the the Selected Altitude shown above the Altimeter The aircraft to attain a new Vertical Speed Reference 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 Reterence Flight Level Change Mode FLC in the AFCS Status Box The Airspeed Reference is also displayed directly above the Airspeed Indicator along with a bug corresponding to the Airspeed Reference along the tape Engine power must be adjusted to allow the autopilot to fly the aircraft at a pitch attitude corresponding to the Airspeed Reference and the desired flight profile climb or NOTE The Selected Altitude should be set before selecting Flight Level Change Mode 6 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL 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
34. and the speakers These four keys can be selected individually or together Figure 5 6 Navigation Radios PILOT KEY COPLT KEY l Pilot Hears Copilot Hears Passenger Hears Annunciator Annunciator Selected radios aural Selected radios aural 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 08 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 v v MAN T CREW WS 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 transmiss
35. at the Decision height and land the aircraft SPOIN AVN Sd9 e Use the GA Switch to execute a missed approach Figure 6 38 LPV Approach to KCOS 6 32 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A Go Around Missed Approach NOTE As a result of calculations 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 full power to execute a missed approach The flight director Command Bars establish a nose up climb to follow 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 SS GAD EAP SS ALTS 2 Start the climb to the prescribed altitude in the published Missed Approach Procedure in this case 10 000 ft a Press the AP Key to re engage the autopilot b If navigating an ILS approach press the CDI Softkey to select GPS as the navigation source c Press the NAV Key to have the autopilot fly to the hold _ GPS AP ALTS 3 Use the ALT Knob to set a Selected Altitude to hold To hold the current airspeed during the climb press the FLC Key As the aircraft nears the Selected Altitude the flight director transiti
36. closing descending upon terrain at an excessive speed Figure 10 22 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 SS Ee vIOwVouss 0 20 40 60 80 100 120 140 Altitude Loss Feet 6000 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 23 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 22 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 S
37. 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 should MFD1 SERVICE MFD1 needs be serviced service 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 contig error Contig service req d The PFD and or MFD configuration settings do not match backup configuration MFD1 CONFIG MFD1 config error memory The G1000 system should be serviced Contig service req d 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 Ke euk key n A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by 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 mod
38. icon cursor Airspace Alerts Box Ifthe projected course takes the aircraft inside an airspace within the next ten minutes Ahead is displayed e Ifthe aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside Ahead lt 2 nm is displayed e Ifthe aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside Within 2 nm is displayed 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 29 SECTION 7 NAVIGATION Blank Page 7 30 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 8 FLIGHT PLANNING The following discussions pertain to the Multi Function Display unless otherwise indicated 8 1 USER DEFINED WAYPOINTS 17 95 196 975 118 000 coz B imme 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 name 3 Turn the large FMS Knob to move the cursor to the next character field 190 00384 08 Rev A 5 6 1 8 SECTION 8 F
39. 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 Pilot 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 08 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 e 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 3 ENGINE INDICATION SYSTEM EIS 3 8 Engine Manifold Pressure Gauge MAN IN Models 182 T182 206 T206
40. is intercepted See Figure 7 25 y VZ44LAA fis ULUS 322 o T EAREN Arrival KCOS TBEDBRY1 ALL TBE a7 n CURRENT VNV PROFILE ACTIVE VNV WPT T at VS TGT FPH FPA ere VS PEO FPM TIME TO TOD V DEV FT 100r i 1000Ff7 i EI NOL VNV 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 E Key The Direct to Window is now displayed as shown in Figure 7 26 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION DIRECT TO LIDENT FACILITY CITY H NH NORTH UP LOCATION ERG 2B pis TE1NH 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 DIRECT TO Eee EOGILITY aa 0PSHN a SH US i LOCATION 260 DIS 101 ACTIVATE Figure 7 27 Enter VNV Altitude e An altitude of 10 000 feet is entered as requested by ATC 1 11 SECTION 7 NAVIGATION f Press the ENT Key The cursor is now displayed in the VNV offset field as shown in Figure 7 28 A NOTE If the loaded arrival procedure has waypoints with altitude constraints retrieved f
41. is not engaged the pitch trim servo may be used to provide manual electric trim This allows the aircraft to be trimmed using 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 LAP UPL ALTS Figure 6 26 Autopilot Engaged 190 00384 08 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 surface
42. lope upon release of the CWS Button Approach Mode Active Active ILS Frequency Tuned Command Bars Indicate Descent on Localizer Glides lope Path HSI Set to LOC2 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 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 100001 GS Figure 6 18 Glideslope Mode Armed 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 Glideslope Mode Active 118 200 136 975 con 136 975 118 888 conz _ Glideslope Indicator 29 921N XPORI 1253 ALT RIEL 9 40 27Pm Figure 6 17 Glideslope Mode 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around GA Mode Pushing the GA Switch 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 Arou
43. 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 08 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 WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is s
44. 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 FREQUENCY AUTO TUNING Auto tuning on the PFD NEAREST AIRPORTS 124 6 8NM VFR 122 700 RNWY 2440FT 270 10 2NM ILS 123 000 RNWY 57 FT 150 11 4NM ILS 7T339FT 133 000 RNWY 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
45. 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 Temperature 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 Pressing the ASSIST Softkey causes the EGT deviation from peak APEAK Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 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 caution and warning ranges appear in yellow and red re
46. should alleviate the condition 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 08 Rev A RECORD OF REVISIONS Part Number Change Summary 190 00384 03 Added XM Radio and XM Weather Rev A 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 190 00384 03 Updated system software numbers Rev B 190 00384 04 Retormatted manual to new format Rev A Added TAS capability 190 00384 04 Added DONE Softkey XM INFORMATION Page and XM RADIO Rev B Page operation 190 00384 05 Added explanation of EIS display behavior upon exceedances Rev A Added better explanation of Intercom System Isolation Added Stormscope operation upon loss of heading input Added TAWS B Added CO Guardian Added new Fuel Totalizer Updated G1000 System Messages 190 00384 06 Added GDU 7 00 WAAS VNAV amp Charts software parameters Rev A 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 Added GDU 8 02 parameters Airways and ADS B 190 00384 08 Added GDU 8 20 parameters including gradient background on the PFD and GFC 700 for the C172
47. the Alerts Window Pressing the ALERTS Soitkey 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 the alert message list Softkey Annunciation During certain alerts the ALERTS Softkey may appear as a flashing annunciation to accompany an alert The ALERTS Softkey assumes a new label consistent with the alert level WARNING CAUTION or ADVISORY System _ Annunciation Red X SECTION 12 ANNUNCIATIONS amp ALERTS 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 System Annunciations Typically a large red X appears in windows when a failure is detected in the LRU providing the information to the window See the G1000 System Annunciations section for more information e Audio Alerting System The G1000 system issues audio alert tones when specific system conditions are met See the Alert Levels Definitions section for more information TEE LELENE s Annunciation Window GDC1 CONFIG GDC1 configuration error Config service req d AHRS TAS AHRS not receiving airspeed APPR VPROF Approaching YN
48. 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 Flash Up to 10 sec Indicating Automatic Transition Figure 6 6 Automatic Mode Transitions During Altitude Capture Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Changing the Selected Altitude 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 aircratt 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 l
49. the Cessna Nav III 190 00384 08 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 Engine Display Default display shows all critical engine fuel and electrical indicators e Lean Display Provides engine leaning information e 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 display and can be displayed after viewing other EIS displays by pressing the ENGINE Softkey The EIS automatically detaults 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 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 pre
50. 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 J GPS TAP 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 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 _ GPS AP 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 ALT Mode Figure 6 34 FLC Descent Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 190 00384 08 Rev A Vertical Path Tracking descent to VNV Target Altitude 1 Select VNV flight control a Press the VNV Key to arm Vertical Path Tracking Mode The white annunciation VPTH appears _ 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 flig
51. 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 Press to display traffic on the map 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 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 1 SYSTEM OVERVIEW a Tooeou cen oo eo BRG1 NAV1 BRG2 NAV2 Press the STD BARO or BACK Softkey to return to the top level softkeys Figure 1 4 PFD Configuration Softkeys PFD
52. 00k T of ia k LEL 506 14PH Figure 6 25 Backcourse Mode 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 22 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 4 AUTOPILOT OPERATION NOTE Refer to the AFM for specific instructions regarding emergency procedures Cessna Nav III s 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
53. 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 27 SECTION 12 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 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 np A red X through any other display field such as engine instrumentation RICE Hanoi eG MAIN fields indicates that the field is not receiving valid data 12 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS A red X may be the result of an LRU or an LRU function failure The Figure 12 6 illustrates all possible flags and the responsible LRUs GIA 63 63 Re GIA 63 63 Integrated Avionics 3 3 Integrated Avionics nits tae Phi Units ma mS j sA l xX 4 Ai 7 GDC 744A Air Data N E y yo Computer lt CRA Ph N 2700 A A i J PITT FFLOW GPH EL Fa E amp _ m GRS 77 AHRS GEA 71 Engine OIL PRES p Wi Or Airframe Unit r q i GMU 44 Or SL Biwi Magnetometer GIA 63
54. 118 98 TSJC Command Bars Indicate Descent on Glidepath Fri TAS I1DOKT HSI Set to GPS 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 Approach Mode Glidepath Mode Active 118 200 136 975 cont 136 975 118 000 conz Eo Glidepath T Indicator LPV Ap proac Active RILCL 8 42 56PH Figure 6 15 Glidepath Mode 6 14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A _ GPS AP ALTS GP Figure 6 16 Glidepath Mode Armed If vertical guidance becomes or is expected to become 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 NOTE Pressing the CWS Button while Glideslope Mode is active does not cancel the mode The autopilot guides the aircraft back to the glides
55. 136 975 118 0909 conz CELL HOV SIG AIR METAR LEGEND HORE WX 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 Limitations 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
56. 29 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 12 6 VHF 4 1 VNAV 1 11 7 1 7 4 12 22 VNAV Target Altitude 6 10 6 13 VNAV Target Altitude Capture Mode 6 13 VNV 1 10 1 11 7 15 Voice alerts 12 3 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Voltmeter 3 2 3 8 Volume squelch 5 4 VS 1 4 VSI 7 16 Vspeeds 2 3 W WAAS 2 6 6 24 7 5 12 16 WAAS precision approach 6 32 WARN 2 11 2 12 WARNING 12 2 Warning alerts 12 3 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 Index 3 INDEX Blank Page Index 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 91 3 397 828 Garmin AT Inc oe 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 2138 i EUN S d 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 08 Rev A 2004 2007 Garmin Ltd or its subsidiaries
57. 3NM VFR MULTICOM 122 900 RNWY 350 FT KIDA 261 9 5NM ILS TOWER 118 5600 RNWY 960 1FT KRXE 4 352 20 11NM UNICON 122 800 RNWY Identifier Runway Length 4200FT Primary COM Frequency Figure 7 59 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 frequency 7 26 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 10 NEAREST INTERSECTIONS Figure 7 60 Nearest Intersections Page Select the Nearest Intersections Page 1 2 Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to select the second rectangular page icon View Information on the Nearest Intersection 1 2 3 With the Nearest Intersections Page displayed press the FMS Knob to activate the cu
58. 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Message Comments o Abort approach due to loss of GPS navigation Abort approach 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 A failure has been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system 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 still NAV2 SERVICE NAV2 needs service be available The G1000 system should be serviced Return unit for repair NAV1 RMT XFR NAV1 remote a transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transter switch again to cycle its operation If the problem persists NAV RMT XFR NAV2 remote the G1000 system should be serviced transfer key is stuck ile ieee OTRA A failure has been detected in glideslope receiver 1 and or re
59. 63W CHT DA Integrated Avionics SE Unit aaa FUEL QTY GAL ELECTRICAL 2 L ee Cl 63 63W Senne A nits In BATT s ey ol A oAT J ORES XPDR FAIL ay ALERTS GTX 33 Transponder ENGINE PFD CDI DME XPOR IDENT TR GDC 74A Air Data Or Computer a GIA 63 63W Figure 12 6 G1000 System Failure Annunciations Integrated Avionics Units 12 8 G1000 SYSTEM MESSAGE ADVISORIES 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 A 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 message 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 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 9 SECTION 12 ANNUNCIATIONS amp ALERTS MFD amp PFD Message Advisories The pilot profile data was lost System reverts to default pilot profile and settings lost Recheck settings The pilot may reconfigure the MFD amp PFD with preferred settings it desired
60. 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 strike location Therefore the exact location of the strike is not displayed 190 00384 08 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 disp
61. 700 con ALTS 123 800 135 325 conz Selected Altitude Din an e 1000 9AA XPOR 1200 SIBY itl_2 32 19eH Figure 6 5 Pitch Hold Mode 190 00384 08 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 director 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 until Selected Altitude Capture Mode becomes active 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
62. A GARMIN G1 01010 Integrated Flight Deck Cockpit Reference Guide Cessna SEWAIL Copyright 2004 2007 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0563 05 or later for Cessna 172R 172S 1827 T1827 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 hereby 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 com
63. 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 associated 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 Th
64. AY prof ile STEEP TURN Steep turn ahead pro 1200 ALT Lol 004653 Figure 12 1 G1000 Alerting System Garmin G1000 Cockpit Reference Guide for the Cessna Nav III n Alerts Window se SM GS ALERTS Sofikey Annunciation 12 1 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 ALERT LEVEL DEFINITIONS WARNING The G1000 Alerting System as installed in Cessna Nav II aircraft uses three alert levels Figure 12 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 also accompanied by a flashing WARNING Soitkey annunciation as shown in Figure 12 2 Pressing Figure 12 3 CAUTION Softkey the WARNING Softkey acknowledges the presence Annunciation of the warning alert and stops the aural tone if applicable e CAUTION This level of alert indicates the existence of abnormal conditions on the aircraft that may require pilot intervention A caution alert ADVISORY is annunciated in the Annunciation Window and is DVI S RY accompanied by a single aural tone Text appearing Figure 12 4 ADVISORY Softkey in the Annunciation Window is YELLOW A caution Annunciation alert is also accompanied by a flashing CAUTION Softkey annunciation as shown in Figure 12 3 Pressing the CAUTION Softkey acknowledges the prese
65. Approoch KOOS RNAY 35Riees LP HABUK tof eee renee A a _SECURITY WIDEPIELD FALUR E eee CEGIX fof Sa peed F RHR mnp 351 4 3HH BS68FT 348 DAH MOGAL mohp 168 B NA ICURRENT WHY PROFILE ACTIVE Wh WPT _ __FT at VS TGT VS REO V DEV Figure 7 47 Descending to the Missed Approach Point Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION In this missed approach procedure the Tix immediately following the MAP in this case 6368FT is not part of the published procedure It is simply a fix that defines a leg which guides the aircraft along the runway centerline until the required altitude to make the first turn on the missed approach 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 this fix until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to is established to the published fix in this case MOGAL If 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 the fix is not part of the published procedure In some missed approach procedures this altitude fix may be part of the published procedure For example the procedure dictates a climb to 5 500 feet then turn left and proceed t
66. B MISMATCH Airport Terrain The PFD and MFD have different airport terrain databases installed Install database mismatch correct airport terrain database in both displays Pee Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 12 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 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 config error Config 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 er
67. C Switch is located forward of the MET Switch on the pilots control wheel left grip This switch may be used to 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL 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 Autopilot Roll Modes Status 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 Figure 6 2 Command Bars Pitch Modes Armed Active Active Mode Reference AFCS Status Box nave 113 08 118 98 IIKO mz 115 90 118 98 IIXD Command Bars Select
68. 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 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 FM
69. Color Refer to Figure 1 8 and Table 1 1 for more detail regarding the significance of text size and color 8 8 8 Some altitudes retrieved from the database have ACTIVE FLIGHT PLAN associated restrictions indicating to stay At At or Above KIXD KDFW or At or Below a specific altitude These restrictions are indicated using a bar above and or below the appropriate KARLA AMER ge Large White altitude as shown in Figure 1 9 COVIE 221 9 NM 1200F LEMYN nT Mec lea t Laree Light SLESSTEAM Cross AT or ABOVE 5 000 fi Approach KDFW RNAV 17LePs LPV ever RIVET iof Mee MCE Small Light FANGS Cross AT 2 300 ft DRAAK im aa Puc Text INWOD 176 3 2MM 380 ET eisau Cross AT or BELOW 3 000 ft ae ed ei Pe i i Figure 1 9 Altitude Restrictions RW17L map 176 5 3MM Small White 99 FT 174 SNM S9GFr Text with POLKE oe See Section 7 Navigation for a sample flight plan Figure 1 8 VNAV Altitudes Bar vaio further illustrates vertical navigation in more etall 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 111 SECTION 1 SYSTEM OVERVIEW 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
70. DL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software mismatch The GDL 69 has incorrect software installed The G1000 system should be communication halted serviced GDC 74A Message Advisories Ape ee Bava aitus The GDC 74A is reporting that the altitude error correction is unavailable correction is unavailable AJI gt a a ECR The GDC 74A is reporting that the airspeed error correction is unavailable correction is unavailable MANIFEST GDC1 software The GDC 74A has incorrect software installed The G1000 system should be mismatch communication halted serviced 12 20 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories FPL WPT LOCK Flight plan waypoint Upon power up the G1000 system detects that a stored flight plan waypoint is 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 identitier to reflect the new information FPL WPT MOVE Flight plan The system has detected that a waypoint coordinate h
71. EC Th A nl ard Figure 10 7 Navigation Map Page Displaying NEXRAD Weather 190 00384 08 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 the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes NORTH UP areor ts KMSP PUBLIC MINNEAPOLTS ST PAUL INTL MINNEAPOLTS HN pe METAR Lee Text FT BROKEN ZSRREFT BROKEN TEMPERATURE 23 DEW POINT 14 c ALTIMETER 29 721n _ 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 10 3 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
72. F CONTENTS 12 3 CO Guardian Messages ccccceeeeen 12 3 12 4 ECS AIOU tS ies o 550i cte cctacctamsiiendnserngmiccntoneccnnacts 12 4 System Status ANNUNCIATION cccssssssssssnesscsoonsececnuess 12 4 12 5 TAWS Alerts 12 5 12 6 Other G1000 Aural Alerts 0 0 0 ccccceen 12 6 12 7 G1000 System Annunciations 0 0 0 12 7 12 8 G1000 System Message Advisories 12 9 MFD amp PFD Message AdVISOI S cscesceeseeseeseesen 12 10 Database Message AdVISOFES c sscsseseeseseereesen 12 11 GMA 1347 Message Advisories ccsscestecseesteeseeseeen 12 13 GIA 63 Message Advisories c scesscesseseeseesesseeen 12 13 GIA 63W Message Advisories n u 12 16 GEA 71 Message Advisories sesiis 12 18 GTX 33 Message Advisories 12 19 GRS 77 Message Advisories 12 19 GMU 44 Message Advisories scessceseesseeseesesseean 12 20 GDL 69A Message Advisories cessceseeseesessesseeen 12 20 GDC 74A Message Advisories 12 20 Miscellaneous Message AdVISOFES c ssseeseses 12 21 INDEN esp ne veto Po vn On OC Ore Index 1 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 1 SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions for the Primary Flight Display PFD Multi The purpose of thi
73. GHT 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 while in LOC Navigation Mode 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 uses the selected navigation receiver deviation a
74. H 16 76 Sh F ELECTRICAL M BUS E 12 245 VOLTS 24 5 BATT 5 M 13 0 0 AMPS AO Model 206H 0 0000 190 00384 08 Rev A Cruise Manifold CL Pressure HAN IN 3s 3 RPM 5790 a 2430 FFLOW ater Cruise OIL PRES Fuel Flow OIL TEMP a TIT me FUEL TY GAL m ry 4 16 62H ELECTRICAL M BUS E 24 5 volts 24 5 M BATT 5 0 4 aMPS 6 0 Model T182T 000000 SECTION 3 ENGINE INDICATION SYSTEM EIS OTA gg RPM 2700 2000 Maximum FFLOW GPH ech Fuel icin CCIM OIL PRES ee OIL TEMP CHT L V TIT D FUEL QTY GAL 4 m 5 160 z0 Sh F ELECTRICAL H BUS E E 2145 vots 245 BATT 13 he AMPS i Model T206H FTOR Figure 3 2 Engine Display Turbocharged Aircraft 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III a2 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 4 LEAN DISPLAY NOTE The pilot should follow the engine man ufacturer s recommended leaning procedures in the Pilot s Operating Handbook POH 1 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
75. HRS is not receiving backup GPS information The G1000 system should backup GPS information be serviced AHRS1 GPS AHRS1 operating The 1 AHRS is operating exclusively in no GPS mode The G1000 system should exclusively in no GPS mode be serviced AHRS1 SRVC AHRS1 Magnetic tield The 1 AHRS earth magnetic field model is out of date Update magnetic field model needs update model when practical GEO LIMITS AHRS1 too far North The aircraft is outside geographical limits for approved AHRS operation Heading South no magnetic compass is flagged as invalid MANIFEST GRS1 software The 1 AHRS has incorrect software installed The G1000 system should be mismatch communication halted serviced 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 19 SECTION 12 ANNUNCIATIONS amp ALERTS GMU 44 Message Advisories HDG FAULT AHRS1 magnetometer A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS fault has occurred uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software The GMU 44 has incorrect sottware installed The G1000 system should be mismatch communication halted serviced GDL 69A Message Advisories Message GDL69 CONFIG GDL 69 contig GDL 69 contiguration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be serviced G
76. ITY KSLH N CEN USA m NORTH UP 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 E 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 08 Rev A Press the Direct to G39 Key Turn the large FMS Knob to highlight 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 E Key Pre
77. L Se F L PYNON 352 0 7mm 10000FT Approach KCOS RNAV SSRors LPY HABUK iaf 021 5 SNN 3000 FALUR 261 GCONH 8600 CEGIX fof 351 G ONH 7800r RH SR sap 351 5 1NH CURRENT VNV PROFILE ACTIVE VNV WPT 9000FT ot HABUK lof VS TOGT 7S6FPH FPA 25 VS REQ 471FPn TIME TO TOD 0057 TERRAIN T v DEV 750FT 100r l 1000r1 m 5 VS 1 Ea S nn VIEW VNV PROF CNCL VNV VNV amp pis 3nn BRG 351 f Figure 7 42 Approaching PYNO Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Jel SECTION 7 NAVIGATION 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 43 FPL ACTIVE FLIGHT PLAN 136 975 118 688 conz ACTIVE FLIGHT PLAN KMKC KCOS DIS ALT OPSHN 3Nn Sa A FT OPSHN Stare RAY 5 FSHER binan RSS PYNON set oo fee FT Approoch KCOS RNAV 35RoPs LPV gt HABUK iof 021 5 2NM 93000 d FALUR 261 5 0NH 8600 CEGIX fof 351 6 0NM 7890f RH SR map 351 SINH 6368FT 348 8 4Nn MOGAL sahp CURRENT VNV PROFILE ACTIVE viv WPT SBOGeT at HABUK iaf VS TGT 7S5FPH FPA 25 VS REQ 627FPH TIME TO TOD TERRAIN T v pev 290FT 100r1 Figure 7 43 Approach Leg is Now Active To m
78. LIGHT 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 the Navigation Map Page 1 With the Navigation Map Page displayed push the Joystick to activate the panning function The target pointer is displayed
79. M Standby COM Frequency Field Frequency Frequency Frequency Field THEE e 118 580 con nav2 114 60 110 60 Ckv WPT VOR INFORMATION 118 400 121 400 comz Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field 135 100 126 058 com 3 600 121 980 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 Frequency Transfer Key Dual NAV Dual COM Knob Knob Turn to tune in desired frequencies e 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 08 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 121 908 118 680 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
80. MOGAL mahp 1000061 6 0NH CURRENT VNV PROFILE ACTIVE VNV WPT 10 00FT at OPSHN 3NH VS TGT 7S6FPM FPA 75 va RED 23 49 Figure 7 34 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 190 00384 08 Rev A a Press the VNV PROF Softkey to place the cursor in the target vertical speed field VS TGT as shown in Figure 7 35 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 PL ACTIVE FLIGHT PLAN 136 975 esthh JAGTIVE FLIGHT PLAN el TFR KMKC KEOS HI DATA LAA y VW263 TBE TBE poet resuseceriel 5 becuase FT Arrival KCOS TBE DBRY1 ALL OPSHN 3H 20 SANH 10000FT OPSHN 259 Z 10000FT
81. NT FACILITY CITY TE F Figure 8 13 Airway Insertion Point 4 Turn the small FMS Knob to display the Waypoint Information Window and begin entering the desired airways entry point WAYPOINT INFORH TIOH IDENT FACILITY CITY AnA HORTH UF LOCATION BRG DIS Press ENT to accept Figure 8 16 Enter Airway Identifier 7 When the desired airway is entered press the LD a AIRWY Softkey ERG B63 kj DIS 39 0MM Teel Fress ENT to accept Figure 8 14 Load Airway Entry Point 190 00384 08 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 ot 8 11 LOAD AN APPROACH available exit points See the Procedures section for a discussion 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 z procedure s waypoints Figure 8 17 Select Desired Exit Point 3 Press the CLR Key to display a confirmation window 9 With the desired exit point highlighted press the AMOK ignlignted pea a ENT Key the selected procedure or airway 10 With LOAD highlighted press the ENT Key
82. OC1 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 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 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 O
83. Press to display the additional softkeys for additional configuration of the PFD DFLTS Press to reset default settings on the PFD WIND Displays softkeys to select wind data parameters OPTN 1 Wind direction arrows with headwind and crosswind components OPTN 2 Wind direction arrow and speed OPTN 3 Wind direction arrow with direction and speed OFF Information not displayed DME optional Press to display the DME Information Window BRG bearing Press to cycle through the following Nav sources making the pointer the indicator for the corresponding source and displaying the appropriate information NAV 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 ARC HSI Press to display the HSI in an arc format BRG2 bearing Press to cycle through the following Nav sources making the pointer the indicator for the corresponding source and displaying the appropriate information NAV2 Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window 1 6 Garmin G1000
84. Pressing this softkey displays removes terrain and obstacle data on the Navigation Map 1 3 MFD SOFTKEYS ee ENGINE Pressing this softkey makes available the LEAN and SYSTEM Soitkeys which in turn access the Lean Page and the System Page respectively mw n optional optional ENGINE LEAN SYSTEM BACK Default softkey is dependant on Press the BACK Softkey on this the selection made level to return to the top softkey level in the map setup options optional optional optional m A E A A Press the BACK Softkey to return Press the ENGINE Softkey to to the previous softkey level the default Engine Page level gt ee TE re oe Ge Ge Ge ee ere PT rs ry a se a N X airframe specific values i m gt rT Press the ENGINE or BACK Softkey to petro ne delaull Engine age eye The DONE Softkey changes to UNDO when the checklist item is already checked non A ry mw mm D Figure 1 6 MFD Softkeys 1 8 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A gt wn gt I ep 4 SECTION 1 SYSTEM OVERVIEW AIRWAYS Pressing this softkey displays removes 1 4 MFD PAGE GROUPS airways information The default is dependent on map setup option selected Pressing cycles through 1 Turn the large FMS Knob until the desired page all airways displayed AIRWY ON low altitude group is selected airways only AIRWY LO and high altitude airways 2 Turn
85. RRAIN Softkeys are available not dimmed and other database features are functioning Power down the G1000 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 1 SYSTEM OVERVIEW Blank Page 1 14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display unless otherwise indicated nav TAB AA 117 9 i l 136 975 126 625 con1 mava 108 68 177 9 136 975 118 000 coz Poe A ILEI 175929 XPOR IDENT THR REF NRST ADVISOR INSET PFD OBS COI NAV Frequency Box Turn Rate Indicator Airspeed Indicator Barometric Setting Box True Airspeed Box Vertical Speed Indicator Altimeter Selected Altitude Box Heading Box Ground Track Bug Horizontal Situation Indicator COM Frequency Box Outside Air Temperature Box Navigation Status Box Slip Skid Indicator Attitude Indicator System Time Box OOOOOOOOO O0 OG2O0O0 IRES Transponder Status Box Figure 2 1 Default PFD Information 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 1 SECTION 2 FLIGHT INSTRUMENTS navi 17 95 110 DIS RG 136 975 120 100 con nava 168 88 117 95 136 975 118 868 coz BARO HIM aler Cari PATYI HIVAK fot RWSL mop SUNNE mohp H B NH HOLD ae Alali GPS POE RILCL 190757 CDI
86. S 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 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 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 ch
87. 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 NAV1 SERVICE NAV1 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may NAV2 SERVICE NAV2 needs service still be available The G1000 system should be serviced Return unit for repair NAV1 RMT XFR NAV1 remote i PN EE E A transfer key is stuck 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 transfer ey is tik A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S1 SERVICE G S1 needs service on N eres sos Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The 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 configuration The GEA1 configuration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be serviced MANIFEST GEA1 soft
88. T 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 ATTS 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 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 SECTION 9 PROCEDURES 9 2 AIRPORT KSTL p PUBLIC AHBERT ST LOUIS INTL ST LOUIS MO ARRIVAL I Citin Figure 9 3 Select Arrival 7 A second window is displayed listing available transitions for the arrival Turn ei
89. Terrain on the TAWS Pad 10 11 Enable Disable Aviation Data csccseseeseseeeeren 10 12 TAWS NID n aE TANART 10 12 Manual System TeSt ariaa a 10 13 Forward Looking Terrain Avoidance FLTA 10 13 Premature Descent Alert PDA oo 10 13 Excessive Descent Rate Alert EDR n 10 14 Negative Climb Rate After TakeotfAlert NCR 10 14 Five Hundred Aural Alert 10 14 Displaying Terrain and Obstacles on the Navigation Malestar n ea An hicecesananh ons E 10 14 PopUp CM aah 10 15 TAWS Alerts SUMMAary ssasssascasseisasmarsassnasiaaaassagns 10 16 Aleit Annunciation seinnaa 10 17 SECTION 11 ABNORMAL OPERATION 11 1 11 1 Reversionary Mode 0 ccccccccesee cea 11 1 11 2 Abnormal COM Operation 0 0 0 0 00 11 2 11 3 Unusual Attitudes cscs 11 2 11 4 Stormscope Operation with loss of Heading Input ccs cesses 11 2 11 5 Hazard Displays with Loss of GPS Position 11 2 11 6 Dead Reckoning 0 0 cc ccc eects eee 11 3 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 12 1 Alert Level Definitions 0 0 0 0 c ccc ee 12 2 12 2 NAV III Aircraft Alerts 0 00 cee 12 3 WARNING AICS ossaa aE 12 3 CAUTION ACHES ainoaan 12 3 CAUTION Alerts T182 T206 and 206 with Prop De1CO OMY estesnen cere ten teseetrin ae aatalercarta nanny 12 3 Safe Operating Annunciation T182 1206 and 206 with Prop De Ic Only cessessesseesecsessessseaneeressen 12 3 TABLE O
90. a FUEL CALC FFLOW GPH 4 0 GAL USED HRT GAL REM A FUEL QTY GAL m 6 10 20 30 F ELECTRICAL M BUS 2 5 VOLTS 20 M BATT S 4 0 AMPS 6 0 Model T182T 2070 Q OLD OOOOH N pa PH i 2 fHE a 2000 OIL PSI 56 0 OIL F 100 ENG 4085 3 HRS VAC E FUEL CALCE FFLOW GPH 00 GAL USED A GAL REM A FUEL QTY GAL F el 160 7H 38 F H ELECTRICAL MH BUS 24 5 voLTS 24 5 M BATT S 6 6 AMPS 6 0 Model T206H Figure 3 6 System Display Turbocharged Aircraft Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 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 Controls NAV Frequency Box navi 1 15 88 IKEGRaRAGOU FFL 4 DME NAVI a 111 28 3 Ss e 46 5 HH ki z J gt TRE HAW HAYT INSET PFD COI Figure 4 1 G1000 VHF NAV COM Interface PFD shown 190 00384 08 Rev A DME APDR IDENT 122 358 SECTION 4 NAV COM amp TRANSPONDER COM COM Frequency Box Controls 121 608 con 126 975 con2 PUSH CRS 4 BARO DHE TUNING Tee saeNAY 1 THR REF NAST ALERTS DME Tuning Window Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 4 1 SECTION 4 NAV COM amp TRANSPONDER Standby NAV Selected NAV Selected CO
91. a Nav III 190 00384 08 Rev A SECTION 10 HAZARD AVOIDANCE The following system status annunciations may also be issued PFD MFD TAWS Alert Type Page MED Aural Message YP Je Pop Up Alert J Annunciation TAWS TANS System Test Fal Test Fail AWS FA e TAWS TAWS System Failure Failure No GPS position or excessively degraded TAWS NAA None TAWS Not Available GPS signal TAWS Available will be heard when sufficient GPS signal is re established System Test pass None TAWS System Test OK Alert Annunciations Alert Annunciation TERRAIN 1 D0F1 Figure 10 27 TAWS Alert Annunciation on the PFD Alert Annunciation Figure 10 26 Alert Annunciation on the TAWS Page 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 17 SECTION 10 HAZARD AVOIDANCE Blank Page 10 18 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 11 ABNORMAL OPERATION 11 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 Minimal navigation capability is available on the Reversionary Mode display SECTION 11 ABNORMAL OPERATION Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display proble
92. a entered by the user 12 22 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A A Abnormal COM operation 11 2 Activate a flight plan 8 3 Active flight plan 8 2 ADF 1 6 1 7 5 3 ADS B RR 1 10 7 10 9 12 6 AFCS 12 4 Age 10 6 AHRS 12 19 12 20 Aircraft alerts 12 3 AIRMET 10 5 Airport frequency 7 25 Airport information 7 21 Airspace alerts 7 29 Airspeed indicator 2 3 Airspeed Reference 6 8 Airspeed trend vector 2 3 Airways 8 5 Alerting system 12 1 Alerts 12 1 Alert levels 12 2 Alert Pop Up 10 15 ALT 1 4 1 7 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 2 3 8 AP 1 4 Approach ILS 6 31 Missed 6 33 WAAS 6 32 Approaches 9 2 Approach activation 4 4 Approach markers 190 00384 08 Rev A Signal augmentation 5 2 Approach Mode 6 20 6 31 Approach Mode AFCS 6 32 AP DISC Switch 6 1 6 34 Arrivals 9 1 Assist 3 4 3 6 3 Attitude indicator 2 3 Audio alerting system 12 1 Audio panel 4 3 5 1 Audio panel controls ADF 5 3 DME 5 3 NAV1 5 3 NAV2 5 3 Aural alerts 12 6 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 disconne
93. a of A aL fais Selecte Ai Pn Waypoint ad H Map Range LOCATION Bearing BRG 129 DIS 1885NH Distance 7 COURSE as 146 ACTIVATE Activate Field Figure 7 2 MFD Direct to Window Enter a Direct to Destination 1 Press the Direct to 8 Key 2 Enter the destination waypoint identifier 3 Press the ENT Key to contirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNAV altitude field 6 Enter the desired altitude 7 Press the ENT Key The option to select MSL or AGL is now displayed 8 Turn the small FMS Knob to select MSL or AGL Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 1 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 2 Key 2 Turn the smal
94. ains a procedure turn vector or other unsupported leg type in flight plan type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive crosstrack error VNV Unavailable Excessive track angle error VNV Unavailable Parallel course selected 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 trom the traffic system The trattic device failed should be serviced STRMSCP FAIL Stormscope has failed The current crosstrack exceeds the limit causing vertical deviation to go invalid The current track angle error exceeds the limit causing the vertical deviation to go invalid A parallel course has been selected causing the vertical deviation to go invalid Stormscope has failed The G1000 system should be serviced FAILED PATH A data path has failed 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 from the actual magnetic heading by more than 2 SCHEDULER lt message gt Message criteri
95. al use airspace is near and ahead of the aircraft position ARPE NEAR AI PACE 0aT E Special use airspace is within 2 nm of the aircraft position than 2 nm APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 21 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont Comments The system notities the pilot to load the approach trequency for the appropriate NAV receiver Select the correct frequency for the approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver Message SLCT FREQ Select appropriate frequency for approach SLCT NAV Select NAV on CDI for approach PTK FAIL Parallel track unavailable bad geometry PTK FAIL Parallel track unavailable invalid leg type PTK FAIL Parallel track unavailable past IAF UNABLE V WPT Can t reach current The current vertical waypoint can not be reached within the maximum flight path vertical waypoint angle and vertical speed constraints The system automatically transitions to the next vertical waypoint Bad parallel track geometry Invalid leg type for parallel offset AF waypoint for parallel offset has been passed VNV Unavailable Unsupported leg The lateral flight plan cont
96. an 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 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 ia SECTION 7 NAVIGATION 2 Figure 7 11 shows the aircraft on the assigned heading of 240
97. anesesaarvotsandevatennasnanciet 4 4 4 7 Transponder 4 4 Mode SCIC CON mansis 4 4 REV BS 2 epee ne eer cece eee 4 5 Code Selections ai 4 5 Fight ID REDON suenen 4 6 SECTION 5 AUDIO PANEL 5 1 5 1 COM Radio Selection 0 cccccssessesseeees 5 2 5 2 Cabin Speaker ccc 5 2 5 3 Passenger Address PA System T 182T and T 206H Only once etivetnasencniedaueuie 5 2 5 4 Marker Beacon Receiver ccccccceeeceen 5 2 Marker Beacon Signal Sensitivity c scence 5 2 5 5 Nav Radio Audio Selection cccceee 5 3 5 6 Intercom System ICS Isolation 5 3 5 7 Intercom Squelch Control 00 cccces 5 4 5 8 Digital Clearance Recorder and Player 5 4 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 1 6 1 AFCS Controls 6 1 6 2 Flight Director Operation 0 0 c cc 6 2 Activating the Flight DireCtOr scriure 6 2 Comman GUD GNS ers E nse 6 2 PREC Ses aS BOM tah ian a tat 6 3 6 3 Flight Director Modes 0 0 cccseees 6 3 PU NOES re 6 3 ROIMOUES siron nn a 6 17 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III TABLE OF CONTENTS 6 4 Autopilot Operation 0 0 ee 6 22 PONEC CONTO oninia nan 6 22 Engaging the AUTOPIG tis casdsansccaduassctadsoasepedaantaactsdade 6 22 Control Wheel Ste rind ccsscessesseesseesecsessesseeaseesees 6 23 DISCO AGING WNC AUTO ONO iensen 6 23 6 5 Example Procedures 0 c cccsesese
98. ange the page mode press the AUTO or MANUAL Softkey Ending WPT TRIP STATS L STATS OTHER STATS Tk EET Ticean DENSITY ALT ors AICHA OTAL ENOUR Cee TRUE AIRSPEED ETE i REH FUEL 4 GL WIND OTRECTION cH WIND SPEED HEAD WIND MANUAL Bac 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 08 Rev A 190 00384 08 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 Knob to select the desired leg of the flight plan or select CUM to
99. annunciation disappears when the overspeed condition is resolved nav1115 5 113 00 nav2 108 08 lt 117 95 a Airspeed E Indicator JAVOD a id fa a f La f l Figure 6 41 Overspeed Annunciation 190 00384 08 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 08 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 1 NAVIGATION MAP PAGE WARNING The map display should only be used for situational awareness 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 136 975 118 000 conz NORTH UP Figure 7 1 Navigation Map Page Enroute 190 00384 08 Rev A SECTION 7 NAVIGATION 7 2 DIRECT TO NAVIGATION Direct to Navigation from the MFD I dentifier IDENT cece ies hic KMIA SE USA egion Facility Name HIAMI INTL 6 City Sigua VNAV Target Altitude ny m Offset Before Selected ne 300051 5i Direct to Target Altitude l 8 b Sei aE Map Orientation M
100. anually 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 Figure 7 44 PROCEDURES OPTIONS ACTIVATE VECTOR TO FINAL ACTIVATE APPROACH SELECT APPROACH SELECT ARRIVAL SELECT DEPARTURE Figure 7 44 Activate Missed Approach c Press the ENT Key to activate the approach Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 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 136 975 118 688 conz hd 5358FT s TIVE FLIGHT PLAN a KMKC KOOS ALT OPSHN Stt CEA AN RE FT OPSHN APAY CISS a eT FSHER eat ese hae FT PYNON EREA anaes FT sera KCOS RNAV 35Ro6rs LPV HABUK lof 26 FALUR 251 5 NH CEGIX fof 351 6 01Nn 1 7N RHSSR map 351 5 Nn 6368F1 348 O 4NN MOGAL aahp CURRENT VNV PROFILE ACTIVE viv WPT SB OGeT at HABUK iaf VS TGT 7S5FPH FPA S REO FPH TIME TO BO TERRAIN VS REO baini IME B00 T V DEV S FT 1009F 1000F7 Figure 7 45 Descending Turn to the Initial Approach Fix IAF 190 00384 08 Rev A 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 accordin
101. 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 indicated altitude Press the ENT Key when finished 11 The flashing c
102. armin 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 Path Tracking becomes active and tracks the descent pro file An altitude capture mode ALTS or ALTV is armed as appropriate navi 1H8 AA 117 95 naz 188 08 117 95 Fri TAS IOOKT HSI Set to GPS Vertical Path Tracking A ctive ay Target Altitude Capture Armed bs 232 136 975 gt 118 000 com A eile __ 118 008 conz VNAV TE E Target Altitude Vertical Deviation Indicator Required Vertical Speed Bug Terminal Phase of Flight xPOR1 ALT Rit 21514535 Figure 6 12 Vertical Path Tracking Mode Automatic Pitch Hold Reversion Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode Vertical Path Tracking and the appropriate altitude capture modes are armed for possible descent profile recapture if the vertical deviation e Exceeds 200 ft during an overspeed condition e Experiences a discontinuity exceeding 200 ft due to a flight plan change e Becomes invalid due to excessive cross track error track angle error e Cannot be computed for a leg type such as a hold or procedure turn Garmin G1000 Cockpit Reference Guide for the Cessna Nav III The following circumstances cause mode reversion without arming Vertical Pa
103. armin 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 in the bottom card slot of the PFD The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD 3 4 5 SECTION 1 SYSTEM OVERVIEW 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 Basemap Land 1 01 A gt SofeToxi Expires 28 SEP 2006 ae Terrain 2 04 a Airport Terrain 2 04 aN Obstacle Expires 28 SEP 2006 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 and 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 TE
104. as changed due to a new waypoint moved aviation database update Verity 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 manually Verity user moditied procedures edited This alert is issued only after an aviation database update Verify that the user moditied procedures in stored flight plans are correct and up to date 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 aie era NAAN Arriving at waypoint xxx where xxxx is the waypoint name 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 less Special use airspace is ahead of aircraft The aircraft will penetrate the airspace than 10 minutes within 10 minutes cent NEAR A ACETRE Speci
105. ase specified altitudes a Press the PROC Key to display the Procedures therefore dashes are displayed Keep the CDI Window centered and maintain a track along the magenta If the GPS system is not WAAS capable or WAAS line to OPSHN is not available the LPV approach will not be Note the Direct to waypoint is within the loaded displayed in the list of available approaches arrival procedure therefore phase of flight scaling Selecting the LNAV approach for runway 35R gives for the CDI changes to Terminal Mode and is vertical guidance up to the IAF annunciated by displaying TERM on the HSI TD Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A b SELECT APPROACH should be highlighted as shown in Figure 7 30 PROCEDURES SELECT ARRIVAL SELECT DEPARTURE APPROACH ARRIVAL KCOS TBE DBRY 1 ALL DEPARTURE KMEC ALL WLOCT 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 Kcos b PUBLIC CITY COLORADO SPRINGS CO APPROACH CHANNEL CHANNEL 97799 TO W35A APPROACH RNAV 35Rops LPV Lops LNAV V Ropes LPV j Arps LNAV Y IRM SRGF a LFY L NDE 35L pe ee ee ney stad wel NM RW3SR mop 357 5 1NH 6358FT 343 BANM HOGAL mohp HOLD So 60s LOAD oR ACTIVATE Figure 7 31 List of Available Ap
106. 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 ast 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 KIXD ver re AF ts Figure 8 4 Flight Plan Catalog Page Approoch ILS 30R O0DS iof 127 19 01 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 press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight
107. bove own aircraft a Altitude Trend up arrow Intruder indicates Arcot climbing down Heading arrow indicates extends in the direction of the aircraft heading descending Figure 10 15 Example ADS B Traffic Advisory Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 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 i g BS MAP TERRAIN PROXIMITY 136 975 118 088 com aircraft latitude is greater than 75 degrees north ary st oF or 60 degrees south ot lt 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 Terrain Obstacle above or within 100 below or above aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Aircraft Altitude 100 Threshold Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Height is less than Height is less than Heig
108. c 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 display 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 Set the range to 2 6 nm 2 Press the STANDBY Softkey 3 Press the TEST Softkey 4 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 136 975 118 000 core HOG UP AP Ss AT Figure 10 12 Self Test OK Display 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 10 8 Garmin G1000 Cockpit Refer
109. ce is manually switched e Localizer signal is not captured by the final approach fix FAF while in LOC Navigation Mode 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 08 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 roll steering commands from the Selected Course and deviation when in Backcourse Mode Backcourse Mode Active nav 111 90 nav2 113 88 4 114 10 suc LOC2 is Active Navigation Receiver on HSI 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 tlying the aircraft does not reset any reference data while in Backcourse Mode The autopilot guides the aircraft back to the Selected Course or GPS flight plan when the CWS Button is released Glideslope Mode Active AB 136 975 com 118 000 conz 3700 cul 36
110. ceiver 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 S needs service may still be available The G1000 system should be serviced when possible Return unit for repair 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 15 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories GIA1 CONFIG GIA1 configuration error Contig service req d The GIA1 and or GIA2 configuration settings do not match backup configuration GIA2 CONFIG GIA2 configuration memory The G1000 system should be serviced error 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 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 uni
111. ct 6 16 6 23 Backcourse Mode 6 21 Barometric minimum 2 8 Base reflectivity 10 4 BRG1 2 11 BRG2 2 11 C CAUTION 12 2 Caution alerts 12 3 CDI 2 9 2 11 7 3 7 6 7 12 7 16 7 20 9 2 12 22 Cell 10 2 Cell mode 10 2 Cell movement 10 5 Cloud Tops 10 4 CLR 1 3 3 8 Coast mode 10 7 Code selection 4 5 Command Bars flight director 6 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III INDEX 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 Dead Reckoning 2 12 11 3 12 8 Departures 9 1 Direct to 7 1 7 5 7 11 7 12 8 8 DME 1 7 DR 2 12 DR mode 11 3 11 4 Dual CDU failure 11 2 E ECHO TOPS 10 4 Edit a flight plan 8 7 EDR 10 14 Engine Hours 3 2 3 8 Engine Leaning 3 6 Engine Page 3 1 Excessive Descent Rate 10 14 Exhaust Gas Temperature 3 1 3 4 F FD 1 4 Five Hundred Aural Alert 10 14 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 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 FLIA 10 13 Index 1 INDEX Forward Looking Terrain Avoidance 10 13 Freezing level 10 5 Frequency toggle key 1 3 4 3 Fuel Calculations 3 7 Flow totalizer 3 7 Remainin
112. ction 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 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 ALT 300061 VPTH PPS Figure 6 10 Vertical Path Tracking Armed Annunciations Prior to descent path interception the Selected Altit
113. e 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 08 Rev A SECTION 4 NAV COM amp TRANSPONDER Enter Code Using Softkeys 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 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 SECTION 4 NAV COM amp TRANSPONDER Flight ID Reporting If so configured the Flight ID may be entered in the Timer Retfe
114. e aircraft J GPS AP VPTH 4 When the next TOD is reached Vertical Path Tracking becomes active may require acknowledgment to allow descent path capture _ GPS AP ALTV 5 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 _ GPS AP 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 HABUK A Figure 6 36 Non path Descent Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A Approach Flying an ILS approach 1 Transition from GPS Navigation Mode to Heading Select Mode a Load the Runway 35L ILS approach for KCOS into the flight plan and select VECTORS for the transition 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 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 a
115. e 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 tone 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 EE 1800 Altimeter 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 08 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 8 BOLATION deselects the audio source and activates the annunciator Figure 5 7 ICS Isolation Selected audio can be heard over the headset
116. e 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 6 26 6 21 Navigation status window 2 2 NAV frequency window 4 1 NCR 10 14 Nearest Airports Page 7 21 7 25 7 29 8 1 Nearest ARTCC amp FSS frequencies 7 28 Negative Climb Rate After Takeoff 10 14 NEXRAD 1 9 10 3 10 6 Non path descent 6 12 6 30 6 31 0 OBS 2 12 Obstacles 10 10 10 15 12 12 12 16 Oil Pressure 3 1 3 8 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 PDA 10 13 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 Premature Descent Alert 10 13 Procedures GFC 700 6 24 6 36 Procedure examples AFCS 6 24 6 31 190 00384 08 Rev A Red pointer 2 3 Remove departure arrival or approach 8 6 Replies 4 5 Required Vertical Speed 2 6 7 15 Required Vertical Speed Indicator 7 15 Reversionary mode 5 1 11 1 ROC 10 13 10 16 12 5 Roll Hold Mode ROL 6 17 Roll modes flight director 6 17 6 20 Roll Reference 6 18 RTC 10 13 RVSI 7 15 7 16 RX indicator 4 3 R indication 4 5 S Secure Digital SD card 1 12 Selected Altitude 6 6 6 10 6 13 Selected Altitude Capture Mode 6 6 6 10 6 13 Selected Course
117. ed 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 terrain database is present on another LRU but is missing on the specified LRU The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced The obstacle database is present on another LRU but is missing on the specified LRU The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced SECTION 12 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 SateTaxi database error exists PFD1 DB ERR PFD1 SafeTaxi 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 t
118. ed 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 cell 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 08 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 118 000 com WORTH UP 136 975 p IME HFL ni m a i HPPEETO IT
119. ed Heading GPS is Selected Navigation Source 118 700 con 135 925 123 888 con Selected Altitude Selected Course PIR 1200 STAY LCL 237 55F RS ALERTS Figure 6 3 PFD AFCS Display Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 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 rol
120. eeeees 6 24 Depari Go teat E AOO 6 25 Intercepting a VOR Radidl scsecssesesesesseesesseean 6 26 Flying a Flight Plan GPS COUrSE cssessessessesseeen 6 27 DESCON iraa i I N 6 28 N E AE EN TT E EES 6 31 Go Around Missed Approach sssssssssssssssssssssrsrrrrrnnn 6 33 6 6 AFCS Annunciations and Alerts 6 34 AECS SIE ATES uirre a an ney tcneceabenntc 6 34 Over pecd Prote Oisman 6 35 SECTION 7 NAVIGATION 7 1 7 4 Navigation Map Pag cccccseeeceen 7 1 7 2 Direct to Navigation 0 0 cc cece 7 1 Direct to Navigation trom the MFD 7 1 Direct to Navigation trom the PFD s 7 3 7 3 Navigating an Example Flight Plan 7 5 7 4 Airport Information 0 0 00 7 21 7 5 Intersection Information 0 0 0 ccce 1 23 7 6 NDB Information 0 0 cc ccc 7 24 7 7 VOR Information 0 c ccs eee 7 24 7 8 User Waypoint Information Page 7 25 7 9 Nearest Airports 0 0 0 7 25 Nearest Airport Information on the MFD cesse 7 25 Nearest Airports Information on the PFD 1 26 7 10 Nearest Intersections cccccssessesen 7 26 7 11 Nearest NDB 00 ccs 1 21 7 12 Nearest VOR 1 21 7 13 Nearest User Waypoint 111111eeeeeeeeeen 7 28 7 14 Nearest Frequencies c ccccseseeeeen 1 28 7 15 Nearest Airspace cscs 7 29 SECTION 8 FLIGHT PLANNING 0000000 8 1 8 1 User Defi
121. ence Guide for the Cessna Nav III 17 37 HAP TRAFFIC HAP 136 975 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 field 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Traffic a Traffic Out of aircraft is 400 below traffic Uut o Traffic Mode mae Mode climbing Range ING HDG UP UNRESTRICTED 7 A lag Non Bearing Traffic system Proximity Traffic is unable to determine bearing 1000 above amp distance is 8 0 nm 1190 above descending and descending Figure 10 13 Traffic Map Page 190 00384 08 Rev A Displaying Traffic on the Navigation Map 1 Ensure the KTA 870 system is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory MAP NAVIGATION HAP 136 975 118 000 con sto _NORTH UP al AMLE Non Bearing Traffic Off Scale Non Threat Traffic Advisories ihe Traffic Figure 10 14 TAS Traffic on Navigation
122. er passing OPSHN the next leg of the arrival turns magenta as shown in Figure 7 41 The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active FPL ACTIVE FLIGHT PLAN 136 975 z NORTH UP a OTH UF ACTIVE FLIGHT PLAN TFR KMKC KEOS HI DATA 118 088 corz Airwoy W26S TBE TEE cee a BE Arrival ECOS TBE DBRY 1 ALL OPSHN 3i Salk OPSHH a a M FSHER 2 TONHA T0O0OFT PY NOM 352 11 S0H TOEDUFT Approoch KOOS RMAY 3 amp Rioes LPW HABUK lof B21 5 SNH S000F1 FALUR 261 S NH B600 CEGIX fof 351 6 8NH CURRENT WHV PROFILE ACTIVE Ve WPT VS TGT V5 REG V DEV Figure 7 41 Tracking the OPSHN to FSHER Leg 20 The flight continues through the arrival procedure to PYNON see Figure 7 42 At a point 31 nautical miles trom 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 RVSI appear on the PFD as the flight progresses 190 00384 08 Rev A SECTION 7 NAVIGATION Turn right to 21 in 8 seconds TOD within 1 minute 136 975 PL ACTIVE FLIGHT PLAN NORTH UP ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS TEE enti pasate RAY Arrival KCOS TBE DBRY 1 ALL OPSHN 3mh OPSHN FSHER S
123. errain Awareness amp Warning System 2 Press the ALT UNIT Softkey unless TAWS is inhibited 3 Press the METERS Softkey to display altitude in meters When the Final Approach Fix FAF is the active 4 Press the HPA Softkey to display the barometric waypoint in a GPS WAAS approach using vertical guidance setting in hectopascals Press the IN Softkey amp LOW ALT Low Altitude annunciation may appear if to display the barometric setting in inches of the current aircraft altitude is at least 164 feet below the mercury prescribed altitude at the FAF The annunciation initially flashes After a few seconds the flashing stops and the annunciation is displayed as shown in Figure 2 10 1219MT Low Altitude E 4000 Annunciation 5 Press the BACK Softkey to return to the previous level softkeys Figure 2 10 Low Altitude on GPS Approach 1U13HPA Figure 2 9 Altimeter Metric 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 5 SECTION 2 FLIGHT INSTRUMENTS 2 4 VERTICAL DEVIATION GLIDEPATH GLIDESLOPE INDICATOR The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior 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 k 2 7 f f Target z Altitude Vertical Deviation Requ
124. es 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 Joystick Changes the map range distance top to 190 00384 08 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 knob 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 Contro
125. ess than 50 ft In this case the Selected Altitude becomes the flight directors 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 the desired altitude the new altitude is established as the Altitude Reference 190 00384 08 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL 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 Flight Director Alti Mode Active tude Reference navi 1 13 08 gt 118 98 IIxD amp EMCI ts P30 065 133 000 e 118 708 com Nave 115 I0 118 3H TIXO ROL ALT 114 er 123 SHB 135 325 conz Selected Altitude gt Selected Altitude Bug Command Bars Holda Pitch Attitude to Main tain Altitude Reference TAS 1O KTI POIR 1200 STBY LEL 233 06H 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 Vert
126. essure 1 Press the PFD Softkey Barometric E 2 Press the STD BARO Softkey Altitude Minimums Bug Barometric Altitude Alerting Within 1000 ft Within 200 ft Deviation of 200 ft Figure 2 7 Altimeter e dana E 4o00 Selected Altitude Bug a _ Figure 2 8 Altitude Alerting Visual Annunciations The Selected Altitude Bug is displayed at the Selected Altitude or the edge of the tape whichever is closer to the Visual annunciations appear in the Altitude Reference current altitude to provide increased altitude awareness Box Whenever the setting is changed the Altitude and to set the desired hold altitude for the autopilot Alerter is reset The Altitude Alerter is independent of the Set the Selected Altitude Bug Automatic Flight Control System 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 2 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 2 FLIGHT INSTRUMENTS Metric Display Low Altitude Annunciation Display altitude in meters and barometric A NOTE The LOWALT annunciation is only available pressure in hectopascals in G1000 systems configured with WAAS capable 1 Press the PFD Softkey to display the second level GPS Also the LOW ALT annunciation is not softkeys available when the G1000 is configured with TAWS T
127. ffic 3 Press the small FMS Knob to return to the Navigation Map Page PAGE MENU OPTIONS Mop Setup Declutter Measure Bearing Distance Show Chart STRMSCP SMEL NEXRAD DATA NEXRD CELL HOV 4 Cn XM LING Off e 2AOCNM Figure 10 2 Map Setup Menu MAP SETUP GROUP erties Mop dent On Traffic E All Traffic iot Land L 150NH narra Lou SONH Figure 10 3 Map Setup Group List 190 00384 08 Rev A TOPO TERRAIN SECTION 10 HAZARD AVOIDANCE 10 2 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 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page 136 975 118 000 coe isan a ie A I NORTH UP T pn LTNING HIDE CELL RATE 3 Figure 10 4 In Flight Navigation Map Page Displaying Stormscope Lightning Data Lightning Age Symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old foe Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 1 SECTION 10 HAZARD AVOIDANCE At a map range of les
128. ffic 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 08 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS 12 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 Commet 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 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
129. g 3 8 Used 3 8 Fuel Flow 3 1 3 3 3 4 3 8 Fuel Quantity 3 2 3 4 3 8 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 6 31 GMA 1347 1 1 Go Around Mode 6 33 6 34 Go Around Mode GA 6 16 Heading indication 2 9 Heading Select 1 3 1 4 Heading Select Mode 6 18 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 13 Impact point 10 13 Inhibit 10 12 Interrogations 4 5 IOI 10 13 10 16 12 5 ITI 10 13 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III K Key s 1 4 L Leaning 3 7 Leaning Engine 3 4 Lean Display 3 1 3 4 3 5 3 6 Lighted obstacle 10 15 Lightning 1 5 1 9 10 2 10 3 10 4 LNAV 2 6 7 5 Load approach 8 6 Load a VOR frequency 7 27 Load departure 8 6 Load the frequency for a controlling agency 7 29 Load the nearest ARTCC frequency 7 28 LOI 2 11 LOW ALT 2 5 Low Altitude 2 5 LPV 2 6 6 24 7 5 7 20 Manifold Pressure 3 1 3 3 3 4 3 6 3 8 3 10 Manual Electric Trim MET 6 22 MAP 7 1 Map panning 10 5 Marker beacon 2 7 Message advisories 12 2 12 10 12 15 12 17 12 22 METAR 10 3 10 5 Metric display 2 4 MET Switch Manual Electric Trim 6 1 MFD 1 1 4 4 Minimums 12 6 Missed approach 6 33 MKR MUTE 5 2 5 4 Mode S 4 4 Mod
130. gly 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 46 when the final approach course becomes active FPL ACTIVE FLIGHT PLAN 136 975 118 608 conz DOLOR PO SPRI i5 NORTH UP ACTIVE FLIGHT PLAN KCO TFR KMKC KCOS NO DATA c rr Es DTK HE FSHER EDE hee PYNON ae a eee Approuch KCOS RNAV 3SRoes LPV HABUK iof wea hea ae FALUR a a L CEGIX fof 351 5 5m RHSSR map 351 5 1NM 6366FT 346 8 4NN MOGAL aahp HOLD CURRENT VNV PROFILE ACTIVE UNV WPT a VS TGT TERRAIN s 1009r1 100011 m feet a 30Nn CNCL VNV 190 00384 08 Rev A 10000 Figure 7 46 Descending to the FAF SECTION 7 NAVIGATION 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 the ALT field in Figure 7 46 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 47 FPL ACTIVE FLIGHT PLAN 196 975 118 688 conz Eki WURIH U ACTIVE FLIGHT PLAN iL E ays Regs TFR KMKC KCOS R i DATE A HI DATA i BJGBFT DTE prs FSHER Moyo a os ea 3 PYNON pean EA
131. he 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 08 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 gt STORED FLIGHT AAN 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 identitier 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 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 re
132. he 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 The MFD and or PFD detected a failure in the SateTaxi database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced problem persists the G1000 system should be serviced DB MISMATCH Aviation database The PFD and MFD have different aviation database versions installed Crosstill is version mismatch Xtalk is off off Install correct aviation database version in both displays DB MISMATCH Aviation database The PFD and MFD have different aviation database types installed Americas type mismatch Xtalk is off European etc Crossfill is off Install correct aviation database type in both displays DB MISMATCH Terrain database The PFD and MFD have ditterent terrain database versions installed Install version mismatch correct terrain database version in both displays DB MISMATCH Terrain database The PFD and MFD have different terrain database types installed Install correct type mismatch terrain database type in both displays DB MISMATCH Obstacle database The PFD and MFD have different obstacle database versions installed Install version mismatch correct obstacle database version in both displays D
133. he 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 onto the active leg as seen in Figure 7 22 136 975 118 888 conz ACTIVE FLIGHT PLAN KMKC KCOS Airvoy j Airway 244 LAA LAA Airway V263 TBE TRE CURRENT UNU PROFILE ACTIVE VNV WPT FT at VS TGT i FPH FPA ih Q FP 0 TO TERRAIN VS REQ M TIME TO TOD 100rt 1000r1 s 30nn Figure 7 22 Turn on to Active Leg 8 At SLN Victor Airway 244 V244 is intercepted Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 7 23 Turn right to 262 in 3 seconds MTAA A T E E 136 975 il ts P rage A ji woo git pe gt oe a a Figure 7 23 Turn to Intercept V244 9 As seen in Figure 7 24 V244 is now the active flight plan leg ACTIVE FLIGHT PLAN 136 975 Lr TFR KMKC KCOS NO DATA NSS tE Enroute Tre Airwoy V4 SLN Airwoy V244 LA48 HYS LAA PO Airway VER TBE 75 18 KCOS Arrival KOOS TBE DBRY 7 ALL CURRENT VNV PROFILE ACTIVE VNV WPT T VS TGT TERRAIN VS REQ FPM TIME TO TOO V DEV FT 100 1000F 1 ZONH CNCL VNV Figure 7 24 V244 Now Active Leg rere Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 10 At Lamar VOR LAA V263
134. hen 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 08 Rev A Pitch Hold Mode PIT When the flight director is activated the FD Key is pressed Pitch Hold Mode is selected by default Pitch Hold Mode is indicated as the active pitch mode by the green annunciation PIT This mode may be used for climb or descent to the Selected Altitude shown above the Altimeter since Selected Altitude Capture Mode is 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 Mode Active navi 1 13 08 lt gt 118 98 IIXD eee fae ae nav2115 98 118 98 IIXD Command Bars Mai tain Desired Pitch Reference SECTION 6 AUTOMATIC FLIGHT CONTROL Changing the Pitch Reference When operating in Pitch Hold Mode the pitch reference can be adjusted by e Using the NOSE UP NOSE DN Keys e Pressing the CWS Button hand flying the aircraft to establish a new pitch reference then releasing the CWS Button Selected Altitude Capture Mode Armed 118
135. ht 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 changes from light blue to amber in color Garmin G1000 Cockpit Reference Guide for the Cessna Nav III minutes SIGMETSIAIRMETs oo City Forecasts w CountyWarnings f 6 CydoneWamings f 6 Freezing Leves fo oo r Surface Analysis fo oo mes Cid WindsAloft wo ms CT o Oo O Clouds Tops 190 00384 08 Rev A 10 4 TRAFFIC SYSTEMS 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 Soitkey is displayed Traffic Information Service TIS Displaying Traffic on the Traffic Map Page NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site NOTE If the G1000 is configured to use a Traffic Advisory System TAS TIS is not available for use
136. ht 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 Path Tracking Mode To proceed with descent path capture if the white VPTH annunciation begins flashing do one of the following _ D ALT Mode 2 Cruise Altitude of 12 000 MSL sta Figure 6 35 VPTH Descent SECTION 6 AUTOMATIC FLIGHT CONTROL e Turn the ALT Knob to adjust the Selected Altitude e Press the VNV Key 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 SS GPS AP ALT The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude the autop
137. ht 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 08 Rev A SECTION 10 HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Displaying Terrain on the TAWS Page Navigation Nap 1 Turn the large FMS Knob to select the Map Page 1 With the Navigation Map displayed press the MAP Group Softkey 2 Turn the small FMS Knob to select the TAWS 2 Press the TERRAIN Softkey Terrain and obstacle Page proximity is now displayed on the map 3 If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed 10 6 TERRAIN AWARENESS amp WARNING a radar like 120 view is displayed Press the 360 SYSTEM TAWS DISPLAY Softkey to return to the 360 default display OPTIONAL 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller NOTE Terrain data is not displayed when the aoe aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Terrain Obstacle Location Terrain Obstacle above or within 100 below or above aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Black Terrain Obstacle is more than 1000 below aircraft altitude I I Poten
138. ical 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 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 Reference is shown on the indicator 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 7 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Speed a Selected Altitude Capture Mode Active Referen Mode Armed navi 113 00 110 30 IIXD LETE 3 08 133 808 com nav2119 96 118 98 TIXD ROL VS T1000 ALTS 123 800 gt 135 325 conz S y pa y 1t dow Fe meal mmn ees teed Spee ALL wa Vertical Speed 1400 Reference Vertical Speed Reference Bug Command Bars E Indicate Climb to Attain Vertical Speed XPOR 1200 SIBY CL 254 21eH Figure 6 8 Vertical Speed Mode Changing 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
139. if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix 190 00384 08 Rev A SECTION 10 HAZARD AVOIDANCE Manual System Test calculated to come within minimum clearance altitudes in the following table A system test is automatically performed at power up After successful completion of the test TAWS System Phase of Flight Level Flight Descending Test OK is heard 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 proper operation of the aural and visual annunciations of the Pan perlorm the none ay During the final approach phase of flight RTC ROC 1 While the TAWS Page is displayed press the MENU r1 10 alerts are automatically inhibited when the aircraft Key is below 200 feet AGL while within 0 5 nm of the approach 2 Turn the small FMS Knob to select Test TAWS runway or is below 125 feet AGL while within 1 nm of the 3 Press the ENT Key During the test TAWS TEST is runway displayed in the center of the TAWS Page Premature Descent Alert PDA oe WORK EE EA EE A Premature Descent Alert is issued when the system detects that the aircraft is significantly below the normal Forward Looking Terrain Avoidance FLTA 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
140. ight 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 e 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 11 2 Extreme Pitch Indication 11 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 11 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 11 3 BUUUOU Figure 11 3 Loss of Hazard Functions with Loss of GPS Position 190 00384 08 Rev A 11 6 DEAD RECKONING WARNING DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lac
141. ilot 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC 6 30 FLIGHT CONTROL Non path descent using Flight Level Change Mode 1 Command a non path descent using Flight Level Change Mode a Using the ALT Knob set the Selected Altitude below the current aircraft altitude to an alti tude in this case 9 400 feet at which to level off between VNV flight plan altitudes b Press the FLC Key before the planned TOD during an altitude hold while VPTH is armed The Airspeed Reference defaults to the current aircraft airspeed Vertical Path Tracking and Selected Altitude Capture Mode are armed automatically J GPS AP ALTS VPTH 2 Reduce power to allow descent in Flight Level Change Mode The autopilot maintains the Airspeed Reference 3 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 Selected Altitude of 9 400 MSL OPSHN E 3 nn A E GPS AP ALT __VPTH 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 th
142. ion 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 automatically 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 08 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL SECTION 6 AUTOMATIC FLIGHT mien inn 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 Gf in Roll Hold Mode The CWS Button is located on the top of the pilot s cont
143. ired Indicator Vertical Speed 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 approach has been activated and an ILS is tuned in the active NAV receiver field see Figure 2 13 Marker Beacon Annunciation Glideslope Indicator Figure 2 13 Glideslope Indicator 190 00384 08 Rev A 2 5 MARKER BEACON ANNUNCIATIONS Outer Marker Middle Marker Inner Marker Altimeter 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 08 Rev A SECTION 2 FLIGHT INSTRUMENTS 2 7 BAROMETRIC ALTITUDE MINIMUMS The desired barometric altitude 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 4 BARO 1560FT Figure 2 16 Barometric Minimum Descent Altitude Settings The desired barometric minimum descent altitude MDA or Decision Height DH can be set in the Timer
144. iving 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 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 A 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
145. k 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 11 4 In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in Figure 11 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 08 Rev A SECTION 11 ABNORMAL OPERATION Nor
146. ke control of the aircraft and disengage AP or stuck MET Switch If AP disengaged move MET switches separately to unstick Roll Failure ROLL Roll axis control Roll axis control failure AP inoperative AP Roll axis control failure AP inoperative Pitch Failure PTCH Pitch axis control failure AP inoperative System Failure les Oss 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 preflight system test to fail or never Preflight Test to start if servos fail their power up tests Power must be cycled to the servos to remedy the situation PFT Preflight system test failed aural alert sounds at failure Table 6 4 AFCS Status Field Alerts 6 34 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 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
147. l tank left L and right R When full the indicator displays to 35 gallons per side 26 gallons for the Models 172R and 1725 11 Voltmeter M E BUS VOLTS Displays the main and essential bus voltages 12 Ammeter M S BATT AMPS Shows the main and standby battery load in amperes 190 00384 08 Rev A 61 8 OIL F FUEL CALC 0 2 OOO OO FUEL QTY w Er T A 16 ra F ELECTRICAL a BUS EC 38 2 vms Mo H BATT 5 12 0 0 AMPS 6 0 Model 172R 190 00384 08 Rev A 59 6 OIL F FUEL CALC 4 0 4 8 Soc So FUEL QTY A 16 Pa F ELECTRICAL MH BUS EC M BATT S 12 0 46 AMPS 4 4 Model 172S SECTION 3 ENGINE INDICATION SYSTEM EIS MAN IN Ee i _ 58 2 ENG 043 7 HRS a 50 0 ENG 085 3 HRS 2 VAC VAC CC o A FUEL CALC FUEL CALE O FFLOW GPH 12 0 O na GAL USED 1 1 O 6 8 GAL REM Si 2 FUEL TY GAL 9 FUEL QTY GAL Z me H 16 276 SH F H 16 76 3h F ELECTRICAL ELECTRICAL M 3 p E Qe 292 vours 000 MG e245 volts 245 M BATT 5 M BATT 5 2 C OO Model 182T Figure 3 5 System Display Normally aspirated Aircraft Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Model 206H 39 SECTION 3 ENGINE INDICATION SYSTEM EIS COO OOOO A AN MAN IN 213 gt RPM OIL PSI 57 0 OIL F 200 ENG AHAH HRS VAC
148. l FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7 3 IDENT FACILITY CITY KSLN H CEN USA sa 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 8 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 IDENT FACILITY CITY KSLH W N CEN USA mie Dd 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 f 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 08 Rev A 3 4 5 6 DIRECT TO m IDENT FACILITY C
149. l Up Terrain Ahead Pull 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 Five Hundred Sink Rate Don t Sink or Too Low Terrain SECTION 12 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 12 6 OTHER G1000 AURAL ALERTS Aural Alert The aircraft has descended below 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 tra
150. l 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 the flashing annunciation stops and the flight director enters the default mode for the affected axis Figure 6 4 Loss of VOR Signal 190 00384 08 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 Al
151. lay 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 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 190 00384 08 Rev A 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
152. lays vacuum pressure Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 3 ENGINE INDICATION SYSTEM EIS 322 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 11 Engine Hours Tach ENG HRS Models 172R and 172S A numeric readout gives the time in hours the engine has been in service FFLOW GPH iii H OIL PRES OIL TEMP A EGT Laria WI VAC E a FUEL QTY E r H 18 24 F ENG 6000 2 HRS ELECTRICAL Model 172R 0 0000 QIL PRES OIL TEMP pA A EGT Lar VAC FUEL QTY E E T FFLOW GPH H oe OIL PRES OIL TEMP a coal CHT 4 EGT Lr rrr HY 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 RPM SHH 2100 FFLOW GPH OIL PRES me C a OIL TEMP CHT O V EGT UWr 5 16 a F FUEL QTY GAL ENG AHHH HRS Ds ELECTRICAL 6 16 278 36 OF M BUS E ELECTRICAL 7 VOLTS 0 0 M BATT 0 6 AMPS OO Model 172S Model 182T Figure 3 1 Engine Display Normally aspirated Aircraft Garmin G1000 Cockpit Reference Guide for the Cessna Nav III FUEL QTY GAL a
153. le varies if Vectors To Final is activated Drawing not to scale Drawing not to scale o 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 08 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 fee n f Information Bearing 1 Bearing Window Pointer Pointer CDI Bearing Bearing 2 Information Information Window Window Figure 2 25 HSI with Bearing Information Distance to Bearing Source Waypoint Identifier Bearing Pointer Source Icon Figure 2 26 BRG1 Information Window 190 00384 08 Rev A SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source Waypoint Identifier 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 Figure 2 28 DME Information Window 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 L
154. lies 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 08 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 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 the
155. light 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 Change Modes 190 00384 08 Rev A SECTION 1 SYSTEM OVERVIEW 1 2 PFD SOFTKEYS TERRAIN Softkey ON Softkey OFF optional pe e SN TN nnn n nN Mnnnn D VOR1 on HSI VOR2 on HSI GPS on HSI Figure 1 2 PFD Top Level Softkeys he nnnnn n n a Ao a 190 00384 08 Rev A he A Press the BACK or OFF Softkey to return
156. ll 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 Terrain Pull Up Pull Up Reduced Required Obstacle Clearance PULL UP Obstacle Obstacle Pull Up Pull Up Warning ROC or or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact Warning IOI PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up or 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 Aural Message Reduced Required Terrain Clearance Caution RTC Imminent Terrain Impact Caution ITI Caution Obstacle Caution Obstacle or Obstacle Ahead Obstacle Ahead Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Too Low Terrain Five Hundred Sink Rate Reduced Required Obstacle Clearance Caution ROC Imminent Obstacle Impact Caution IOI Premature Descent Alert Caution PDA Altitude Callout 500 Excessive Descent Rate Caution EDR Don t Sink or Too Low Terrain Negative Climb Rate Caution NCR ee 10 16 Garmin G1000 Cockpit Reference Guide for the Cessn
157. ls 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 used 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 selec
158. lso cancels the flashing AP an nunciation Autopilot Manually Disengaged E PT ALTS Figure 6 29 Manual Autopilot Disengagement Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 23 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 5 EXAMPLE PROCEDURES A NOTE The diagrams in this section are for instruc tional purposes only and should not be used for navigation This section provides a scenario based set of procedures showing various GFC 700 AFCS modes used while following a previously entered flight plan The following example closely follows the example flight plan discussed in the Navigation section Refer to the example in Section 7 Navigation when studying the this example 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 after following heading vectors of 240 and 290 assigned by ATC Airway V4 is flown to Salina VOR SLN using VOR navigation then airway V244 is flown using a GPS flight plan The ILS approach for runway 35L and LPV WAAS approach for runway 35R are shown and a missed approach is executed KCOS Salina VOR SLN Figure 6 30 Flight Plan Overview 6 24 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A Departure Climbing to the Selected A
159. ltitude and flying an assigned heading 1 Use the ALT Knob to set the Selected Altitude to 12 000 feet after takeoff Depart KMKC 2 In this example Vertical Speed Mode is used to capture the Selected Altitude Pitch Hold Vertical Speed or Flight Level Change Mode may be used a Adjust the aircraft s vertical speed to the desired 1 000 fom b Press the VS Key to activate Vertical Speed and Roll Hold modes and arm Selected Altitude Capture Mode The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP DN Key or pushing the CWS Button while hand flying the aircraft to establish a new Vertical Speed Reference 40 G Mou To Mode ys wor SECTION 6 AUTOMATIC FLIGHT CONTROL c Press the AP Key to engage the autopilot in a climb using Vertical Soeed Mode _ ROL AP ALTS 3 Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb Use the HDG Knob to set the Selected Heading complying with ATC vectors to intercept Airway V4 The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading LOG AP ALTS 4 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 _ HDG AP ALT At 50 feet from the Selected Altitude the green ALT annunciation fla
160. ltitude 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 or loaded from a database see the Navigation section for details At the same time as 190 00384 08 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL 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 Target 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
161. m 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 11 1 G1000 Reversionary Mode Failed PFD 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 1 SECTION 11 ABNORMAL OPERATION 11 2 11 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 11 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 e Traffic Annunciations e Windows displayed in AFCS Annunciations the lower right corner Flight director Com of the PFD mand Bars Timer References e Inset Map Nearest Airports e Temperatures Fl
162. mal 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 aircraft 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 11 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 and MFD Track Bug e All Bearing Pointer Distances e Active Flight Plan distances bearings and ETE values Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 11 3 SECTION 11 ABNORMAL OPERATION Also while the G1000 is in DR Mode
163. n guidance e An altitude 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 calculations 190 00384 08 Rev A SECTION 1 SYSTEM OVERVIEW WhiteText Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system Altitude has been entered by the The system cannot use this altitude estimating the altitude of the pilot Altitude is designated for in determining vertical speed and aircraft as it passes over the use in giving vertical speed and deviation guidance navigation point This altitude deviation guidance Altitude does is provided as a reference and not match the published altitude is not designated to be used in in navigation database or no determining vertical speed and published altitude exists deviation guidance Small Text Altitude is not designated to Altitude is designated for use in The system cannot use this altitude be used in determining vertical giving vertical speed and deviation in determining vertical speed and speed and deviation guidance guidance Altitude has been deviation guidance Altitude has been retrieved from retrieved trom the navigation the navigation database and is database or has been entered by provided as a reference the pilot and matches a published altitude in the navigation database Table 1 1 VNV Altitude Text Size and
164. n point as shown in Figure 7 13 The V4 entry point TOP is placed immediately above the highlighted waypoint SLN ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS Departure KMKC ALL TIFTOZTIFT MCI TIFTO 206 S 2NH Enroute SLN 90 3NH Airvoy V244 LAA HYS 262 TAINH LAA 251 16D Airway V263 TBE TBE Eo FI KCOS ee ha CURRENT VNV PROFILE ACTIVE UNU WPT ___ Figure 7 13 Begin Adding V4 to the Flight Plan 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION c Turn the small FMS Knob to display the Waypoint Information Window Enter the desired beginning point for V4 leg in this example Topeka VOR TOP is used as shown in Figure 7 14 BAYPOINT INFORHAT ION IDENT FACILITY CITY TJ TOPEKA TOPEKA BS piee NORTH UP ag Hee MENEH OPEKA LOCATION BRG AZ DIS 22 9NH Fress ENT to occept 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 ACTIVE FLIGHT PLAN KMEC KOOS MCI TIFTO Enroute TOP zz Airvoy V244 LAA HS LAA Airway Y263 TBE KEUS CURRENT VHW PROFILE ACTIVE WNW WPT _____ Feo Seales WS TGT FPH FPA VO REQ FPA TIRE TO TOD Figure 7 15 TOP Inserted into the Flight Plan I SECTION 7 NAVIGATION e With SLN still highlighted as in Figure 7 15 turn ere the small FMS Knob to the right The
165. n the FREQUENCY field Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 2 SECTION 7 NAVIGATION 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 ir tape Ae REFERENCE WAYPOINTS EEPE LONII Figure 7 63 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 7 28 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III Waypoint Page pertains to the selected Nearest User Waypoint 3 Press the FMS Knob to remove the flashing cursor 7 14 NEAREST FREQUENCIES em DAIA Ze TER PL Figure 7 64 Nearest Frequencies Page Select the Nearest Frequencies Page 1 Turn the large FMS Knob to select the NRST page 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
166. n 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 2 Key 2 Turn the small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7 8 DT RECT TO KMTA HIAHI FL KIXD KSLN OYATI inf DIGBE OFFSET aNH ors 18 4NxK 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 J 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 pop
167. nce 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 12 4 Pressing the ADVISORY Softkey acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts Window 12 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 12 2 NAV Ill AIRCRAFT ALERTS The following alerts are configured specifically for the Cessna Nav III aircraft See the Cessna Pilots Operating Handbook POH for information regarding pilot responses WARNING Alerts Aural tone is inhibited while the aircratt is on the ground KAP 140 installations only CAUTION Alerts Annunciation Window Text Audio Alert Single Aural Tone Single Aural Tone Single Aural Tone Single Aural Tone CAUTION Alerts T182 T206 and 206 with Prop De Ice Only Annunciation Window Text Audio Alert Single Aural Tone 190 00384 08 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS Safe Operating Annunciation T182 T206 and 206 with Prop De Ice Only Annunciation Window Text Audio Alert 12 3 CO GUARDIAN MESSAGES Alerts Window Message Comments CO DET SRVC The carbon There is a problem within monoxide detector needs the CO Guardian that
168. nd Mode disengages the autopilot and arms Altitude Hold Mode automatically Subsequent autopilot engagement is allowed Attempts to modify the aircraft attitude Q e with the CWS Button or NOSE UP NOSE DN keys result in reversion to Pitch and Roll Hold modes Go Around Mode Active nw 111 90 114 18 SJC 118 200 196 975 con1 tava 113 80 l F 136 975 118 888 conz 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 08 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 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 information regarding Go Around and SECTION 6 AUTOMATIC FLIGHT CONTROL The CWS Button does not change lateral references for Heading Select Navigation Backcou
169. nd 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 left 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 GPSa GPS Je ALTS Figure 6 24 GPS 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 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 It Approach Mode is active and either of the following occur the flight director reverts to Roll Hold Mode wings rolled level Vectors to Final is activated e Navigation sour
170. ndicator nana 2 6 2 5 Marker Beacon Annunciations 2 7 2 6 Vertical Speed Indicator 0 ccceees 2 7 2 7 Barometric Altitude Minimume 2 7 2 8 Horizontal Situation Indicator HSI 2 8 Course FONE earns E 2 9 Course Deviation Indicator CDI 2 9 Bearing Pointers and Information Windows 2 11 DME OPTION esnan S 2 11 Navigation SOUPCES eninin sass 2 11 2 9 Wind Data ccc ccsesseeseeseestesseeseanes 2 12 2 10 Generic Timer oo cece eestessees testes teaees 2 13 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 3 1 190 00384 08 Rev A Engine Display 0 0 ccccccccscesseestesseestesseeseeaees 3 1 TABLE OF CONTENTS 3 2 Lean Display sciiie hos cece eee he hee 3 4 Normally aspirated Aircraft c ssesessessessessesseesesssen 3 7 TUM OCM ai OCC Airera aaea 3 7 3 3 System Display 0 cece 3 1 SECTION 4 NAV COM AND TRANSPONDER 4 1 4 1 Radio Status Indications 4 3 42 Volume noensinne 4 3 4 3 Automatic Squeleh seen 4 3 4 4 Quickly Activating 121 500 MHZ 4 3 4 5 Optional NAV Radios 0cccceseeeen 4 3 DME Radio optional arisane 4 3 ADF Radio optional ct icacescsinensasennarenunenreneinarveunanenes 4 4 4 6 Frequency Auto tuning cccc een 4 4 Autotuning onthe PED scscstcanspeseincasesuranenteaaseueiunesanun 4 4 Auto tuning on the MFD scsssssssssas
171. ned Waypoints 051151111111111112 8 1 Select the User WPT Information Page c 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 i Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 8 4 Activate a Flight Plan Leg 0 ce 8 3 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan 8 3 8 7 Create a New Flight Plan 0 0 8 4 Create a New Flight Plan Using the MFD uu 8 4 Create a New Flight Plan Using the PFD uo 8 4 8 8 Enter an Airway in a Flight Plan 8 5 8 9 Load a Departure ou ccs 8 6 8 10 Load an Arrival ccs ees 8 6 8 11 Load an Approach ou cscs 8 6 8 12 Remove a Departure Arrival Approach or Airway from a Flight Plan ceeeeen 8 6 8 13 Store a Flight Plain cesses 8 6 8 14 Edit a Stored Flight Plan 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 cee 8 7 8 18 Delete a Flight Plan ou seen 8 8 8 19 Graphical Flight Plan Creation 8 8 8 20 Trip Planning 8 8 SECTION 9 PROCEDURES 0 0 0 oc 9 1 9 1 Arrivals and Departures 0551551111111111111 9 1 Load and Activate a Departure P
172. ng Table 6 3 Roll Hold Mode Responses NOTE Pressing the HDG Knob synchronizes the Changing the Roll Reference Selected Heading to the current heading The roll reference can be changed by pressing the CWS The Selected Heading is adjusted using the HDG Knob Button establishing the desired bank angle then releasing on either display Pressing the CWS Button and hand the CWS Button 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 Heading Select Mode Active Pitch Hold Mode Active naval 11 98 114 10 se ee on DIS _ 118 200 136 975 cont nw2113 88 118 98 IsJc ee ALTS 136 975 118 000 conz Command Bars Track Selected Heading Selected Heading Selected Heading Bug XPDOR1 1253 ALT Ff jLCL 5 5643PH Figure 6 21 Heading Select Mode 6 18 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 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 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 Na
173. nnunciations LOC HDG AP ALT 100001 GS c The navigation source automatically switches to LOC After this switch occurs the localizer signal can be captured and the autopilot and flight director determine when to begin the turn to intercept the final approach course 3 There are two options available at this point as the autopilot flies the ILS 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 SECTION 6 AUTOMATIC FLIGHT CONTROL KCOS PoN SO lddV 901 PETEY Y PON AVN Sd9 Figure 6 37 ILS Approach to KCOS 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 31 SECTION 6 AUTOMATIC FLIGHT CONTROL Flying a WAAS precision approach KCOS 1 Arm flight director modes for a precision approach a Make sure the navigation source is set to GPS use CDI Softkey to change navigation source b Load the Runway 35R LPV approach for KCOS into the flight plan apo d9 dY Sd9 2 Press the APR Key once clearance for approach has 38 been acquired GPS Approach Mode is activated and Glidepath Mode is armed _ GPS APL VPTE 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
174. ntained 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 C Aircraft Wing Tips Roll Scale 7 Pitch Scale G Horizon Line Slip Skid Indicator 4 Aircratt Symbol E Sky Representation G Land Representation Roll Index Zero 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 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 2 3 SECTION 2 FLIGHT INSTRUMENTS 2 3 ALTIMETER Altitude Trend Vector Altitude The end of the trend vector displays approximately Altitude Reference what the altitude will be in six seconds if the current rate aii am of vertical speed is maintained Barometric Setting Box Select barometric pressure eg one Turn the BARO Knob to select the desired Vector Alginde setting Quickly enter standard pr
175. o the Missed Approach Hold Point MAHP In this case the altitude fix would be labeled 5500rFt Again if the aircraft altitude is lower than this prescribed altitude a direct to is established to this fix 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 oy 3 A direct to is initiated to MOGAL which is the Missed Approach Hold Point MAHP as seen in Figure 7 48 The aircraft is climbing to 10 000 feet The CDI flight phase now changes from LPV to MAPR as seen on the HSI r P WORTH UF active FLIGHT PLAN TFR KMKC KDOS Tal DATA a FSHER PYNON Approach KCOS RNAV 35Rices LPW HABUK iof k CURRENT VNV PROFILE ACTIVE VV WPT ____FT at 1 V5 TGT EET REG TERRAIN gt PEO I V OEY lRDrT m 1000r M E w CNCL VNV 10 10 39 Yag I Z spi o Figure 7 48 Missed Approach Active 710 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 7 NAVIGATION 26 The aircraft continues climbing to AT or ABOVE 7 4 10 000 feet at MOGAL A holding pattern is established at the MAHP MOGAL as shown in Figure 7 49 AIRPORT INFORMATION 136 975 118 888 corz 136 975 ACTIVE FLIGHT PLAN KMKC
176. oftkey 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 23 illustrates the envelope for alerts 10 14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 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 116 80 116 000 cor NORTH OF Figure 10 24 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 25 TAWS Symbols 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 15 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 Pu
177. old Mode Unless NAV Key is Pressed Figure 6 33 Transition to GPS Flight Plan 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 6 27 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 28 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 Alti 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
178. olely 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 according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp G WARNING Because of anoma
179. ons to Selected Altitude 190 00384 08 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds J GPS TAP B01 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 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 6 Om NOGAL ozs BRG PON AVN Sd9 apo VO Y Figure 6 39 Go Around Missed Approach Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC 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 1 13 88 110 90 IIXD nav2115 98 110 90 IIXD AFCS Status Annunciation Figure 6 40 AFCS Status Annunciation Alert Condition Aileron Mistrim Right Roll servo providing sustained force in the indicated direction Aileron Mistrim Lett Elevator Mistrim Down Pitch servo providing sustained force in the indicated direction Elevator Mistrim Up Pitch Trim Failure PTRM If AP engaged ta
180. oviding sustained force in the indicated direction 12 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A 12 5 TAWS ALERTS SECTION 12 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 Premature Descent Alert Caution PDA Altitude Callout 500 Excessive Descent Rate Caution EDR bad or TOO LOH TERRAIN Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 5 Negative Climb Rate Caution NCR 190 00384 08 Rev A PFD MFD TAWS Page Annunciation Excessive Descent Rate Warning EDR PULL UP PULL UP PULL UP AAE 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 Pul
181. play the RECENT airports as shown in Figure 7 54 AIRPORT KHCI Figure 7 54 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 from which to choose the desired location 6 To remove the flashing cursor press the FMS Knob 190 00384 08 Rev A SECTION 7 NAVIGATION Access Runway Information 7 5 INTERSECTION INFORMATION 1 With the Airport Information Page displayed press Select the Intersection Information Page the FMS Knob to activate the cursor 2 Turn the large FMS Knob to place the cursor on the 1 Turn the large FMS Knob to select the WPT page RUNWAYS identifier field ser 2 Turn the small FMS Knob to select the second rectangular page icon 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
182. plete 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 SateTaxi 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 November 2007 190 00384 08 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 O WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain function The G1000 Terrain Proximity 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 aware of surroundings during flight The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system Terrain data is obtained from third party sources Garmin is not able
183. proaches 190 00384 08 Rev A 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 AIRPORT KCOS P PUBLIC COLORADO SPRINGS CO APPROACH CHANNEL CHANNEL 97799 10 HISA ri SS e RNAV 35Reps LPV TRANSITION VEC TORS quency LIIDRAKE jrw HABUK inf FALUR NM CEGIX fof B N RYS5R mop BIH BaSSFT 348 0 O HOGAL mohp LOAD oR 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 7 13 SECTION 7 NAVIGATION h With LOAD highlighted again press the ENT Key The selected approach is added to the flight plan as seen in Figure 7 33 FPL ACTIVE FLIGHT PLAN 136 975 118 808 conz Billa il ACTIVE FLIGHT PLAH KMKC KOOS E N e Arrival KCOS TBE DBRY1 ALL OPSHN 3M fou BBSNH TPCODF OPSHN 259 FSHER Jz OLSNH PY AOH 5 el nn Approoch KCOS RMAY 35Riors LPY HABUK iof a1 5 SNN S000 FALUR 251 BANA J NNI F CURRENT VNV PROFILE ACTIVE We WET TOOOGFT at OPSHN Jhr VS TGT JFF FPA 25 VG REG 24 TERRAIN gt E T 100Fr gl 1000FT N SAE FPL z VIEH VHV
184. ption 1 e Wind direction arrow and speed Option 2 e Wind direction arrow with direction and speed Option 3 Option 1 Option 2 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 08 Rev A 2 10 GENERIC TIMER REFERENCES 164 nO 40a Oe a ART REFERENCES TIMER 00 25 05 DN SUUM REFERENCES TIMER 00 25 13 UP ies Figure 2 31 Timer Status Prompts Change the Generic Timer 1 190 00384 08 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 press 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 2 14 Garmin G1000 Cockpit Reference Guide for
185. rence Window 4 6 REFERENCES TIMER OPAVA UP START GLIDE SSKT OFF MINIMUMS BARO 1568FT FLIGHT ID AIR265 Flight ID Figure 4 16 Timer References Window Press the TMR REF Softkey to display the Timer References Window Turn the large FMS Knob to place the cursor in the Flight ID field Turn the small FMS Knob to enter the desired first character Turn the large FMS Knob to place the cursor in the next desired field Turn the small FMS Knob to enter the next desired character Repeat steps 4 and 5 until the desired Flight ID is entered Press the ENT Key updating is displayed as the Flight ID is loaded into the system Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 5 AUDIO PANEL SECTION 5 AUDIO PANEL oo il com r OM COMI Transmitters a e m Receiver Audio COM3 Disabled Passenger Address Disabled on 172R S Cabin Speaker Marker Beacon Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio Optional disabled if ADF and or DME are not installed Aircraft Navigation Radio Audio Disabled Manual Squelch eae Digital Clearance Recorder Play Key CREW w PILOT con i ICS Isolation ES ISOLATION PILOT QO PASS VOL SQ VOL Annunciation SQ Annunciation Reversionary Mode DISPLAY BACKUP Figure 5 1 Front Panel Controls 190 00384 08 Rev
186. rocedure 11111 9 1 Load and Activate An Arrival Procedure 9 1 9 2 Approaches 00 0 0 ccs 9 2 Load and or Activate an Approach Procedure 9 3 Activate An Approach in the Active Flight Plan 9 3 SECTION 10 HAZARD AVOIDANCE 0000 10 1 10 1 Customizing the Hazard Displays on the Navigation Map 0 0 ccccccesesesteeeesen 10 1 10 2 STORMSCOPE Optional 0 0 10 1 Displaying Stormscope Lightning Data on the Navigation Wap Padian 10 1 DLOMMSCO DG PAC Eii 10 2 10 3 XM Weather Service Optional 10 3 Displaying METAR and TAF information on the Airport Information Page 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 sssrin 10 5 Weather ProquctAge wx cssenacscocnenaresornumies 10 6 190 00384 08 Rev A 190 00384 08 Rev A 10 4 Traffic SysteM ou ccc cess eestesseesteaees 10 7 Traffic Information Service TIS 10 7 Traffic Advisory System TAS Optional cescees 10 8 ADS B Traic OpUoNal raisasi 10 9 10 5 Terrain and Obstacle Proximity 10 10 Displaying Terrain and Obstacles on the Terrain POX PAG aieia a A 10 10 Displaying Terrain and Obstacles on the Navigation al T TA AT E nA 10 11 10 6 Terrain Awareness amp Warning System TAWS Display Optional 0 00 000 000 10 11 Displaying
187. rol 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 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 DIS
188. rom the database those altitudes are displayed as white numerals This indicates the altitudes will not be used by the system for vertical guidance DIRECT T 9 until manually accepted by the pilot To accept the displayed altitude place the cursor over the then changes to light blue numerals indicating the altitude will now be used by the system for providing vertical guidance PSH eae altitude and press the ENT Key The altitude entry 15H LOCATION ERG 260 DIS 161NK OURS E 257 ACTIVATE Figure 7 28 Enter VNV Offset Distance Arr g Enter the offset or distance from the waypoint ee at which the selected altitude will be reached In y this case three miles prior to OPSHN is entered In other words the G1000 gives vertical guidance AENT VA PROFILE ee so the aircraft will arrive at an altitude of 10 000 vA a vs Tor feet three miles prior to OPSHN Te Tv ocu h Press the ENT Key twice to activate the direct to k iI Note in Figure 7 29 the magenta arrow in the Active Flight Plan Window indicating the direct to Figure 7 29 Direct to Active 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 PYNON 12 The aircraft is proceeding to OPSHN The expected approach is the RNAV LPV approach to runway 35R so it is selected procedure have no datab
189. ror 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 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 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III ER SECTION 12 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 7 transmitter is operating at reduced power If the problem persists the G1000 system A a should be serviced Reducing transmitter power C OM1 SERVICE
190. rse 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 Takeoff Modes Roll Mode Roll Hold default Heading Select HDG Key EE 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 GPS Arm Capture Track Approach VOR Arm Capture Track Approach ILS Arm Capture Track APR Key LOC Glideslope Mode automatically armed Go Around in air GA Switch Table 6 2 Roll Modes 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC FLIGHT CONTROL ROL ALTS Heading Select Mode HDG Figure 6 20 Roll Hold Mode Annunciation 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 Changing the Selected Headi
191. rsor Turn either FMS Knob to select the desired intersection Press the FMS Knob to remove the flashing cursor 190 00384 08 Rev A 7 11 NEAREST NDB 118 000 conz Select the Nearest NDB Page 1 2 Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to select the third rectangular page icon Access Information on a Specific NDB 1 2 3 190 00384 08 Rev A With the Nearest NDB Page displayed press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired NDB The remaining information on the Nearest NDB Page pertains to the selected NDB Press the FMS Knob to remove the flashing cursor 1 2 SECTION 7 NAVIGATION 7 12 NEAREST V OR IEAREST VOR 1 196 975 118 000 coe al Ty WORTH UP Ti NEAREST WOR TFR IL ai a WO DATA mepa Ta Figure 7 62 Nearest VOR Page Select the Nearest VOR Page Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to select the fourth rectangular page icon View Information on the Nearest VOR 1 2 3 With the Nearest VOR Page displayed press the VOR Softkey to place the cursor in the NEAREST VOR box Turn either FMS Knob to select a VOR 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 i
192. s Cockpit Reference Guide is Function Display MFD and the GMA 1347 Audio Panel to provide the pilot a resource with which to find System operating instructions on the major features of the G1000 system more easily It is not intended to be a A comprehensive operating guide Complete operating procedures for the complete system are found in the Garmin G1000 Pilots Guide for the Cessna Nav II 190 00498 03 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 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 1 1 SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS O 0 0O O ODO Of r PUSH VOL sQ lt gt COM ji EMERG PUSH 1 2 CRS 4 BARO PUSH PUSH HDG SYNC CRS CTR FD PUSH CRSR H MENU s PUSH CHSH GFC 700 AFCS Only Figure 1 1 PFD MFD Controls 1 2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 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 frequenci
193. s and allows the aircraft to be hand flown At the same time the flight director is synchronized to the aircraft attitude during the 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 _ ROL CHS P 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 08 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 a
194. s 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 OE Aas 136 975 118 000 corz TRIKE RATE a 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 tea aries we display STRIKE data CELL or STRIKE is display
195. se 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 Wwww garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause 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
196. service requires services CO DET FAIL The carbon Loss of communication monoxide detector is inopera between the G1000 and tive the CO Guardian Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 12 ANNUNCIATIONS amp ALERTS 12 4 AFCS ALERTS System Status Annunciation ws 113 00 118 98 1DD wr bis ore T 118 700 cos wwz 115 90 118 98 Tix 35 325 123 888 cog System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD Figure 12 5 AFCS System Status Annunciation Aileron Mistrim Right Roll servo providing sustained force in the indicated direction Aileron Mistrim Left Elevator Mistrim Down ore Elevator Mistrim Elevator Mistim Up Pitch Trim Failure PTRM If AP engaged take control of the aircraft and disengage AP Roll Failure ROLL Roll axis control failure AP inoperative Pitch Failure PTCH Pitch axis control failure AP inoperative System Failure lit egy 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 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 Pitch servo pr
197. shes for up to 10 seconds the autopilot transitions to Altitude Hold Mode and levels the aircraft Selected Altitude of 12 000 MSL ALT Mode Figure 6 31 Departure 190 00384 08 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 SLN 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 120007 2 Once the CDI shows less than one dot the flight director transitions from Heading Select to VOR Navigation Mode and the VOR annunciation flashes green The autopilot begins turning to intercep
198. sna Nav III 7 15 SECTION 7 NAVIGATION 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 38 Keep Vertical Align Actual Deviation Pointer Vertical Speed Centered with Required Vertical Speed Figure 7 38 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 39 Upon reaching the OPSHN offset waypoint three miles before OPSHN the aircraft will be at 10 000 feet 136 975 136 975 Figure 7 39 Approaching Bottom of Descent BOD at OPSHN 7 16 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 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 40 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 59 136 975 136 975 _ FPL ACTIVE FLIGHT PLAN nls i ACTIVE FLIGHT PLAN TFR KMKC KOOS SLANA THOOOFT SANK TOCOIFT JSHH TOCOOFT 113m 10000FT Approach KCOS RNAY 35 i HABUK iaf BT FALUR 251 CURRENT WH PROFILE TERRAIN gt 0 V DEV rT m 1000F1 EL by a pe a Se PEAR EN Figure 7 40 Turn to intercept OPSHN to FSHER Leg 190 00384 08 Rev A 19 Aft
199. spectively 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 08 Rev A A LLJ LLI 2 D2 2 Lu gt mn Z 59 ba JU nA ollow Block Peak Represents H es Sh gt gt L lt ee TH Ut L Tn ee gt A ee RS z LLI CE gt TE Eaa SERRE SERRATE i EEL ANNI MN MM MUNII MMM t e 7 MNM NNN MINNN MNN ANN MNN MANN MUNNI NNN MANI U E T H ma MN 5 FUEL amp TY GAL FUEL QTY GAL FUEL QTY T a4 A FUEL amp TY 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 08 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS Cruise Manifold Pressure JF 12345 6 12345 6 1455 1565 rr 4 8 B 428 4 5 6 C 464 C 435 Z j lt n 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
200. ss 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 MENU OPTIONS Concel Direct To NAV Cieor Vertical Constraints Press the FMS CRSR knob to return to bese poge Figure 7 6 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol DIRECT TO Identifier i a a a Facility Name AAIE VNAV Target Altitude Bearing to WPT Course to Selected WPT A FALT 3Q0FT BRG 129 Vinee Offset Distance DIS 1074NM ACTIVATE Figure 7 7 PFD Direct to Window Garmin G1000 Cockpit Reference Guide for the Cessna Nav III WPT Location Distance from WPT i 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 identifier 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 optio
201. ssure Model T182T only 190 00384 08 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS 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 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 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 Oil Temperature Indicator OIL TEMP Displays the engine oil temperature in degrees Fahrenheit F 6 Cylinder Head Temperature Indicator CHT Models 1821 T182T 206H T206H Shows the head temperature of the hottest cylinder number shown in triangular pointer in degrees Fahrenheit F C 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 C Vacuum Pressure Indicator VAC Models 172R and 172S Disp
202. st rectangular page icon Initially the closest airport to the aircraft s present position is displayed 190 00384 08 Rev A SECTION 7 NAVIGATION Access Information on a Specific Airport 1 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 2 Turn either FMS Knob to highlight the desired airport 3 Press the FMS Knob to remove the flashing Cursor Access Runway Information for the Selected Airport 1 With the Nearest Airports Page displayed press the RNWY Softkey to place the cursor in the RUNWAYS field 2 Turn the small FMS Knob to select the desired runway 3 Press the FMS Knob to remove the flashing Cursor Quickly Tune the COM Transceiver to a Nearby Airport Frequency 1 With the Nearest Airports Page displayed press the FREQ Softkey to place the cursor in the FREQUENCIES field 2 Turn either FMS Knob to select the desired frequency 3 Press the ENT Key The selected trequency is placed in the COM standby frequency field 4 Press the Frequency Transfer Key to place the frequency in the active field 5 Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 7 NAVIGATION Nearest Airports Information on the PFD Bearing TO Distance Airport Symbol NEAREST AIRPORTS US6 E ert 9
203. st 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 NORTH LP Chi y E 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 08 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 Figure 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 INFORHATION IDE
204. t 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 G1000 system MANIFEST GIA2 software should be serviced mismatch communication halted Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A A GIA mismatch has been detected where only one is WAAS capable SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories Cont COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP CON2 over temp 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 COM2 SERVICE COM2 needs may still be usable The G1000 system should be serviced when possible service Return unit for repair COM1 PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck COM1 RMT XFR COM1 remote transter key is stuck COM2 RMT XFR COM remote transter key is stuck LOI GPS integrity lost Crosscheck tates din ESR ONENA GPS integrity is insufficient for the curren
205. t phase of flight lk ba pap a OSs J T Loss of GPS navigation due to insufficient satellites navigation Insufficient satellites ie ae ne B el Loss of GPS navigation due to position error navigation Position error ae ma ee oS opis Loss of GPS navigation due to GPS failure navigation GPS fail The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced 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 ABORT APR Lose aka MavJetign Abort approach due to loss of GPS navigation Abort approach APR DUN GRADE APTON Vertical guidance generated by WAAS is unavailable use LNAV only minimums downgraded TRUE APR True north approach Displayed atter passing the first waypoint of a true north approach when the nav Change hdg reference to TRUE angle is set to AUTO 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 12 17 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories Cont GPS1
206. t the Selected Course 3 The autopilot continues the turn until the aircraft is established on the Selected Course Figure 6 32 Intercepting a VOR Radial Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Flying a Flight Plan GPS Course b Press the NAV Key to activate GPS Navigation Mode The autopilot guides the aircraft along A NOTE Changing the navigation source cancels the active tlight plan leg Navigation Mode and causes the flight director if the NAV Key is not pressed within 10 seconds to revert back to Roll Hold Mode wings rolled of VOR signal loss the flight director reverts to level Roll Hold Mode wings rolled level As the aircraft closes on Salina VOR GPS is used to SPS AP ALT 12000r7 navigate the next leg airway V244 The aircraft is cur rently tracking inbound on Airway V4 3 Following the flight plan the autopilot continues to steer the aircraft under GPS guidance Note that in GPS Navigation Mode course changes defined 1 Enter Salina VOR SLN into the GPS flight plan by the flight plan are automatically made without 2 Transition from VOR to GPS Navigation Mode pilot action required a Press the CDI Softkey until GPS is the selected navigation source Due to VOR signal loss VOR Navigation Mode is cancelled The VOR annunciation flashes yellow Flying a GPS flight plan Flashes up to 10 sec Transitions to Roll H
207. ted 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 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 F
208. th Tracking Mode e Navigation source manually changed from GPS e CNCL VNV Softkey selected on the Active Flight Plan Page MFD e All remaining vertical waypoints deleted trom the flight plan e Displays entering Reversionary Mode Non Path Descents Pitch Hold Vertical Speed and Flight Level Change modes can also be used to fly non path descents while 190 00384 08 Rev A 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 OE 20kr ALTS_VPTH Figure 6 13 Flight Level Change VNAV Non Path Descent To prevent immediate profile re capture the following must be satisfied 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 exclusive 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 A
209. 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 08 Rev A SECTION 7 NAVIGATION 3 Press the ENT Key to load the frequency into the e If the aircraft has entered an airspace Inside is COM frequency standby field displayed 4 Press the FMS Knob to remove the flashing View Additional Details for a Listed Airspace Cursor 1 With the Nearest Airspace Page displayed press 7 15 NEAREST AIRSPACES the FMS Knob to activate the cursor 2 Turn the large FMS Knob to scroll through the list highlighting the desired airspace 3 Press the ALERTS Softkey to place the cursor in the AIRSPACE ALERTS field 4 Turn either FMS Knob to select the desired airspace 5 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 Figure 7 65 Nearest Airspaces Page 2 Turn either FMS Knob to select the desired Select the Nearest Airspaces Page frequency 1 Turn the large FMS Knob to select the NRST page 3 Press the ENT Key to load the frequency into the group COM frequency standby field 2 Turn the small FMS Knob to select the seventh 4 Press the FMS Knob to remove the flashing rectangular page
210. the small FMS Knob to select pages within the only AIRWY HD group See Figure 1 7 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 Soitkey is displayed EXIT Press to exit the checklist EMERGCY Pressing this softkey displays the emergency checklist Nearest Group Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group Figure 1 7 Page Group Icon Selected Page 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 1 9 SECTION 1 SYSTEM OVERVIEW 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 g
211. 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 Cloud Top Echo Top e XM Lightning e Cell Movement SIGMETs AIRME Is e METARs e City Forecast e Surface Analysis Freezing Levels Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 10 HAZARD AVOIDANCE 10 6 e Winds Aloft e County Warnings e Cyclone Warnings Echo Top Cloud Top and Echo Top Mutually Exclusive Np te tt 5 NE Fa 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 flig
212. ther FMS Knob to highlight the desired transition waypoint and press the ENT Key Figure 9 4 Select Arrival Transition 8 A third window is displayed listing the available runways Turn either FMS Knob to select the desired runway and press the ENT Key IRMAT Figure 9 5 Select Arrival Runway 9 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 proper frequency and selecting that
213. tial Impact Point Projected Flight Path 4 Unlighted Obstacle 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 10 11 SECTION 10 HAZARD AVOIDANCE 17 95 HAP TAWS 124 000 118 000 cord i HOG UP 7 UP TERRAIN 1000F 1 100 Fft 118 000 conz TERRAIN 100e el 1000r1 M Figure 10 19 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 3 Press the ENT Key 10 12 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III PAGE MENU OPTIONS Inhibit TAWS View Arc Show Aviation Data Press the FMS CRSR knob to return to base page Figure 10 20 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
214. titude 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 glideslope 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 i 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 ne NITV Capture cepa APR Key Glideslope A 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 w
215. tivate 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 ACTIVATE S a Or 011m Figure 7 20 Comfirm Active Leg d Verify 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 08 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 ACTIVE FLIGHT PLAN R i NORTH UP ACTIVE FLIGHT PLAN KMKC KCOS V4 SLN iA V244 LAA H Airway V263 TBE TBE CURRENT VNV PROFILE ACTIVE UNV WPT _____FT at V5 TOT L FPH FPA G ee ds OT temari gt REO PH TIME TO TOO V DEV SS 5 1009r1 1000r1 7 10Gnn TONEL VNV Figure 7 21 V4 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 t
216. 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 the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use
217. 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 com1 135 675 35 VOLUM Figure 4 6 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 SECTION 4 NAV COM amp TRANSPONDER Squelch Indication 121 988 so 118 600 com sa 118 406 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 DME MODE WEVA 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 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 4 3 SECTION 4 NAV COM amp TRANSPONDER ADF Radio
218. ude 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 kt ALTS GP V 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 08 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 vertical deviation and vertical speed required appear on the PFDs in magenta Figure 6 11 Vertical Path Tracking Armed Flashing Indi Altitude Hold Mode Active cates Acknowledgment Required nav 108 08 117 95 136 975 118 000 con nav2 108 68 117 95 136 975 118 000 conz VNAV Target Altitude 7 Selected Altitude Below Z 6 pg VNAV larget Rma D Vertical Deviation oe Indicator Goot 2 ron Oa ae Required Vertical ae 1 Speed Bug Save F E arnn 2o 4921H Enroute Phase of Figure 6 11 Vertical Path Capture 190 00384 08 Rev A G
219. ulated when navigating a flight plan 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 08 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 G33 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 KMIA 86 4 MIAMI FL OFFSET SHH DIS 1H 4HH 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 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 Cancelling Direct to Navigation 1 Press the Direct to G8 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 08 Rev A SECTION 7 NAVIGATION 7 3 NAVIGATING AN EXAMPLE FLIGHT PLAN O NOTE The following example flight pl
220. ule backup memory has failed The G1000 system module is inoperative should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The PFD and or MFD voltage is low The G1000 system should be serviced p16 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A Database Message Advisories SECTION 12 ANNUNCIATIONS amp ALERTS 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 basemap 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 PFD1 DB ERR PFD1 terrain database missing MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 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 servic
221. ursor 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 flashing 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 08 Rev A 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1 2 3 4 5 8 190 00384 08 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 OD eT XD PUBLIC HEH CENTURY ATRCENTER OLATHE KS DEPARTURE CHIEFS Figure 9 1 Select Departure A list of runways may be displayed for the departure Turn either FMS Knob to select the desired runway and press the EN
222. vigation 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 ALT Figure 6 23 GPS Navigation Mode Armed GPS Navigation Se Altitude Hold Mode Active oe Mode Armed _ navi 115 58 113 00 133 558 120 059 con hav2108 00 gt 117 95 121 900 136 975 cond Command Bars Indicate Left Turn to Track GPS Course and Climb to Inter cept Selected Altitude GPS is Active Navigation Recetver on HSI 14108 14000 Selected Course Figure 6 22 Navigation Mode 190 00384 08 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Nav III SECTION 6 AUTOMATIC FLI
223. ware The 1 GEA 71 has incorrect sottware installed The G1000 system should be mismatch communication halted serviced 12 18 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS GTX 33 Message Advisories XPDR1 CONFIG XPDR1 config error The transponder configuration settings do not match those of backup Contig service req d configuration 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 ADR 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 GRS 77 Message Advisories AHRS1 TAS AHRS1 not receiving The 1 AHRS is not receiving true airspeed trom the air data computer The AHRS airspeed relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup The 1 AHRS is using the backup GPS path Primary GPS path has failed The GPS source G1000 system should be serviced when possible AHRS1 GPS AHRS1 not receiving The 1 AHRS is not receiving any or any useful GPS information Check AFMS any GPS information limitations The G1000 system should be serviced AHRS1 GPS AHRS1 not receiving The 1 A
224. will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course Figure 9 7 Selecting an Approach Transition 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 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 J3 SECTION 9 PROCEDURES Blank Page 9 4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190 00384 08 Rev A SECTION 10 HAZARD AVOIDANCE 10 1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 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 2 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 tra

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