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Garmin Software Version 0530.04 Cockpit Reference Guide

1. Figure 6 29 Flight Plan Overview 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 23 6 24 SECTION 6 AUTOMATIC FLIGHT CONTROL Departure Climbing to the Selected Altitude and flying an assigned heading 1 2 Before takeoff set the Selected Altitude to 12 000 feet using the ALT Knob In this example Vertical Soeed Mode is used to capture the Selected Altitude Pitch Hold Vertical Speed or Flight Level Change Mode may be used a Adjust the vertical speed to the desired value In this example 500 fom is used 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 and hand tlying the aircraft adjusting pitch angle to establish a new Vertical Speed Reference then releasing the CWS Button HD G Moy yo mo c Press the AP Key to engage the autopilot in a climb using Vertical Soeed Mode _ ROL AP ALTS 3 Use the HDG Knob to set the Selected Heading complying with ATC vectors to intercept Airway V4 Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading _ HDG AP TEE 4 As the aircraft
2. 100Ff1 1000F7 ZE O PuEE s 3ONH VIEW VNY PROF CNCL VNV VNV amp Figure 7 43 Approach Leg is Now Active To manually activate the approach procedure perform the following steps a Press the PROC Key b Turn the large FMS Knob to highlight ACTIVATE APPROACH as shown in Figure 7 44 PROCEDURES OPTIONS 2 or i Aer ERED Figure 7 45 Descending Turn to the Initial Approach Fix IAF ACTIVATE APPROACH SELECT APPROACH SELECT ARRIVAL SELECT DEPARTURE Figure 7 44 Activate Missed Approach c Press the ENT Key to activate the approach PAS Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 23 After crossing FALUR the next waypoint is the FAF The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator as shown in Figure 7 46 when the final approach course becomes active FPL ACTIVE FLIGHT PLAN 136 975 DOLOR DO SPRI iS NORTH UP ACTIVE FLIGHT PLAN KCO TFR KMKC KCOS NO DATA rp SOEs DTK E FSHER EDE hee PYNON ae a eee Approuch KCOS RNAV 3SRoes LPV HABUK iof wea hea ae FALUR e a a L CEGIX fof 351 5 5m RHSSR map 351 5 INH 6368FT 346 8 4NN MOGAL aahp HOLD CURRENT VNV PROFILE ACTIVE VNV WPT
3. gt SONH CNEL VNV Figure 7 24 V244 Now Active Leg 190 00567 01 Rev B SECTION 7 NAVIGATION 10 At Lamar VOR LAA V263 will be intercepted See oe eT Figure 7 25 PSN cA H NH gt NORTH UP ir fas V4 SLN E y VZ44LAA fis ULUS 322 o T EAREN Arrival KCOS TBEDBRY1 ALL TBE a7 n LOCATION CURRENT VNV PROFILE sane ERG 2B DIS 10114 ACTIVE UNV WPT at V5 TOT FPH FPA i Q FP OT TERRAIN VS REQ M TIME TO TOD T V DEV FT 100r i fenti Figure 7 26 Direct To OPSHN 30mnf CNL VNV Figure 7 25 HYS to LAA Leg Active ACTIVATE d Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7 27 11 ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure and E 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 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 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 7 11 SECTION 7 NAVIGATION 7 12 f Press the ENT Key The cursor is now displayed in the VNV offset fi
4. 4 Turn the small FMS Knob to display the Waypoint 6 Turn the small FMS Knob to display the Waypoint Information Window and begin entering the desired Information Window airways entry point WAYPOINT INFORHATION IDENT FACILITY CITY WAYPOINT INF ORHATION IDENT FACILITY CITY AnA Six yu NORTH UP NORTH UF LOCATION ee BRG LOCATION N CEN USA DIS ERG 063 N 39 DIS 39 0 ioga TIL Press ENT to occept Press ENT to occept Figure 8 16 Display Waypoint Information Window 7 Press the LD AIRWY Softkey A list of available 5 When the desired entry point is entered press the airways is now displayed ENT Key Figure 8 14 Load Airway Entry Point Figure 8 15 Airway Entry Point Loaded LOAD Figure 8 17 Select Desired Airway 8 Turn either FMS Knob to highlight the desired airway 9 Press the ENT Key A list of available exits is now displayed 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 g 5 SECTION 8 FLIGHT PLANNING 8 6 10 Turn either FMS Knob to highlight the desired exit point Figure 8 18 Select Desired Exit Point 11 With the desired exit point highlighted press the ENT Key 12 With LOAD highlighted press the ENT Key Figure 8 19 Airway Added to Flight Plan 8 9 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures 8 10 LOAD AN ARRIVAL See the
5. 1 8 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled displays altimeter in meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals STD BARO Press to set the barometric pressure to standard pressure BACK Press to return to the previous level softkeys ALERTS Press to display the Alerts Window OBS Press to select OBS Mode on the CDI when navigating by GPS only available with active leg CDI Press to change navigation mode on the CDI between GPS VORI and VOR2 XPDR Press to display the transponder mode selection softkeys STBY Press to select Standby Mode ON Press to select Mode A ALT Press to select Altitude Reporting Mode GND Press to select Ground Mode VFR Press to automatically squawk 1200 only in the U S A refer to ICAO standards for VFR codes in other countries SECTION 1 SYSTEM OVERVIEW CODE Press to display transponder code selection softkeys 0 7 0 through 7 Press numbers to enter code IDENT Press to provide special aircraft position identification to Air Traffic Control ATC BKSP Press to remove numbers entered one at a time BACK Press to return to the previous level softkeys IDENT Press to provide special aircraft position ide
6. acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration WARNING GDL 69 Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69 is approved only for weather avoidance not penetration WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B WARNINGS CAUTIONS amp NOTES WARNING The Garmin G1000 as installed in the Cessna 350 400 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 E WARNING For s
7. 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 GPS Navigation Section for details At the same time as 190 00567 01 Rev B 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 and the Vertical Track aural annunciation is issued 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 WNAV Target Altitude Capture to Altitude Hold Mode and tracks the level leg As Altitude Hold Mode becomes active the white ALT annunciation moves to the active pitch mode field and flashes green for ten seconds to indicate the automatic transition The flight director automatically arms Vertical Path Tracking
8. 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 the 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 35 Non path Descent 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 29 SECTION 6 AUTOMATIC FLIGHT CONTROL Approach KCOS Flying an ILS approach 1 Transition from GPS Navigation Mode to Heading Select Mode 8 a Select the Runway 35L ILS approach for KCOS and select VECTORS for the transition Load and activate the approach in the flight plan b Use the HDG Knob to set the Selected Heading after getting vectors from ATC c Press the HDG Key The autopilot turns the aircraft to the desired heading d Use Heading Sele
9. Figure 1 11 PFD Setup Menu Window Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1 8 DATABASE UPDATES The G1000 System uses Secure Digital SD cards to load and store various types of data For basic flight operations SD cards are required for database storage as well as Jeppesen aviation and ChartView database updates The following procedures pertain to updating the G1000 system with SD cards as outlined in Appendix B of the G1000 Cessna 350 400 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 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 12 Database Update Prompt 3 Press the ENT Key to start the database update A prompt similar to the following is displayed 190 00567 01 Rev B 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
10. Troffic device hos Foiled LOW FUEL R Low tuel in the right lt POR RILCL 10 50 33 aPOR IDENT TMR REF NRST ALERTS Q Q Bearing Information Windows C Selected Course Alerts Window Barometric Minimum Descent Altitude Annunciation Window 11 Vertical Deviation Glideslope Indicator 12 Marker Beacon Annunciation 13 AFCS Status Annunciation Figure 2 2 Additional PFD Information Distance to Next Waypoint Bearing to Next z Waypoint Figure 2 3 PFD Navigation Status Box 190 00567 01 Rev B 2 1 AIRSPEED INDICATOR Airspeed re _ Vspeed ee References Actual Airspeed Speed Ranges True Air speed Figure 2 4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer The pointer will become red upon reaching Vne At altitudes above 12 000 feet Vno and Vne will vary with altitude Refer to the Airplane Flight Manual AFM Figure 2 5 Red Pointer at V 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 At altitudes above 12 000 feet caution and excessive speed range markings will vary with altitude Refer to the Airplane Flight Manual AFM for airspeed limitations and indicator markings 190 00567 01 Rev B SECTION 2 FLIGHT INSTRUMENTS Airspeed Trend Vector The end of
11. Operations in the following discussions may also be performed with the corresponding controls on the MFD PFD Control Unit NAV COM Controls NAV Frequency Box COM Frequency Box Controls navi 108 00 117 95 i 136 975 118 000 com nav2 108 00 117 95 RE _ COH2 l 7 E 13000 CRS 4 BARO l PRRI 2800 CAS CTA g RANGE Hana ey 29 92 1 a a TRENAR INSET IDENT THR REF NRT Figure 4 1 G1000 VHF NAV COM Controls PFD 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 4 1 SECTION 4 NAV COM amp TRANSPONDER Standby NAV Selected NAV Selected COM Standby COM Frequency Field Frequency Frequency Frequency Field nav1 189 98 gt 110 60 Cv TSI 188 Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field an 135 100 0S0 cont 3 600 gt 121 900 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 350 400 190 00567 01 Rev B 4 1 RADIO STATUS INDICATIONS RX When a COM signal is received a white RX appears by the active COM frequency during si
12. See the Flight Planning section for a discussion on creating and modifying user defined waypoints 7 9 17 9 NEAREST AIRPORTS AnD rey Figure 7 60 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 first rectangular page icon Initially the closest airport to the aircraft s present position is displayed 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 190 00567 01 Rev B 2 3 SECTION 7 NAVIGATION Press the FMS Knob then turn the large FMS Knob to highlight the desired airport 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 EN
13. Turn the small FMS Knob to select Show or Hide disabled Aviation Data 3 p oT Inhibit TAWS t PMs i While the TAWS Page is displayed press the INHIBIT PAGE MENU Softkey TAWS INHB will be annunciated in the OPTIONS lower right of portion of the screen Inhibit TAWS T Enable TAWS iew Arc If TAWS has been inhibited from the TAWS Page press the INHIBIT Softkey The TAWS INHB annunciation will be removed Press the FMS CRSR knob to return to base page Figure 10 18 TAWS Page Menu 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 10 11 SECTION 10 HAZARD AVOIDANCE 10 12 Manual System Test A system test is automatically performed at power up After successful completion of the test TAWS System Test OR will be heard The system test may also be initiated manually but only when the aircraft is on the ground To manually verity proper operation of the aural and visual annunciations of the system perform the following steps 1 While the TAWS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS Page When all is in working order TAWS System Test OK will be heard Forward Looking Terrain Avoidance FLTA The Forward Looking Terrain Avoidance alert is composed of two sub functions Reduced Required Terr
14. a ee ae 20 20 pa bi av ral T FPL ACTIVE FLIGHT PLAN ronm ue f ACTIVE FLIGHT PLAN KMKC KOOS y W26S TBE E SEE i G Arrival KOOS TBE DBRY1 ALL OPSHH JMH fo SELENA TOCOOFT 25g JONH TOCHUFT ETY GSH TOCOUFT na Jz 11 51 ORT Approach KCOS RNAY 35RioGrs LPY HABUK inf rea SSN S000 FALUR 261 SONH 8600 CURRENT WHY PROFILE ACTIVE Ve WPT V5 TGT aN 9 Y DEI 10 FT 136 975 136 975 d y k a i T 7 _ A y N i t Nt A a R Vee N f 7 Bons p g f e we aS ze p d ri 4 Pm 1 FA ON a aN Z Figure 7 40 Turn to intercept OPSHN to FSHER Leg 190 00567 01 Rev B 19 After passing OPSHN the next leg of the arrival will turn 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 a NORTH UP ACTIVE FLIGHT PLAN d TFR KMEC KDOS HI DATA Airwoy W263 TBE TEE Arrival RCOS TBE DBAY 1 ALL delala KPUB Pur OPSHN SnH Pu ae OPSHN erences i FSHER 352 1000061 PYNOH 352 1154H RGGFT Approoch KCOS RNAV 35Riers LPW HABUK iaf w1 SIN SQ00F1 FALUR 251 S NA B600 CEGIX fof 351 B NH CURRENT VN PROFILE ACTIVE UNU WET VS TGT TERRAIN VS REG FPH TIRE TO BOO 10FT rt M u SOnn CHEL YNY Figure 7 41 Tracking the OPSHN to FSHER Leg 20 The f
15. 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 190 00567 01 Rev B 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 Longitudinal and lateral components Option 1 Total wind direction and speed Option 2 Total direction with head and crosswind speed components Option 3 Option 1 Option 2 cc No Data NO WIND DATA Option 3 Figure 2 30 Wind Data Window Displaying wind data 1 2 3 4 190 00567 01 Rev B Press the PFD Softkey Press the WIND Softkey to display wind data below the Selected Heading Press one of the OPTN softkeys to change how wind data is displayed To remove the Wind Data Window press the OFF Softkey SECTION 2 FLIGHT INSTRUMENTS 2 10 GENERIC TIMER REFERENCES TIMER 01 20 10 UP REFERENCES TIMER 00 25 05 DN REFERENCES TIMER 00 25 13 UP STOP RESET Figure 2 31 Timer Status Prompts Change the Generic Timer 1 2 3 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
16. 13 6 18 6 20 6 21 Cyclones 10 5 D Databases 1 14 Dead Reckoning 2 12 11 2 Departures 9 1 Direct to 7 1 7 5 7 11 7 12 8 8 DR 2 12 DR mode 11 2 11 3 Dual CDU failure 11 2 E ECHO TOPS 10 4 Edit a flight plan 8 6 EDR 10 13 Endurance 3 6 Excessive Descent Rate 10 13 F FD 1 4 1 6 FLC 1 4 Flight director 6 1 6 1 6 2 Pitch modes 6 3 6 9 Roll modes 6 16 6 19 Flight level change 1 4 Flight Level Change Mode 6 27 6 29 Flight Level Change Mode FLC 6 8 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Index 1 INDEX Index 2 Flight Plan Catalog 9 1 9 2 FLTA 10 12 Forward Looking Terrain Avoidance 10 12 Freezing level 10 5 Frequency toggle key 1 3 4 3 Fuel remaining 3 6 Fuel used 3 6 G GA 6 1 Glidepath 2 6 7 19 Glidepath Mode 6 14 6 20 Glidepath Mode GP 6 31 Glideslope 2 6 2 7 7 19 Glideslope Indicator 2 2 Glideslope Mode 6 15 6 20 6 30 GMA 1347 1 1 Go Around 6 1 Go Around Mode 6 32 6 33 Go Around Mode GA 6 16 Heading 2 1 Heading indication 2 10 Heading Select 1 3 1 4 Heading Select Mode 6 18 Heading Select Mode HDG 6 24 Headset s 5 3 Horizontal situation indicator 2 9 Horizontal Situation Indicator HSI 2 1 Hurricanes 10 5 ID 1 3 4 3 ILS approach 6 30 Imminent Terrain Impact 10 12 Impact point 10 12 Inhibit 10 11 Inset Map PFD 2 2 Interrogations 4 4 IOI 10 12 10 15 12 6 ITI 10 12 Garmin G1000 Cockpit Refe
17. 400 Figure 3 1 Engine Instrument Display 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 3 1 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 EIS DISPLAY Selecting the SYSTEM Softkey on the MFD acesses the Engine Indication System EIS Display For all instruments green indicates the acceptable operating range yellow and red indicate caution and warning respectively Oxygen System Optional Selecting the OXYGEN Softkey on the MFD turns the oxygen system on or off If no oxygen system is installed the oxygen gauges will be blank Oxygen Quantity OXY QTY PSI Amount of remaining oxygen in terms of pressure Oxygen Outlet Pressure OXY OUTLET PSI Oxygen outlet pressure in pounds per square inch psi Oil Oil Manifold Temperature Pressure Pressure auge Gauge Gauge Trim Correct takeoff aileron and elevator trim positions are indicated by the green boxes Carbon Monoxide Detection If carbon monoxide in the cabin becomes too high above 50 ppm a flashing annunciation will be displayed in the lower left of the EIS System Display as shown in Figure 3 2 The current amount of CO is displayed in parts per million A warning annunciation will also be displayed on the PFD in the Annunciations Window and an aural warning will be generated Oxygen Quantity Tachometer Gauge gt 5 aoa JS 20 C Pal oxy QTY 203 43 3 1600 gi E Fuel Flow __ GAL REM ENDUR _ Oxy
18. 5 Traffic advisory 10 7 10 8 10 9 10 14 Traffic Annunciation 2 2 Traffic map page 10 7 10 8 10 9 10 14 Transponder 4 4 Transponder standby mode 4 4 Transponder Status bar 4 5 Transponder Status Box 2 1 Trim 3 2 6 1 Trim Manual Electric 6 21 Tropical storms 10 5 True airspeed 2 1 Turn Rate Indicator 2 1 TX 4 3 U Unlighted obstacle 10 14 V VDI 7 15 7 16 Vertical Descent Indicator 7 15 INDEX Vertical Deviation 2 6 Vertical deviation guidance 1 12 1 13 Vertical Deviation Indicator 2 2 Vertical navigation 1 12 1 13 Vertical Navigation flight control 6 10 6 14 Vertical Path Tracking Mode 6 10 6 11 6 28 Vertical speed 1 4 2 7 Vertical speed guidance 1 12 1 13 Vertical Speed Indicator VSI 2 1 Vertical Soeed Mode 6 7 Vertical Speed Reference 6 7 VHF 4 1 VNAV 1 13 12 22 VNAV Target Altitude 6 10 6 13 VNAV Target Altitude Capture Mode 6 13 VNV 1 12 1 13 7 1 7 4 7 15 VNV Target Altitude 2 6 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Volume squelch 5 4 VS 1 4 VSI 7 16 Vspeeds 2 3 W WAAS 2 6 6 23 7 5 12 16 WAAS precision approach 6 31 WARN 2 12 Warning 12 1 12 2 Weather data link page 10 4 Weather product symbol 10 5 Weather product symbols 10 6 Weather warnings 10 5 Wind direction 10 5 Wind speed 10 5 Wings level 6 16 6 17 X XM weather 10 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Index 3 INDEX Blank Page Ind
19. ALERTS GIA 63 Message Advisories Cont Message Comments o COM1 SERVICE COM1 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may COM2 SERVICE COM needs still be usable The G1000 system should be serviced when possible service Return unit for repair COM1 PTT COMI push to talk key is stuck COM2 PTT COM2 push to talk key is stuck COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck 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 posi tion Press the transter switch again to cycle its operation If the problem persists the G1000 system should be serviced 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 si eae psa J n g Loss of GPS navigation due to insufficient satellites tion Insufficient satellites ah NAY a 7 DL Loss of GPS navigation due to position error navigation Position error Loss of GPS integrity monitoring GPS NAV LOST Los
20. AP VPTH 2 When the top of descent TOD is reached the flight 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 This altitude was entered director transitions to Vertical Path Tracking Mode and begins the descent to the VNV Target Altitude Intention to capture the VNV Target Altitude is in the flight plan as a component of an offset waypoint from OPSHN intersection as indicated in the example flight plan in Section 7 GPS EEE ALTV Navigation indicated by the white ALTV annunciation 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 If the Selected Altitude is not adequately adjusted below the VNV Target Altitude the flight director will command descent to the Selected Altitude rather than the VNV Target Altitude once Vertical Path Tracking Mode becomes active ALTS willbe GSS Sa ALT 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 trom Altitude Hold to Vertical Path Tracking Mode To proceed with descent path capture if the white VPTH annunciation begins GPS AL flashing do one of the following The green ALT annunciation flashes f
21. Alert Pop Up Press the ENT Key to display the TAWS Page or press the CLR Key to remain on the Navigation Map Page Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed select the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map 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 23 TAWS Symbols 10 14 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 UF ame Pull Up Reduced Required Terrain Clearance Warn PULL UP Terrain Terrain Pull Up Pull Up ing RTC or or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact Warning ITI PULL UP Terrain Ahead Pull Up Terrain Ahead Pull Up or or TERRAIN PULL UP Terrain Terrain Pull Up Pull Up Reduced Required Obstacle Clearance PULL UP Obstacle Obstacle Pull Up Pull Up Warning ROC or or Obstacle Ahead Pul
22. At the TOD establish automatically become active The approach may a descent vertical speed as previously discussed in be activated at any point to proceed directly to the Step 16 The aircraft altitude will be 9 000 feet IAF In this example the aircraft has progressed upon reaching HABUK through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF we oo 1 E 5368FT ED TIV FL iT AN as the active leg activating the approach procedure srn ATER a R KKC Koos see Figure 7 43 FPL ACTIVE FLIGHT PLAN 136 975 _NORTH UP OPSHN 3n PIO en el OPSHN FSHER ACTIVE FLIGHT PLAN SHER _ _ _ TFR KMKC KCOS NO DATA WE DTK DIS OPSHN 3M sae SET BAAN PYNON Daaa tread ere KCOS RNAV 35Roes LPV HABUK lof 251 1 7N FALUR 261 E NH CEGIX fof 351 6 21Nn OPSHN SE ee A FSHER binan RSS PYNON a WH E FT Approoch KOOS RNAV 35RGPs LPV gt HABUK iof 021 5 2NM 93000 FALUR 251 5 0NH A CEGIX fof 351 6 0m RH SR map 351 5 1Nn RHSSR map 351 5 1NM 6368FT 348 8 4NM MOGAL aahp CURRENT VNV PROFILE ACTIVE UNV WPT S OGeT at HABUK laf VS TGT 7S5FPH FPA VS REO __ _ _FPH TIME TO BOD 6368FT 348 O 4NN TERRAIN v Dev SOFT MOGAL f MUGAL mahp 100Ff1 1000Ff7 CURRENT VNV PROFILE ACTIVE UNV WPT 90OOFT at HABUK iaf sj JONN VS TGT 796FPH FPA VIEH NY PROF CNCL VNV VNY amp raain VS REO 627FPH TIME TO TOD f Vv DEV 290FT
23. B TABLE OF CONTENTS 10 6 Terrain And Obstacle Proximity 0 10 9 12 6 G1000 System Annunciations 0 0008 12 7 Displaying Terrain and Obstacles on the Terrain 12 7 G1000 System Message Advisories 12 9 PROMIIMILVP AGG as ca euscnenseadenrastnheneseudsarachasentasianseunsians 10 9 MFD amp PFD Message AdVISOTICS ccscessecseseeseeren 12 10 Displaying Terrain and Obstacles on the Navigation Database Message AdVISOFES ccsseseseeseeresren 12 11 IN cst stave tae E E E as eat E A eden 10 9 GMA 1347 Message Advisories s s s 12 12 10 7 Terrain Awareness amp Warning System GIA 63 Message Advisories scesecseesecssesteeseeseen 12 13 TAWS Display Optional 0 0 0 000 10 10 GIA 63W Message Advisories 12 16 Displaying Terrain on the TAWS Page sesseees 10 10 GEA 71 Message Advisories scescesceseeseesteeseeseen 12 18 Enable Disable Aviation Data cscseseseereesen 10 11 GTX 33 Message Advisories 12 19 TANS OUD Eroen arona 10 11 GRS 77 Message AVISOLGS scesscescesecssesteeseeseen 12 19 Manual System Test scssceseseseesessessessereessen 10 12 GMU 44 Message Advisories scessseseseesessesseeen 12 20 Forward Looking Terrain Avoidance FLTA 10 12 GDL 69A Message Advisories s s 12 20 Premature Descent Alert PDA cnn 10 12 GDC 74A Message Advisories 12 20 Excessive Descent Rate Alert EDR a an 10 13 GCU 476 Message A
24. HABLUE iof B21 S SNH 30001 FALUR 251 S NA 86001 Aporooch KOOS RHAV 35Rors LPY CURRENT VNV PROFILE ACTIVE We WET TOOOGFT at OPSHN Jhr VS TGT S5FPH FPA VS REG Terman gt PE Y 100Fr gl 1000F eee 30nn FPL z VIER YAW PROF CHOL YNV VA SH CHAT 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Altitude constraint values associated with the Final Approach Fix FAF and waypoints beyond the FAF cannot be designated for vertical guidance These altitude values will always be displayed as white text as in Figure 7 34 Vertical guidance to the FAF and on to the Missed Approach Point MAP is given using the WAAS GPS altitude source therefore the displayed altitude values are for reference only r
25. Hold Mode when the altitude error is less than 50 ft In this case the Selected Altitude becomes the flight director s Altitude Reference Changing the Altitude Reference NOTE Turning the ALT Knob while in Altitude Hold Mode changes the Selected Altitude but not the flight director s Altitude Reference and does not cancel the mode With the CWS Button depressed the aircraft can be hand flown to a new Altitude Reference When the CWS Button is released at the desired altitude the new altitude is established as the Altitude Reference 190 00567 01 Rev B 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 Mode Active Altitude Reference nav1 188 88 gt 117 95 B KICI ors IP Bnn ens 227 118 000 con Selected Altitude Selected Altitude Bug Command Bars Hola Pitch Attitude to Maintain Altitude Reference TAS 120KT OAT 77 FISA 21 F Figure 6 7 Altitude Hold Mode Vertical Speed Mode VS 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 V
26. Procedures section for a discussion on loading and activating arrival procedures Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 11 LOAD AN APPROACH 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 procedures waypoints 3 Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure or airway 8 13 STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan Figure 8 20 Store Flight Plan Confirmation 8 14 EDIT A STORED FLIGHT PLAN 1 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired 190 00567 01 Rev B flight plan and press the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired locations fo
27. RVSI Upon Reaching Top of Descent TOD 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 BRG 258 136 9750 136 975 k ao ie as i AAR VE 12000 ots ion E lj Ji 1 f o_o 4 _ Ae dea S Keep Vertical Deviation Pointer Align Actual Centered _ Vertical Speed 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 will be 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 136 975 186 975 i L Figure 7 39 Approaching Bottom of Descent BOD at OPSHN 7 16 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 18 The aircraft is approaching OPSHN The upcoming turn and next heading will be annunciated at the top lett 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 tor the OPSHN to FSHER leg and center the CDI 117 95 Turn right to 352 in 10 seconds pice 259 136 975 7 95 P8697 S F s T VL te 7o rs Rae A n D T
28. SECTION 4 NAV COM AND TRANSPONDER 4 1 4 1 Radio Status Indications 0 ccccceeen 4 3 BD MOWING reconnues anan 4 3 4 3 Automatic Squelch sce 4 3 4 4 Quickly Activating 121 500 MHZ 4 3 4 5 Frequency Auto tuning 0 0 cccccce een 4 3 Autotuning onthe PED sas erascsacasseadereminostiakernts 4 3 Auto tuning on the MFD nsss 4 3 4 6 Transponder 4 4 Mode selectiON siisii 4 4 REDIW StAtUs soiusno nii E E 4 4 Code selecto asasen 4 5 SECTION 5 AUDIO PANEL 000 5 1 5 1 COM Radio Selection 5 2 5 2 Split COM Function usec 5 2 5 3 Marker Beacon Receivel ccccesesesees 5 2 5 4 Nav Radio Audio Selection cccceee 5 3 5 5 Intercom System ICS Isolation 5 3 5 6 Intercom Squelch Control 0 c ccces 5 4 5 7 Digital Clearance Recorder and Player 5 4 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 1 6 1 ARCS Control Sociorum 6 1 6 2 Flight Director Operation 5 515551111111111 6 1 Activating the Flight Director 6 1 COMMING BANS srera a 6 2 AFC STATUS DOK aa S 6 2 6 3 Flight Director Modes 0 0 cccccceeeen 6 3 PRA MOES raer a S 6 3 ROI MOGES oisinnean stnaiamnsstsntnestiaaancboastessteaisad 6 16 6 4 Autopilot Operation ue 6 21 EMGaCING TC AUTON Obes seccsreccettredaaeninerestiaieieeate 6 21 Control Wheel Ste rind ccssccsscesssessessessessesseesneesees 6 21 Di
29. 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 PIT Selected Altitude Capture ALTS Altitude Hold ALT Key ALT nnnnn FT Vertical Speed VS Key VS nnnn FPM 2000 to 1500 fpm 100 tom Flight Level Change IAS 80 to 200 kt C350 FLC K FL 1k Hold CRY PAG MAK I 80 to 210 kt C400 Vertical Path Tracking WAAS systems only ene a VNAV Target Altitude NTV Capture Glidepath WAAS onl GP WAAS onl a y APR Key y Glideslope GS Go Around in air GA Switch ALTS is armed automatically when PIT VS FLC or GA is active and under VPTH when the Selected Altitude is to be captured instead of the VNAV Target Altitude ALTV is armed automatically under VPTH when the VNAV Target Altitude is to be captured instead of the Selected Altitude Table 6 1 Flight Director Pitch Modes 6 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL Pitch Hold Mode PIT Changing the Pitch Reference When the fli
30. 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 2 FLIGHT INSTRUMENTS Blank Page Jd Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B INDICATION SYSTEM EIS SECTION 3 ENGINE INDICATION SYSTEM EIS The Engine Instrument Display is displayed on the lett side of the MFD Manifold Pressure Gauge s Tachometer Indicates Selected Fuel Indicates FUEL QTY GAL Tank STER ac Selected Fuel an Tank Sep 5 Fuel Quantity se H 16 76 30 46 F In icator E 16 76 30 46 F FFLOW GPH 15 0 FFLOW GPH 15 0 ne ee _ Fuel Flow _ i ene i Indicator ae OIL PSI 21 a OIL PSI 51 z ee Indicator Oil Tempera Ei 189 ELEV OIL F 188 ture Indicator SE 2a TRIM Elevator Trim 46 Slide Bar TIT F Exhaust Gas 5 Turbine Inlet Mik 1436 Temperature Temperature Cylinder Head 392 Indicator Temperature Indicator CHT F 392 RA tl i AILERON TRIM AILERON TRIM bA Aileron Trim Slide Bar Cessna 350 Cessna
31. V4 will now be made the active leg of the flight plan a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight SLN The TO waypoint of the leg is selected in order to activate the leg c Press the ACT LEG Softkey The confirmation window is now displayed as in Figure 7 20 Note the TOP to SLN leg is actually part of V4 TOP gt SLN ACTIVATE ummm Or 01m Figure 7 20 Confirm Active Leg d Verity the displayed leg is the desired leg and press the ENT Key Note in Figure 7 21 the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg Note also the crosstrack XTK distance on the HSI indicating 16 9 nm to the intercept point Note the phase of flight 6 SECTION 7 NAVIGATION 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 PL ACTIVE FLIGHT PLAN NORTH UP ACTIVE FLIGHT PLAN V4 SLN V244 LAA LAR Airway V263 TBE TBE CURRENT VNV PROFILE ACTIVE UNV WPT SN 9 A ero V5 TOT FPH FPA s tae o TERRAIN VS REQ FPH TIME T i v DEV aan F T 1001 i 1000r1 m 10Gnn CNCL VNV Figure 7 21 V4 Now Active Leg The aircraft continues on heading 290 When 2 0 nm trom the intercept the XTK will disappear t
32. 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 00567 01 Rev B SECTION 8 FLIGHT PLANNING Repeat steps 2 and 3 until the desired name is entered 5 Press the ENT Key 6 The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be moditied by changing the reference waypoint Turn the FMS Knobs to enter the position coordinates or the radial and distance trom the reference waypoint 7 Press the FMS Knob to remove the flashing cursor Modify a User Waypoint 1 With the User Waypoint Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to move the cursor to the desired field and turn the small FMS Knob to make changes 3 Press the ENT Key to accept the changes 4 Press the FMS Knob to remove the flashing cursor Delete a User Waypoint 1 Select the User Waypoint Information Page and press the DELETE Softkey 2 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key Create User Waypoints from the Navigation Map Page 1 With the Navigation Map Page displayed push the Joystick to activate the pann
33. airspeed input from air data computer Display is not receiving altitude input from the air data computer Display is not receiving vertical speed input from the air data computer GPS information is either not present or is invalid for navigation use Note that AHRS utilizes GPS inputs during normal operation AHRS operation may be degraded if GPS signals are not present see AFM A red X through any other display field such as engine instrumentation fields indicates that the field is not receiving valid data Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 Integrated Avionics Units GIA 63 Integrated Avionics Units GDC 4A Air Data Computer mar ey af W A A ATTITUDE SI EL M N a EN GRS 77 AHRS GEA 71 Engine ll P Or Airframe Unit 91 GMU 44 Or FFLOW GPH a Magnetometer GIA 63 Integrated 48 Avionics Unit OIL PSI INTEG GIA 63 Integrated TS OR URES Avionics Units ALT AMPS AILERON TRIM a j jait _ s _ L POROS a re a a ENGINE CDI OBS XPDR IDENT TMREREF NAST ALERTS GDC 74A Air Data GTX 33 Transponder Or ae o GIA 63 Integrated Figure 12 6 G1000 System Failure Annunciations Avionics Units 12 7 G1000 SYSTEM MESSAGE A NOTE This sect
34. alert Minimums Minimums is generated 2 8 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 2 8 190 00567 01 Rev B HORIZONTAL SITUATION INDICATOR HSI C1 Turn Rate Indicator Lateral Deviation Scale G Navigation Source 4 Aircraft Symbol Course Deviation Indicator Rotating Compass Rose OBS Mode TO FROM Indicator Heading Bug Course Pointer Flight Phase Turn Rate and Heading Trend Vector Heading 14 Lubber Line QOOOOOQOOOOO Figure 2 18 Horizontal Situation Indicator 360 SECTION 2 FLIGHT INSTRUMENTS Arc HSI A NOTE When the Arc HSI is displayed the BRG1 and BRG2 Information Windows and pointers are disabled A NOTE If the pilot makes a heading change greater than 105 with respect to the course the CDI switches to the opposite side of the deviation scale and displays reverse sensing The Arc HSI is a 140 expanded section of the compass rose The Arc contains a Course Pointer arrow the TO FROM indicator a sliding deviation indicator the TO FROM and sliding deviation indicators are one and the same and a deviation scale Upon station passage the TO FROM indicator flips and points to the tail of the aircraft just like the conventional TO FROM flag Depending on the navigation source the CDI on the Arc HSI can appear in two different ways GPS OBS VOR Arrowhead e Localizer Diamond Lateral Course Deviation and Deviation T
35. an LRU function fails a large red certain windows remain invalid as G1000 X is typically displayed on windows associated with the equipment begins to initialize All windows failed data The following section describes various system should be operational within one minute of annunciations Refer to the AFM for additional information power up Should any window continue to remain flagged the G1000 system should be regarding pilot responses to these annunciations l l hop nee 6 6 P P serviced by a Garmin authorized repair facility system Annundaion Commet Attitude and Heading Reference System is aligning Display system is not receiving attitude information from the AHRS mE Display is not receiving valid heading input from AHRS Display is not receiving valid transponder information 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 127 SECTION 12 ANNUNCIATIONS 12 8 amp ALERTS System Annunciation Commet eet a r Other Various Red X Indications Indicates a configuration module failure This annunciation will only be 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 will soon appear over the Attitude Indicator Display system is not receiving
36. 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 nav 111 90 114 18 Suc nava 113 88 110 Autopilot Disconnect Se Annunciation Flashes Yellow 5 sec Command Bars Indicate Climb 108 Of H rir TAS 110KT OAT TT FIISA 21F 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 Navigation GPS VOR LOC Captures and tracks the selected navigation source Approach GPS VAPP LOC BC Captures and tracks the selected navigation source with greater sensitivity for approach Go Around Commands a constant pitch angle and wings level while in the air 118 000 con g COM F aan G 3000 A C908 280g Figure 6 19 Go Around Mode 6 16 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL Table 6 2 relates each roll mode to its respective control RM ALTS and annunciation Refer to the pitch modes section for Figure 6 20 Roll Hold Mode Annunciation information regarding Go Around Mode The CWS Button does not change lateral references Bank Angle Flight Director Response for Heading Select Na
37. brakes are active Message Advisory Alerts Cessna 400 only 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 service requires services CO DET FAIL The carbon Loss of communication monoxide detector is inopera between the G1000 and tive the CO Guardian 12 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 12 ANNUNCIATIONS amp ALERTS 12 4 AFCS ALERTS System Status Annunciation wv 113 00 110 90 IDD uir DIS ote Th 118 700 con TT 118 98 ttm 35 325 T System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD Figure 12 5 AFCS System Status Annunciation Alert Condition Aileron Mistrim Right Roll servo providing sustained force in the indicated direction Aileron Mistrim Left Elevator Mistrim Down Pitch servo providing sustained force in the indicated direction Elevator Mistrim Up Pitch Trim Failure PTRM lf AP engaged take control of the aircraft and disengage AP _ om stuck MEPT Switch Do io disengaged move MEPT switches separately to unstick RollFailure Failure k Row 9 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 Fai
38. changes that relate to particular pages PROC Key Gives access to IFR departure procedures DPs arrival procedures STARs and approach procedures IAPs for a flight plan If a flight plan is used available procedures for the departure and or arrival airport are automatically suggested and can be loaded into the active flight plan If a flight plan is not used both the desired airport and the desired procedure may be selected G Joystick Changes the map range distance top to bottom of map display when rotated activates the map pointer when pressed Alphanumeric Keys Allow data entry without using the GDU FMS Knob to select individual characters BKSP Key Moves the cursor back one character space SPC Key Adds a space 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 1 SYSTEM OVERVIEW ENT Key Validates or confirms a menu selection or data entry CLR Key Erases information cancels entries or removes page menus Press and hold to immediately display the Navigation Map Page 11 SEL Key The center of this key activates the selected softkey while the right and left arrows move the softkey selection box light blue box around the softkey label to the right and left respectively 12 Decimal Key Enters a decimal point 13 Plus Minus Key Switches entry between the and characters NAV Key Selects NAV Radio Con
39. in vertical guidance calculations Waypoint altitude constraints may be designated up to but not including the FAF The FAF will always be 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 Altitudes that have been designated for use in vertical guidance may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude To help interpret the meanings of how the altitudes are presented keep the following points in mind e When the altitude is displayed in light blue the system is using that altitude designated to determine vertical speed and deviation guidance e When the altitude is displayed in white it is not being used by the system non designated to determine the vertical speed and deviation guidance e 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 00567 01 Rev B 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 canno
40. is populated only when navigating a flight plan 190 00567 01 Rev B 3 4 5 6 DIRECT TO m IDENT FACILITY CITY 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 J Key followed by pressing the ENT Key twice If a missed approach point MAP is the current destination the approach will be canceled Manually Define the Active Direct to 1 2 3 4 5 6 1 8 190 00567 01 Rev B Press the Direct to 39 Key Turn the large FMS Knob to highlight the VNV 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 VNV offset field Enter the desired the 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 d
41. lower right of the MFD a ee dis pl ay Bearing BRG 129 ns 1085H Distance 2 Turn the small FMS Knob to select the first MAP as Sus ma Activate Field page indicated by a solid rectangular icon 136 975 115 000 oog Figure 7 2 MFD Direct to Window Bi Enter a Direct to Destination 1 Press the Direct to 8 Key 2 Enter the destination waypoint identifier 3 Press the ENT Key to confirm 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 contraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV 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 Figure 7 1 Navigation Map Page Enroute 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 again to activate the Direct to Select a Direc
42. 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 aw 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 und as an aid to situational awareness to continue Press ENT or rightmost softkey E Figure 1 14 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 select the MAP Softkey and check to make sure that the TOPO and TERRAIN Softkeys are available not dimmed and other database features are functioning Power down the G1000 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 1 SYSTEM OVERVIEW Blank Page 1 16 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display unless otherwise background shown in the following illustrations is used in WAAS capable systems A solid blue and brown background will be seen in non WAAS systems aD w W w D
43. on the Nearest VOR 1 With the Nearest VOR Page displayed press the VOR Softkey to place the cursor in the NEAREST VOR box 2 Turn either FMS Knob to select a VOR 3 Press the FMS Knob to remove the flashing cursor Select and Load a VOR Frequency 1 With the Nearest VOR Page displayed press the FREQ Softkey to highlight the VOR frequency in the FREQUENCY field 2 Press the ENT Key The selected VOR frequency is placed in the NAV standby frequency field Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 7 27 SECTION 7 NAVIGATION 3 Press the FMS Knob to remove the flashing cursor 7 13 NEAREST USER WAYPOINT INFORMATION QJ41 16 REFERENCE WAYPOINTS Figure 7 65 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fifth rectangular page icon Select a Nearest User Waypoint 1 2 1 28 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 these will be displayed with the closest listed first Turn either FMS Knob to select the desired waypoint The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 3 Press the FMS Knob to remove
44. plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint Press the ACT LEG Softkey using MFD only Or Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This 190 00567 01 Rev B 3 8 5 1 2 3 8 6 1 190 00567 01 Rev B step must be used when activating a leg trom the PFD With Activate highlighted press the ENT Key KOJE KSLN ACTIVATE or CANCEL Figure 8 5 Activate Flight Plan Leg Confirmation STOP NAVIGATING A FLIGHT PLAN Press the FPL Key to display the Active Flight Plan Page Press the MENU Key to display the Page Menu window Press the FMS CRSA knob to return to bese poge Figure 8 6 Delete Flight Plan Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan Figure 8 7 Delete Flight Plan Confirmation INVERT ACTIVE FLIGHT PLAN From the Active Flight Plan Page press the MENU Key to display the Page Menu 2 3 8 7 SECTION 8 FLIGHT PLANNING Turn the large FMS Knob to highlight Invert Flight Plan and press t
45. 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 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 change the page mode press the AUTO or MANUAL Softkey Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Starting WPT Ending WPT AGY WODE AUTOMATIC FPL 01 G CUH CALIBRATED AS KHCT kS IND ALTITUDE PRESSURE t DEP TIME TOTAL AIR TEHP 6S UNITED STATES OF AMERIC rye riow 4 ew Cia _500nn FUEL ONBOARD TRIP STATS FUEL STATS EFFICIENCY TOTAL EDUR REH FUEL REH ENDUR soot FT FUEL REG TOTAL RANGE 1 OTHER STATS DENSITY ALT _W _ F TRUE AIRSPEED WIND DIRECTION WIND SPEED HEAD WIND MANUAL FF HPT Figure 8 22 Trip Planning Page For Direct to planning press the WPTS Softkey and verify 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 For point to point planning turn the FMS
46. receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for The system notifies the pilot to set the CDI to the correct NAV receiver Set the approach CDI to the correct NAV receiver PTK FAIL Parallel track unavailable Bad parallel track geometry bad geometry PTK FAIL Parallel track unavailable on Invalid leg type for parallel offset invalid leg type a iy alg EGR OR Nie waypoint for parallel offset has been passed 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 will automatically transition to the next vertical waypoint VNV Unavailable Unsupported leg The lateral flight plan contains a procedure turn vector or other unsupported leg type in flight plan type prior to the active vertical waypoint This will prevent vertical guidance to the active vertical waypoint oY Metal eXcesle The current crosstrack exceeds the limit causing vertical deviation to go invalid crosstrack error VNV Unavailable Excessive track The current track angle error exceeds the limit causing the vertical deviation to angle error go invalid a CONE A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 The selected waypoint xxxx does not use the WGS 84 datum Cross check waypoint for navigation xxxx p
47. single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and 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 trademarks of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc Ryan is a registered trademark of Avidyne Corporation December 2007 190 00567 01 Rev B Printed in the U S A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 WARNINGS CAUTIONS amp NOTES B O O 666 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 n
48. tae oo b O OFT 100r7 Salina VOR SLN Figure 6 32 Transition to GPS Flight Plan 6 26 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 Altitude at a constant airspeed This descent method does not account for flight plan waypoint altitude constraints e Vertical Path Tracking descent Vertical Path Tracking Mode is used to follow the vertical descent path detined 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 SECTION 6 AUTOMATIC FLIGHT CONTROL b Press the FLC Key to activate Flight Level Change Mode The an
49. 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 specitied altitude 6 368 feet after crossing the MAP a direct to will be established to this fix until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to will be 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 will be established to the published tix 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 to the Missed Approach Hold Point MAHP In this case the altitude fix would be labeled 5500rFr Again if the aircraft altitude is lower than this prescribed altitude a direct to will be 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 A direct to is initiated to MOGAL which is the Missed Approach Hold Poi
50. the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration deceleration is maintained Vspeed References Vspeed References are turned on or off in the Timer References Window Select 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 2 3 SECTION 2 FLIGHT INSTRUMENTS 2 4 2 2 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 Roll Pointer 2 Roll Scale G Horizon Line 4 Aircraft Symbol Land Representation C Aircraft Wing Tips 7 Pitch Scale Slip Skid Indicator E Sky Representation 10 Roll Scale Zero Figure 2 6 Attitude Indicator Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 2 3 ALTIMETER Altitude Altitude Reference Reference Box Bug Altitude Trend Current Vector Altitude Barometric Altitude Minimums Bug 800 p arometric 29 52IN
51. 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 transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds a GPS AP NMS 10000rr ALT The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft 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 4 The autopilot flies the holding pattern after the missed approach is activated Annunciations are displayed in the Navigation Status Box above the AFCS Status Box DIS BRG PON AVN Sd9 NY spon VO Figure 6 38 Go Around Missed Approach GPS 35R KCOS 190 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL 6 6 AFCS ANNUNCIATIONS AND ALERTS nav 108 00 117 95 aa AFCS Status _ AFCS Status Alerts EON The annunciations in Table 6 4 listed in order of increasing priority can appear on the PFDs above the Airspeed and Attitude indicators Only one annuncia tion may occur at a time and messages are prioritized by criticality Aileron Mistrim Righ
52. to the aircraft s present position is ese DOEDE _ fet displayed herah COO ors LPV Select an Airport from the Database fof es 1 With the Airport Information Page displayed press keri Shu eher the FMS Knob to activate the cursor HOGAL mahp 2 Enter the desired airport identifier CURRENT WW PROFILE ACTIVE Vii WET corn A i Select an Airport from the Active Flight Plan mE ang 1 With the Airport Information Page displayed press roonr M the FMS Knob to activate the cursor Turn the small FMS Knob to the left to display a list of flight plan airports as shown in Figure 7 54 HERI ENCL VNV 2 Figure 7 50 Hold Established 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 l 21 SECTION 7 NAVIGATION AIRPORT 2 Turn the small FMS Knob to the left Initially a flight KMCI plan waypoint list is displayed as in Figure 7 54 The list is populated only when navigating a flight plan 3 Turn the small FMS Knob to the right to display the RECENT airports as shown in Figure 7 56 Figure 7 54 Flight Plan Airport List AIRPORT EHCI 3 Turn the large FMS Knob to select the desired airport 4 Press the ENT Key Select a Nearest Airport Figure 7 56 Recently Entered Airports List 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor airport 2 Turn the small FMS Knob to the left Initially a flight plan airport lis
53. 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 will change from light blue to amber in color 10 6 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 10 4 TRAFFIC INFORMATION SERVICE TIS NOTE If the G1000 is configured to use the optional Ryan 9900BX Traffic Advisory System TIS will not be available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site 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 Traffic Map Page 3 Select the OPERATE Softkey to begin displaying traffic OPERATIING is displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby mode STANDBY will be displayed in the Traffic 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 will be displayed in the lower left of of the screen along with the annuciation that the system has entered Coast mode The system will maintain the traffic display up to 60 seconds until the next data
54. 0KT GPS is Active Navigation Receiver on HSI OAT 77 F ISA 21 F 118 200 136 975 com 136 975 coma R iLEL 01 15 5 Figure 6 22 Navigation Mode 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL When the CDI has automatically switched from GPS to LOC during a LOC ILS approach GPS Navigation Mode remains active providing GPS steering guidance until the localizer signal is captured LOC Navigation Mode is armed in anticipation of localizer signal capture if the APR Key is not pressed prior to the automatic source switch If Navigation Mode is active and either of the following occur the flight director reverts to Roll Hold Mode wings rolled level e Different VOR is tuned while in VOR Navigation Mode VOR Navigation Mode reverts to armed e Navigation source is manually switched e Localizer signal is not captured by the final approach fix FAF 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 th
55. 1 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 12 17 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories Co GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair NAV1 RMT XFR NAV1 remote transter key is stuck NAV2 RMT XFR NAV2 remote transter key is stuck G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair GEA 71 Message Advisories GEA1 CONFIG GEA1 configuration error Contig service req d MANIFEST GEA1 software mismatch communication halted nt Comments A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced The remote NAV1 and or NAV2 transter 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 5 failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 sy
56. 3 Engine Leaning Assist Display First Peaked Cylinder Cessna 350 Indicates First Cylinder to Peak 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 ome SECTION 3 ENGINE INDICATION SYSTEM EIS Leaning for Best Economy 5 Monitor the Peak temperature and continue leaning the mixture until reaching the value 1 Select the SYSTEM Softkey indicated in the Cessna Airplane Flight Manual 2 Select the ASSIST Softkey AFM 3 Lean the mixture until ie of the cylinder s exhuas Selecting the ASSIST Softkey returns the MFD to the ramen se _ j ae je p EIS Display Selecting the SYSTEM Softkey exits the E Figure 32 Sy Se pene weirs Ce eect Display and returns the MFD to default operation 4 Continue leaning the mixture until the last of the cylinders peaks This is indicated by Last being displayed below the last peaking cylinder as shown in Figure 3 4 Indicates Difference Between Present and Peak Temperature of the Last Peaked Cylinder FFLOW GPH 15 0 TEMPERATURE ST F CHT F 1426 1438 1366 4 pea 392 378 378 1900 1400 1402 1374 S15 sap 372 380 352 1750 TE A E d E REE S lewis es eae 1450 Fi iLi 300 1300 200 f 1150 1050 1 s 45 6 Figure 3 4 Engine Leaning Assist Display Last Peaked Cylinder Cessna 350 Indicates Last Cylinder to Peak 3 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B Engine Lea
57. 567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 i TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 1 SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the complete system are found in the G1000 Cessna 350 400 Pilots Guide 190 00552 01 SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions for the Primary Flight Display PFD Multi Function Display MFD GCU 476 MFD PFD Control Unit and the GMA 1347 Audio Panel System NOTE The pilot should read and thoroughly understand the Cessna 350 400 Airplan Flight Manual AFM for limitations procedures and operational information not contained in this Cockpit Reference Guide The Cessna 350 400 AFM always takes precedence over the information found in this guide NOTE Speed ranges and V speeds shown in this guide are for example only Refer to the AFM for values pertaining to the Cessna 350 and Cessna 400 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS QO 0 0 Oo 0O OO PUSH 1 2 CRS BARO PUSH PUSH HDG SYN
58. 67 01 Rev B ALERTS Softkey SECTION 12 ANNUNCIATIONS amp ALERTS from annunciations that are not yet acknowledged Acknowledged annunciations are always above the line Annunciations are displayed in order of priority from top to bottom The highest priority annunciation is displayed at the top of the Annunciation Window Alerts Window The Alerts Window displays alert text messages Up to 64 prioritized alerts can be displayed in the Alerts Window Selecting the ALERTS Softkey displays the Alerts Window Selecting the ALERTS Softkey again removes the Alerts Window from the display When the Alerts Window is displayed the pilot may use the large FMS Knob to scroll through the alert list Higher priority alerts are displayed at the top of the window Lower priority alerts are displayed at the bottom of the window Active alerts are displayed in white text Alerts that have become inactive will change to gray text The ALERTS Softkey will flash if the state of a displayed alert changes or a new alert is displayed The inactive alerts can be removed from the Alerts Window by selecting the flashing ALERTS softkey ALERTS Softkey Annunciation When the Alerting System issues an alert the ALERTS Softkey is used as a flashing annunciation to accompany an alert During the alert the ALERTS Softkey assumes a new label consistent with alert level WARNING CAUTION or ADVISORY Pressing the softkey annunciation acknowledges that th
59. 7 Nearest Airports Window PFD 1 Select 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 active NAV frequency field 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 350 400 SECTION 4 NAV COM amp TRANSPONDER 4 6 TRANSPONDER Mode Selection The STBY ON ALT GND VER CODE and IDENT Softkeys can be accessed by pressing the XPDR Softkey Ground Mode Automatic or Manual GND is displayed when the aircraft is on the ground or when the GND Softkey is pressed The transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely address Mode S interrogations pT EK OSY Figure 4 8 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 Wh
60. 9 1 9 1 Arrivals and Departures 5115551151111111112 9 1 Load and Activate a Departure Procedure uu 9 1 Load and Activate An Arrival Procedure 9 1 9 2 Approaches eerrerrerrrrrrrrr 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 00000 10 1 10 1 Customizing the Hazard Displays on the Navigation Map 0 cccccccsceseesteeeesen 10 1 10 2 STORMSCOPE Optional 350 only 10 1 Displaying Stormscope Lightning Data on the Navigation Map PAG eG s scuireutehataveniasertumnaoaiuvates 10 1 SUOMMSCON Ee Esd a 10 2 10 3 XM Weather Optional 0 0 0 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 and Symbols ssssssecseeseesseen 10 5 Weather Product AQE ssssssssesssesssessesssesneessesssen 10 6 10 4 Traffic Information Service TIS 10 7 Displaying Traffic on the Traffic Map Page 10 7 Displaying Traffic on the Navigation Mapu 10 7 TS AUGIO AE eei 10 7 10 5 Ryan 9900BX Traffic Advisory System TAS LODTION Al nasama 10 8 Displaying Traffic on the Traffic Map Page 10 8 Displaying Traffic on the Navigation Map 10 8 190 00567 01 Rev
61. A GARMIN G1 01010 Integrated Flight Deck Cockpit Reference Guide Cessna 350 400 SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV COM TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE Copyright 2006 2007 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0530 04 or later for the Cessna 400 and System Software version 0545 00 or later tor the Cessna 350 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
62. A alerting is disabled the Timer Reterences Window The altitude ranges from 0 to 16 000 feet in 10 foot increments The minimums are Within 2500 ft Within 100 ft reset anytime the power is cycled p 00 MINIMUMS 4BARO 15Q0FT Figure 2 16 Barometric Minimum Descent Altitude Settings Paci Minimum Bug Set the barometric altitude minimums Barometric _ 1 Press the TMR REF Softkey Pannen 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 BARO MIN 3U U4IN 5 To remove the window press the CLR Key or the TMRIREF Softkey Figure 2 17 Barometric Minimum Descent Altitude Alerting Visual Annunciations The desired barometric minimum descent altitude MDA or Decision Height DH can be set in the Timer References Window Visual annunciations alert the pilot when approaching the MDA e When the aircraft altitude descends to within 2500 feet of the MDA setting the Barometric Minimum Box appears with the altitude in light blue text The bug appears on the tape in light blue once in range e When the aircraft descends 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
63. A 63W Integrated Avionics Units and WAAS is 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 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 DIS 3 NH BRG Jd 136 975 118 080 com 136 975 118 000 conz o eE p i l E m E p Glidepath eed M Indicator E 2500 p 2400 ESI LPV Approach a R LEL 055054 Figure 6 15 Glidepath Mode Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B _ 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 lope upon release of the CWS Button Approach Mode Active Active ILS Frequency i Sa Tuned Command Bars Indicate Desc
64. ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS ALT FSHER 352 9 8M 1000 FT PYNON 352 11 93m 10000FT Approach KCOS RNAV 35RGPS LPV HABUK iof 021 5 9M J000FT FALUR 261 5 0NH 8600 CEGIX faf 351 GON 7800F1 RW3S5R aap 351 5 1NH 6368FT 348 O 4NH 6370r1 MOGAL mahp 1000061 6 0NH CURRENT VNV PROFILE ACTIVE VNV WPT 10 000FT at OPSHN 3NH VS TGT 7S6FPM FPA VS REQ 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 will be computed to maintain the 2 5 FPA To change the vertical flight path perform the following steps 190 00567 01 Rev B SECTION 7 NAVIGATION a Press the VNV PROF Softkey to place the cur 15 As seen in Figure 7 36 the aircraft is approaching sor in the target vertical speed field VS TGT as TOD Note the target vertical speed required to shown in Figure 7 35 reach the selected altitude The Vertical Deviation b At this point the descent vertical speed can be Indicator VDI and the Required Vertical Speed selected or the FPA can be selected Turn the Indicator RVSI are now displayed on the PFD as large FMS Knob to select the desired selection shown in Figure 7 37 field then turn the small FMS Knob to enter the FPL ACTIVE FLIGHT PLAN 136 975 HOATH UF I CTIVE FLIGHT _FLAH
65. AFCS Keys In addition to the AFCS Automatic Flight Control System keys on the MFD as discussed in the System Overview section the following buttons and switches used by the AFCS are located in the cockpit separately from the PFD and MFD e AP DISC Autopilot Disconnect Button Located on the left and right control sticks pressing this button disengages the autopilot Pressing it also acknowledges an autopilot disconnect e CWS Control Wheel Steering Button Located on the left and right control sticks pressing and holding the CWS button disengages the control surface servos without disengaging the autopilot If the flight director has not been activated pressing 190 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL the CWS button will activate the flight director in the default pitch and roll hold modes e GA Go Around Button Located on the instrument panel the Go Around Button disengages the autopilot and selects the Go Around wings level mode e MET Manual Electric Trim Switch This switch is used to operate manual electric pitch trim Moving the switch forward trims the aircraft nose down Moving the switch aft trims the aircraft nose up 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 limi
66. C CRS CTR RANGE Romie Figure 1 1 PFD MFD Controls 000 PUSH CHEH Oe O MFD Only 1 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System AFCS keys located only on the MFD bezel NAV VOL ID Knob Controls the NAV audio level Press to turn the Morse code identifier ON and OFF Volume level is shown in the field as a percentage NAV Frequency Transfer Key Transfers the standby and active NAV frequencies Dual NAV Knob Tunes the MHz large knob and kHz small knob standby frequencies for the NAV receiver Press to switch the tuning box light blue box between the NAVI and NAV2 fields Heading Knob Turn to manually select a heading on the HSI When pressed it synchronizes the heading bug with the compass lubber line Selected Heading provides the heading reference to the Flight Director while operating in Heading Select Mode Joystick Changes the map range distance top Q 190 00567 01 Rev B to 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 currentl
67. DB Information Page 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 7 24 With the NDB 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 If there are duplicate identifiers in the database a list is displayed trom which to choose the desired location Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Figure 7 59 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 00567 01 Rev B 7 8 USER WAYPOINT INFORMATION PAGE
68. DIO AUDIO SELECTION Pressing NAVI or NAV2 selects and deselects the radio source and activates the annunciator Selected audio can be heard over the headset and the speakers These two keys can be selected individually or together SECTION 5 AUDIO PANEL Figure 5 6 Navigation Radios 5 5 INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select who is isolated from hearing the NAV COM radios and music Selection scenarios are addressed in Table 5 1 CREW w PILOT COPLT ICS ISOLATION Figure 5 7 ICS Isolation PILOT KEY COPLT KEY Pilot Hears Conilot Hears Passenger ANNUNCIATOR ANNUNCIATOR p Hears 190 00567 01 Rev B FF FF ON ON Table 5 1 ICS Isolation Modes Selected radios pilot copilot passengers MUSIC 1 Selected radios pilot Selected radios pilot passengers MUSIC 1 Selected radios pilot copilot Selected radios pilot copilot passengers MUSIC 2 Selected radios pilot copilot passengers MUSIC 1 Copilot passengers MUSIC 1 Copilot passengers MUSIC 2 Selected radios pilot passengers MUSIC 2 Copilot Selected radios pilot copilot Passengers MUSIC 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 J SECTION 5 AUDIO PANEL 5 4 5 6 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 switc
69. FLIGHT INSTRUMENTS Metric Display Display altitude in meters and barometric pressure in hectopascals 1 2 3 4 5 Press the PFD Softkey to display the second level softkeys Press the ALT UNIT Softkey Press the METERS Softkey to display altitude in meters Press the HPA Softkey to display the barometric setting in hectopascals Press the IN Softkey to display the barometric setting in inches of mercury Press the BACK Softkey to return to the previous level softkeys Figure 2 9 Altimeter Metric 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 2 5 SECTION 2 FLIGHT INSTRUMENTS 2 6 Low Altitude Annunciation WAAS Only A NOTE The LOWALT annunciation is not available when the G1000 is configured with TAWS Terrain Awareness amp Warning System unless TAWS is inhibited When the Final Approach Fix FAF is the active waypointin a GPS WAAS approach using vertical guidance a LOW ALT Low Altitude annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed altitude at the FAE The annunciation initially flashes After a few seconds the flashing stops and the annunciation is displayed as shown in Figure 2 10 Low Altitude Annunciation Figure 2 10 Low Altitude on GPS Approach Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 2 4 VERTICAL DEVIATION GLIDEPATH GLIDESLOPE INDICATOR The Vertical De
70. FMS Knob in the direction of the green arrow to display the next runway for the selected airport Continue turning the small FMS Knob to select the desired runway 4 To remove the flashing cursor press the FMS Knob Access Frequency Information 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 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 trequency has sector or altitude restrictions the frequency is preceded by an info i designation Figure 7 57 Intersection Information Page Press the ENT Key to view the information The following may be displayed with the frequency Access Information on an Intersection e TX transmit only 1 With the Intersection Information Page displayed e RX receive only press the FMS Knob to activate the cursor e PT part time frequency 2 Enter an intersection identifier and press the ENT 4 Press the ENT Key to place the selected frequency Key in the standby field of the COM or NAV box 3 Press the FMS Knob to remove the flashing 5 To remove the cursor press the FMS Knob cursor 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 a SECTION 7 NAVIGATION 7 6 1 2 NDB INFORMATION Pipro Figure 7 58 NDB Information Page Select the N
71. Guide for the Cessna 350 400 J SECTION 9 PROCEDURES AIRPORT 118 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 either 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 will become the active flight plan 9 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 9 2 APPROACHES 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 will not have this designation meaning the GPS receiver can be used for suppl
72. IA1 and or GIA2 temperature is too high If problem persists the G1000 GIA2 COOLING GIA2 over system should be serviced temperature GIA1 SERVICE GIA1 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 GIA2 SERVICE GIA2 needs service system should be serviced Return the unit for repair HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system MANIFEST GIA2 software should be serviced mismatch communication halted Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 COM2 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 ke eerie P y The COM1 and or COM2 external push to talk switch is stuck in the e
73. J 136 975 136 975 Nav 108 48 117 9 NAV 117 9 13200 13108 m WEL 12900 a ao ke an 12sne TTF ISA 21 F 6 T 7 PDR INSET XPOR IDENT THR REF System Time C Transponder Data Box Selected Heading Bug 11 Turn Rate Indicator 12 Altimeter Barometric Setting 13 Vertical Speed Indicator VSI Selected Altitude Bug Figure 2 1 Primary Flight Display Default NAV Frequency Box Airspeed Indicator G True Airspeed 4 Current Heading G Horizontal Situation Indicator HSD 6 Outside Air Temperature OAT C Softkeys 190 00567 01 Rev B TA ALERTS l Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 indicated The gradient color 118 808 con con 090006000 006096 R Lo 0550 54 15 Altimeter Selected Altitude 17 COM Frequency Box AFCS Status Box Navigation Status Box Slip Skid Indicator 21 Attitude Indicator 2 SECTION 2 FLIGHT INSTRUMENTS NAVI nave 108 084 177 95 OAT J7 FIISA 21 F INSET Traffic Annunciation Vspeed References G Selected Heading 4 Wind Data G Inset Map Active Flight Plan Leg I Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 2 118 875 133 088 con 136 975 DOH H E 1266 E a c 508 egua E cii HARU HIN 2JSHTIH 126HFT tarik LOW FUEL L Low fuel in the lef tank l TRAFFIC FAIL
74. 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 identitier 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 190 00567 01 Rev B SECTION 8 FLIGHT PLANNING 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 apply trip planning calculations to the entire flight plan Selecting FPL 00 will display an active flight plan If an active flight plan is selected REM will be 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 7 Turn the FMS Knobs t
75. LU VS TGT TERRAIN mp 100rt im 1000r1 30nn CNCL VNV Figure 7 46 Descending to the FAF 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 Eki a _NORTH UP l ACTIVE FLIGHT PLAN Pens TFR KMKC KEOS S i DATA A HI DATA DTE prs FSHER eee paced SE PYNON oe ee ad Approoch KOOS RNAVY 35Riees LP HABUK of E G _SECUHITY WIDEFIELO FALUR i BJGBFT said j fy a CEGL fof DET ee fee RH25F mop 5 4 3HH BS68FT 348 DANA mmt HOGAL mohp 6 8NH JQURRENT WH PROFILE ACTIVE Wh WET FT at VS TGT VS REO V DEV Figure 7 47 Descending to the Missed Approach Point 7 19 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
76. O FROM Indicator Scale Figure 2 19 Arc HSI Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 2 9 SECTION 2 FLIGHT INSTRUMENTS 2 10 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 O finn naie Standard Turn Trend Vector Rate Tick Mark rate gt 4 F deg sec Turn Rate Trend Vector standard rate Figure 2 21 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Figure 2 22 Course Pointer Course Deviation Indicator CDI The CDI scale automatically adjusts to the current phase of flight as seen in Figure 2 23 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 Approach LPV WAAS only 1 0 nm dec
77. PFD coastlines terrain rivers lakes etc and OFF Press to remove the Inset Map elevation scale on the Inset Map DCLTR 3 Press momentarily to select the desired TERRAIN Press to display terrain information on amount of map detail The declutter level appears the Inset Map adjacent to the DCLTR Softkey STRMSCP optional Press to display the No declutter All map features are visible Stormscope lightning data on the Inset Map Declutter 1 Declutters land data within a 200 nm radius of the aircraft Declutter 2 Declutters land and SUA data NEXRAD optional Press to display NEXRAD Declutter 3 Declutters large NAV data weather and coverage information on the Inset remaining removes everything except the Map active flight plan XM LING optional Press to display XM lightning TRAFFIC Press to display traffic on the map information on the Inset Map BACK Press to return to the previous level softkey configuration 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1 7 SECTION 1 SYSTEM OVERVIEW SoA RST ALERTS y annene aaa A A A A L IE Mess Jiac AE 8c _J aterrs SONSAN AnNnNnNDNDN w A L IE om J ome ems Lo LEE ack J avers Rn nnnnnnrnieannki DO A LLL fwerers sea JLT back J nnn nenoennniaAnienk D mA Press the STD BARO or BACK Softkey to return to the top level softkeys Figure 1 5 PFD Conf
78. PL 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 at the Decision height and land the aircraft e Use the GA Switch to execute a missed approach SECTION 6 AUTOMATIC FLIGHT CONTROL KCOS SPO d9 lddV Sd9 SPOIN AVN Sd9 Figure 6 37 LPV Approach to KCOS 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 31 6 32 SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around Missed Approach 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 _ GA AP 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 Press the SUSP Softkey to begin navigating to the Missed Approach Hold Point c Press the NAV Key to have the autopilot fly to the hold _ GPS AP ALTS 3 Use the ALT Knob
79. 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 12 Procedures GFC 700 6 23 6 34 190 00567 01 Rev B Remove departure arrival or approach 8 6 Replies 4 4 Required Vertical Speed 2 6 7 15 Required Vertical Speed Indicator 7 15 Reversionary mode 11 1 ROC 10 12 10 15 12 6 Roll Axis Modes 6 2 Roll Hold Mode ROL 6 17 Roll modes flight director 6 16 6 19 Roll Reference 6 17 RTC 10 12 RVSI 7 15 7 16 RX indicator 4 3 R indication 4 4 S Secure Digital SD card 1 14 Selected Altitude 2 1 6 6 6 10 6 13 Selected Altitude Bug 2 1 Selected Altitude Capture Mode 6 6 6 10 6 13 Selected Course 2 2 6 20 Selected Heading 2 2 6 18 Servos 6 21 Severe thunderstorm 10 5 SIGMET 10 5 Slip Skid Indicator 2 1 Slip Skid indicator 2 4 Softkeys PFD 2 1 Softkey function MFD 1 7 1 10 Speed ranges 2 3 Split COM 5 2 SQ 1 3 Squelch 5 4 STBY Softkey 4 4 Store Flight Plan 8 6 Stormscope lightning data 1 7 1 10 10 2 10 3 Strike 10 2 190 00567 01 Rev B Strike mode 10 2 System annunciations 12 1 12 7 System message advisories 12 9 System time 2 1 T TA 10 7 TAF 10 3 TAS 10 8 10 9 12 19 TAWS 10 10 10 12 10 14 10 16 12 6 12 7 TAWS B 10 10 TAWS system test 10 12 Terrain 10 9 10 10 10 14 11 2 12 12 Terrain proximity 10 9 TIT 3 5 TOD 7 15 7 18 Top of Descent 7 15 Tornado 10
80. Pull Up Pull Up Aural Message Caution Terrain Caution Terrain or Terrain Ahead Terrain Ahead Imminent Terrain Impact Caution ITI Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain o es Reduced Required Terrain Clearance Caution RTC Reduced Required Obstacle Clearance Caution Obstacle Caution Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Imminent Obstacle Impact Caution IOI Premature Descent Alert Caution PDA Too Low Terrain Altitude Callout 500 Five Hundred Excessive Descent Rate Caution EDR TERRAIN see Sink Rate Negative Climb Rate Caution NCR DONT SINK Don t Sink or or TOOLOW TERRAIN Too Low Terrain 12 6 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 12 ANNUNCIATIONS amp ALERTS TAWS System Status Annunciations PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert TAWS System Test Fail TAWS FAIL TAWS System Failure Aural Message No GPS position or excessively degraded TAWS N A None TAWS Not Available GPS signal TAWS Availble will be heard when sufficient GPS signal is re established System Test pass TAWS System Test OK 12 6 G1000 SYSTEM ANNUNCIATIONS ea S A NOTE Upon power up of the G1000 system When an LRU or
81. Reference while climbing or descending to e 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 Reference 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 350 400 190 00567 01 Rev B 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 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 tflying the aircraft to a new airspeed then re
82. S Knob to highlight the desired approach Press the ENT Key 1 8 SECTION 9 PROCEDURES The cursor will move 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 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 will initiate a direct to for IAF and the G1000 will immediately begin navigating to the IAF Selecting Load will add 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 350 400 J3 SECTION 9 PROCEDURES Blank Page 9 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 Navi
83. S Position DEAD RECKONING WARNING DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to deter mine a position Changes in wind speed and or wind direction will compound the relative inac curacy 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 will automatically revert 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 190 00567 01 Rev B NOTE Dead Reckoning Mode will only function in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution will produce a NO GPS POSITION annunciation on the map and the G1000 will stop 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 will be 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 re
84. ST Softkey displays the Checklist Page SYSTEM Displays engine softkeys DONE Pressing this softkey checks off a checklist item If an item is already checked an UNDO Softkey will be displayed EXIT Press to exit the checklist EMERGCY Pressing this softkey displays the emergency checklist Nearest Group Auxiliary Page Group Waypoint Page Group Map Page Group 1 5 SECTION 1 MFD PAGE GROUPS Turn the large FMS Knob until the desired page a group is selected Turn the small FMS Knob to select pages within the group See Figure 1 8 Number of Pages in Current Group Figure 1 8 Page Group Icon Selected Page 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1 11 SECTION 1 SYSTEM OVERVIEW 1 12 1 6 VERTICAL NAVIGATION In WAAS capable installations one of two altitude sources is used by the G1000 when giving vertical navigation guidance WAAS GPS altitude is used when giving guidance for a WAAS approach 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 Cr
85. Setting Box Figure 2 7 Altimeter Altitude Select Bug The Altitude Select Bug is displayed at the selected altitude or if the selected altitude is beyond the altitudes currently displayed the bug is displayed at the top or bottom of the display whichever is closest to the selected altitude Set the Selected Altitude Bug Turn the ALT Knobs to set the Altitude Select 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 Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained 190 00567 01 Rev B Barometric Setting Box Select barometric pressure Turn the BARO Knob to select the desired setting Quickly enter standard pressure 1 Press the PFD Softkey 2 Press the STD BARO Softkey Altitude Alerting Within 1000 ft Within 200 ft Deviation of 200 ft E 4000 E 400A Figure 2 8 Altitude Alerting Visual Annunciations Visual annunciations appear in the Selected Altitude Box Whenever the Selected Altitude is changed the Altitude Alerter is reset The Altitude Alerter is independent of the Automatic Flight Control System An aural tone is heard when the aircraft is within 200 feet of acquiring the selected altitude or when deviating beyond 200 feet of the acquired selected altitude SECTION 2
86. T Key The selected frequency 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 350 400 7 25 SECTION 7 NAVIGATION Nearest Airports Information on the PFD Bearing TO Distance Airport Symbol NEAREST AIRPORTS U56 E er 9 3NM VFR 3500FT 9 5NM ILS TOWER 118 500 RNWY 9001FT KRXE 4 352 20 1NM VOR UNICOM 122 800 RNWY 4200FT Identifier Runway Length MULTICOM 122 900 RNWY KIDA 261 Primary COM Frequency Figure 7 61 Nearest Airports Window Press the NRST Softkey to display the PFD Nearest Airports 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 will be placed in the COM standby frequency field 3 Press the Frequency Transfer Key to make the frequency the active frequency 7 26 Garmin G1000 Cockp
87. The display is updated every five minutes Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 will be the highest level sampled within the square area ECHO TOP Select the ECHO TOP Softkey to show the location elevation and direction the highest radar echo This may not indicate the top of a storm or clouds only the highest radar return echo ECHO TOPS cannot be displayed along with NEXRAD and CLOUD TOPS When ECHO TOPS is activated NEXRAD and CLOUD TOPS are removed Refer to the Legend for a description of the ECHO TOPS coding The display is updated every 7 5 minutes CLD TOP Select the CLD TOP Softkey to show the cloud top altitude determined from satellite imagery The display is updated every 15 minutes LING Selecting the LING Softkey shows the location of cloud to ground lightning strikes The display is upda
88. UPDATING AVIATION DATABASE PLEASE WAIT UPDATED TRIVES SULCESSEURL YT PRESS ANY KEY TO CONTINUE CONTINUING IN 8 SECONDS Figure 1 13 Database Update Confirmation 4 After the update completes the PFD starts in normal 5 6 1 mode Turn the G1000 System OFF and remove the SD card Repeat steps 1 through 4 for the MFD The MFD and PFD databases are now updated Remove the SD card when finished Verify that the correct update cycle is loaded during startup of the MFD Garmin Databases Since these databases are not stored internally in the MFD or PFD a Supplemental Data Card containing identical database versions must be kept in each display unit 190 00567 01 Rev B NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data 1 2 3 4 5 SECTION 1 SYSTEM OVERVIEW 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 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
89. W5A APPROACH RNAV 3SRePs LPW IRI mikit NDE 35L maar y wot wlhe RHJSR mop 351 5 144 B35SrT 38 Bdrm MOGAL mohp HOLD 50 BEN LOAD oR ACTIVATE Figure 7 31 List of Available Approaches 190 00567 01 Rev B 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 b PUBLIC CITY OF COLORADO SPRINGS COLORADO SPRINGS CO APPROACH CHANNEL CHANNEL 97799 I0 W35A RNAV 35Rops LPV TRANSITION HABUK lof VECTORS iouenc HIDRAKE FUE HABUK inf FALUR B N CEGIN fof G m RH35R mop Dim B3B3FT 348 0 O 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 will be used g Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 7 13 SECTION 7 NAVIGATION 7 14 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 a Or A ACTIVE FLIGHT PLAH KMKC KOOS hei GERE p S Arrival RCOS TEE DGRY LALL OPSHN 3mh 260 66 3nh 10000F OPSHN 259 FSHER SZ JAHH PYNON 1194H F J NNI F
90. 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 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 e Flight Level Change Maintains the current aircraft airspeed while the aircraft is climbing descending to the Selected Altitude e Vertical Path Tracking Follows an active vertical profile for enroute and terminal phases of flight only available with WAAS capable system e VNAV Target Altitude Capture Captures the VNAV Target Altitude e Glidepath Intercepts and tracks the WAAS glidepath on approach only available with WAAS capable system 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 350 400 6 3 SECTION 6 AUTOMATIC FLIGHT CONTROL
91. afety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe oo WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Cessna 350 400 Pilot s Operating Handbook 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 m
92. affic Figure 10 13 TAS Traffic on Navigation Map 10 6 TERRAIN AND OBSTACLE PROXIMITY Terrain Obstacle above or within 100 A NOTE Terrain data is not displayed when the below or above aircraft altitude aircraft latitude is greater than 75 degrees north Terrain Obstacle between 100 and 1000 Displaying Terrain and Obstacles on the Terrain opp ___Areraft altitude Proximity Page 1000 1 Turn the large FMS Knob to select the Map Page Group ei SE Ea STE 2 Turn the small FMS Knob to select the last rectangular page icon 3 If desired select the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey 1 With the Navigation Map displayed select the MAP is selected a radar like 120 view is displayed Softkey Select the 360 Softkey to return to the 360 default 2 Select the TERRAIN Softkey Terrain and obstacle display proximity will now be displayed on the map Displaying Terrain and Obstacles on the Navigation Map 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 10 9 SECTION 10 HAZARD AVOIDANCE Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Height is less than Height is less than Height is greater than Height is greater than 1000 AGL 1000 AGL 1000 AGL 1000 AGL Figure 10 15 Obstacle Symbols 17 95 10 7 TERRAIN AWARENESS amp WARNING yi SYSTEM TAWS DISPLAY OPTIONAL A NOTE Terrain data is n
93. ain Clearance RTC and Reduced Required Obstacle Clearance ROC This provides alerts when the aircraft flight path is above terrain and or obstacles yet is projected to come within minimum clearance values outlined in the following table When an RTC or ROC alert is issued a potential impact point is displayed on the TAWS Page as a yellow or red X Imminent Terrain Impact ITI and Imminent Obstacle Impact IOI This provides alerts when the aircraft is below the elevation of terrain in the aircrafts projected path ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS Page as a yellow or red X The alert is given when the projected vertical flight path is calculated to come within minimum clearance altitudes in the following table Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Phase of Flight Level Flight 508 T Approach 150 ft 100 ft 08 co During the final approach phase of flight RTC ROC ITIIOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0 5 nm of the approach runway or is below 125 feet AGL while within 1 nm of the runway Premature Descent Alert PDA A Premature Descent Alert is issued when the system detects that the aircraft is significantly below the normal approach path to a runway The PDA alert mode functions only during descent to land PDA alerting begins when the aircraft is within 15 nm of the destinat
94. al Navigation Mode NOSE UP NOSE DN Keys Controls the active pitch reference for the Pitch Hold Vertical Speed and Flight Level Change Modes 190 00567 01 Rev B 1 2 GCU 476 CONTROLS oO The indicators above the PFD MFD NAV and COM Keys are lit when the respective control mode key is pressed The unit is in MFD Control Mode by default until the PFD Control Mode selection key is pressed Many of the controls duplicate the controls on the PFD and MFD The discussions later in this manual are cen tered around using the controls on the PFD and or MFD When reading these discussions keep in mind that many of the operations may also be performed on the GCU G 40 D OW S El FM NAV COM RANGE oe Ea P MENMU cr OM e gt RO Y PROC Z R Q EMERG i aa 2 NAV COM Qm G O SOFTKEY sevect DFLT MAP l O q b CLA Q Figure 1 2 MFD PFD Control Unit GCU 476 SECTION 1 SYSTEM OVERVIEW FPL Key Displays the active Flight Plan Page for creating and editing the active flight plan Direct to Key Allows the user to enter a destination waypoint and establish a direct course to the selected destination the destination is either specified by the identifier chosen from the active route or taken from the map pointer position MENU Key Displays a context sensitive list of options This list allows the user to access additional features or make setting
95. allowing upcoming descent legs to be captured and subsequently tracked Altitude Reference In This Case Equal To VNAV Altitude Target AFT ALT VPTH Flash up to 10 sec Indicating Automatic Transition M E 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 350 400 6 14 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 GPS 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 naw 108 08 117 95 nav2 108 8 117 95 i 17037 Command Bars B Es Indicate Descent on Glidepath HSI Set to GPS TEGESAN r l ral rire Ti Pil 1ta n NOTE Glidepath Mode is available only in installations with GI
96. an dikit niini kii m a a j 1 1 4 amp pe a GA SSS OAT TFF TSA 421 F tilad x a 85 04 05 Figure 6 5 Pitch Hold Mode 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 see the discussion on Vertical Navigation Modes later in this section 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 ho
97. ancel the direct to 7 3 NAVIGATING AN EXAMPLE FLIGHT PLAN A NOTE The following example flight plan is for instructional purposes only All database information depicted should be considered not current The following discussion is an example of navigating a flight plan with the WAAS capable GPS system while the G1000 provides vertical guidance through descents A lateral flight plan LNAV would be navigated in much the same way but would not include vertical guidance when the final approach course is active The example is a flight plan from KMKC to KCOS filed using the TIFTO2 departure various Victor Airways and the DBRY1 arrival with the transition at TBE Enroute altitude will be 12 000 feet An LPV WAAS approach will be selected for runway 35R A missed approach will be executed at the Missed Approach Point MAP A few enroute changes are demonstrated A NOTE If the loaded arrival procedure has published altitudes contained in the navigation database these are for turbojet aircraft only Accept or change these values as desired to meet the requirements of the clearance 1 Prior to departure the TIFTO2 departure the airways and the DBRY 1 arrival at KCOS are loaded Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 i SECTION 7 NAVIGATION See the Procedures section for loading departures and arrivals Note the magenta arrow in Figure 7 11 indicating the active departure leg After tak
98. appearing in the Annunciation Window is YELLOW A caution alert is also accompanied by a flashing CAUTION Softkey annunciation as shown in Figure 12 3 Selecting the CAUTION Softkey acknowledges the presence of the caution alert Figure 12 3 CAUTION Softkey Annunciation 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 Selecting 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 350 400 190 00567 01 Rev B SECTION 12 ANNUNCIATIONS amp ALERTS 12 2 AIRCRAFT ALERTS See the Airplane Flight Manual for information regarding pilot responses WARNING Alerts Annunciation Window Text Alerts Window Message Audio Alert Voice Message Repeating Chime Door Open Fuel tank is not correctly selected Chime Fuel Valve or in OFF position CAUTION Alerts Cessna 350 only 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 ieee SECTION 12 ANNUNCIATIONS amp ALERTS Annunciation Advisory Annunciation Window Text Alerts Window Message Audio Alert OXYGEN ON Reminder Turn off oxygen SPEED BRAKES Speed
99. 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 Seng etna ypetnl Arriving at waypoint xxxx 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 j MERR AA ACE r Special use airspace is near and ahead of the aircraft position o wan een A Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1221 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont SLCT FREQ Select appropriate The system notities the pilot to load the approach trequency for the appropriate frequency for approach NAV
100. ct 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 f arm Approach and Glideslope modes LOC and o y GS appear in white as armed mode annuncia tions Figure 6 36 ILS Approach to KCOS LOC HDG AP ALT 9000F GS c The navigation source automatically switches to LOC After this switch occurs the localizer signal can be captured and the flight director determines when to begin the turn to intercept the final approach course The flight director now provides guidance to the Missed Approach Point apo SD lddV 207 PETEY PON AVN Sd5 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 6 30 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B Flying a WAAS precision approach 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 Select the Runway 35R LPV approach for KCOS Load and activate the approach into the flight plan 2 Press the APR Key once clearance for approach has been acquired GPS Approach Mode is activated and Glidepath Mode is armed _ GPS A
101. d 7 Turn the small FMS Knob to enter the desired VNV altitude 8 Press the ENT Key The option to select MSL or AGL is now displayed 9 Turn the small FMS Knob to select MSL or AGL 10 Press the ENT Key The cursor is placed in the VNV 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 again to activate the Direct to Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 __DIRECT TO KMIA MIAMI FL OFFSET SNH KIXD pe k ee KSLN lOVATL inf DIGBE 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 ENT 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 lef
102. d by XM Radio ge e ee i MINNEAPOLTS ST PAUL INTL Service is approved only for weather avoidance MENNEAPOLTS MA not penetration a 1 Select the MAP Softkey i rT TE 2 Select the NEXRAD or XM LTNG Softkey to display ee 6 the desired weather Select the applicable softkey TEMPERATURE 23 DEW POINT 14 c again to remove weather data from the Navigation ALTIMETER 28 721 Map Paae T ae 1386 975 100 core cae TAF Text Softkey Figure 10 8 METAR and TAF Text Displayed on the Airport Weather Information Page Figure 10 7 Navigation Map Page Displaying NEXRAD Weather 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 10 3 SECTION 10 HAZARD AVOIDANCE Displaying Weather on 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 Weather Data Link Page Select the available softkeys to select the desired XM weather product Select 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 Softkey to return to the map i ICELL MOV SIG AIR METAR LEGEND HORE WX Figure 10 9 Weather Data Link Page NEXRAD Select the NEXRAD Softkey to show 10 4 NEXRAD weather and radar coverage information Areas where radar coverage is not available will be shown in grayish purple
103. desired value me KMKC KCOS NO DATA Note the information now displayed in the ine LAA TEN CURRENT VNV PROFILE box Also note the ee poda Der ee offset waypoint and a gray circle labeled TOD a ee a are now displayed on the map The gray circle OPS 759 AM 10000FT marks the Top of Descent TOD In this example a ee ae after passing the TOD point vertical guidance ai Aopronch KCOS RNAV 3SRGPS LPY HABUK iaf BT 3 43NH S000 will be provided that will result in a 3 0 degree FALUR 27 S m esor FPA descent to an altitude of 10 000 feet at the z Tepe e e E offset waypoint ve TGT G90FPH FPA 39 TERRAIN VS REG FPL ACTIVE FLIGHT PLAN EAH IE ACTIVE FLIGHT PLAN TFA KMKC KEOS HI DATA r VIEH VA PROP CNOL VNV VA B SHW CHAT LAR z R hirvay V263 7BE Figure 7 36 Approaching Top of Descent TOD TBE are i Arrival RCOS TBE DBRY1 ALL OPSHN 3mm 260 SMON 10000FT TOD within 1 minute 136 975 OPSHN 959 30N 10000FT i 136 975 FSHER 37 SNH 1O000FT FS eee VNAV PYNON SF 11 9 10000eT 1007 a Approach KCOS RNAV 35Rices LPV rene HABUK iaf EFA S Si soad tituae FALUR 251 S 0NH 8600r1 CURRENT VNV PROFILE ACTIVE VA WET TOOOOFT ot OPSHH Jr ae VS TGT 735FPH FPA 30 S WR FPH TIME TOTOO 2330 Vertical S man o oY rt Deviation Indicator VDD Required Vertical i a Speed Figure 7 35 Adjusting the Descent E dicator RVSD c Press the ENT Key Figure 7 37 VDI amp
104. disconnect aural alert After manual disengagement the autopilot disconnect aural alert may be cancelled by pushing the MET ARM or AP DISC Switch AP DISC Switch also cancels the flashing AP an nunciation Autopilot Manually Disengaged a ROL O gt IT ALTS Figure 6 28 Manual Autopilot Disengagement Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 6 AUTOMATIC 6 5 EXAMPLE PROCEDURES USING AFCS 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 GPS Navigation section Refer to the example in Section 7 GPS 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 ey Salina VOR SLN
105. dvisories 12 20 Negative Climb Rate After Takeoff Alert NCR 10 13 Miscellaneous Message Advisories 12 21 Five Hundred Aural Alert 10 13 POD UPATE namiot 10 14 INDEN Ce ee ee ee Index Displaying Terrain and Obstacles on the Navigation E ERA AE E N ATEA E AA 10 1 Alert ANNUNCIatiONS c ccsscesseeseessesseesseeseesteaseeseeaees 10 14 TAWS AIET SUNN GUY ai 10 15 SECTION 11 ABNORMAL OPERATION 11 1 11 1 Reversionary Mode 0 cccccc seers 11 1 11 2 Abnormal COM Operation 0 0 0 00 11 2 11 3 Unusual Attitudes css 11 2 11 4 Stormscope operation with loss of Heading INPUT 2s concrenduconnemarnamecananunnamcuiuomeunonscres 1 2 11 5 Hazard Displays with Loss of GPS Position 11 2 11 6 Dead Reckoning 0 cccccccscesees cesses 11 2 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 12 1 Alert Level Definitions 0 00 ccc een 12 2 12 2 Aircraft Alerts 12 3 WARNING A TERG Saos en 12 3 CAUTONA ellisini 12 3 Annunciation AVISOLY cesccsssessessessesstessesssesseeessen 12 4 Message Advisory Alerts ccsssessssesssessseseesessesseean 12 4 12 3 CO Guardian Messages 11111111eeseeseeen 12 4 12 4 AFCS AlOMtS eoiccidcsscssoriacnioccarantexedonenunianidan 12 5 System Status ANNUNCIATION Pie 12 5 TAWS ALERTS eesicossc sscoscessexecacsamonesscoxeneiaonnanines 12 6 TAWS System Status Annunciations s s s 12 7 190 00
106. e pilot is aware of the alert The softkey then returns to the previous ALERTS label The pilot can then select the ALERTS Softkey again to view alert text messages System Annunciations Typically a large red X appears in a window when a related LRU fails or detects invalid data Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 12 ANNUNCIATIONS amp ALERTS e Audio Alerting System The G1000 system issues audio alert tones when specific system conditions WARNI NG are met See the Alert Levels Definitions section for more information Figure 12 2 WARNING Softkey Annunciation 12 1 ALERT LEVEL DEFINITIONS The G1000 Alerting System as installed in Cessna 350 400 aircraft uses three alert levels WARNING This level of alert requires immediate pilot attention A warning alert is accompanied by an annunciation in the Annunciation Window Warning 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 Selecting the WARNING Softkey acknowledges the presence of the warning alert and stops the aural tone if applicable DYI SORY e CAUTION This level of alert indicates the Figure 12 4 ADVISORY Softkey existence of abnormal conditions on the aircraft Annunciation that may require pilot intervention A caution alert is accompanied by an annunciation in the Annunciation Window Caution text
107. e 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 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 SECTION 6 AUTOMATIC FLIGHT CONTROL Backcourse Navigation Mode is armed when the localizer front course is greater than 105 from the aircratt heading The annunciation BC in the AFCS Status Box indicates Backcourse Navigation Mode When the HSI is coupled to VOR or LOC the flight director creates roll steering commands from the Selected Course and deviation Ifthe 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 from 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 af Navigation Choe Med p Altitude Hold ode Active Meine Mode Armed Command Bars Indicate Left Turn to Track GPS Course and Climb to Intercept Selected Altitude 190 nn TAS 12
108. e data entry It is also used to confirm selections and information entries 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 AP Key Engages disengages the Autopilot and Flight Director Pressing the AP Key activates the Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Flight Director and engages the Autopilot in the default pitch axis and roll axis modes Pressing the AP Key again disengages the autopilot and deactivates the Flight Director 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 NAV Key Selects deselects the Navigation Mode 21 ALT Key Selects deselects the Altitude Hold Mode 22 VS Key Selects deselects the Vertical Speed Mode 23 FLC Key Selects deselects the Flight Level Change Mode HDG Key Selects deselects the Heading Select Mode 25 APR Key Selects deselects the Approach Mode VNV Key WAAS only Selects deselects Vertic
109. e 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 and desired course inputs to fly the approach Approach Mode provides greater sensitivity for signal tracking than Navigation Mode Pressing the APR Key when the CDI is greater than one dot arms the selected approach mode annunciated Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 GPS GPS e ALTS Figure 6 24 GPS Approach Mode Armed LOC Approach Mode allows the autopilot to fly 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 navi
110. e 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 1 SYSTEM OVERVIEW G1000 displays a list that is too long for the display screen a scroll bar appears along the right side of the display indicating the availability of additional items within the selected category Press the small FMS Knob to activate the cursor and turn the large FMS Knob to scroll through the list MENU Key Displays a context sensitive list of options This list allows the user to access additional features or to make setting changes that relate to certain pages 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 complet
111. e rate is every 12 minutes Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols updated every 12 minutes WIND Select 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 selecting the WIND Softkey 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 select the softkey corresponding to the desired e NEXRAD winds aloft altitude The display is updated every Cloud Top Echo Top 12 minutes e XM Lightning COUNTY Selecting the COUNTY Softkey provides e Cell Movement SIGMETs AIRMETs e METARs specific public awareness and protection weather warni
112. e the VOR frequency b Press the CDI Softkey to set the navigation 3 The autopilot continues the turn until the aircraft source to VOR is established on the Selected Course c Use the CRS Knob to set the Selected Course to 255 Note that at this point the flight director i is still in Heading Select Mode and the autopilot continues to fly 290 Salina VOR SLN Figure 6 31 Intercepting a VOR Radial 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 25 SECTION 6 AUTOMATIC FLIGHT CONTROL Flying a Flight Plan GPS Course 2 Following the flight plan the autopilot continues to steer the aircraft under GPS guidance Note that in GPS Navigation Mode course changes defined NOTE Changing the navigation source cancels 7 O ike by the flight plan are automatically made without Navigation Mode and causes the flight director i a to revert back to Roll Hold Mode wings rolled pilot action required level As the aircraft approaches the Salina VOR GPS is used to navigate the next leg airway V244 Flying a GPS flight plan 1 Transition trom VOR to GPS Navigation Mode a Press the CDI Softkey until GPS is the selected navigation source b Press the NAV Key to activate GPS Navigation Mode The autopilot guides the aircraft along the active flight plan leg gt V4 SLN V244 LAA irvay V263 TBE CURRENT VNV PROFILE ACTIVE UNV WPT VS TGT TERRAIN ve
113. eference Guide for the Cessna 350 400 10 1 SECTION 10 HAZARD AVOIDANCE At a map range of less than 25 nm Stormscope lightning data is not displayed but can still be present The presence of Stormscope lightning data is indicated by the annunciation LTNG lt 25 nm in the upper right corner _ NORTH UP NODE CELL LING lt 25nm Figure 10 5 Lightning Display Range Annunciation Select cell or strike as the Stormscope lightning mode on the Navigation Map 1 From the Navigation Map Page press the MENU Key Select Map Setup and press the ENT Key 2 Turn the small FMS Knob to select Weather and press the ENT Key 3 Turn the large FMS Knob to select STRMSCP MODE 4 Turn either FMS Knob to display the Cell Strike Window 5 Turn either FMS Knob to select Cell or Strike Press the ENT Key 6 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope lightning data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Lightning Data field and press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormscope Page is selected 136 975 I COM STRIKE RATE 5 HOG UP Figure 10 6 Stormscope Page Change the Stormsc
114. el mm Press the SYSTEM Softkey to vy Q O po n eS m i te m L Z O TI am m L AIRWAYS Pressing this softkey displays removes airways information The default is dependent on map setup option selected Pressing cycles through all airways displayed AIRWY ON low altitude airways only AIRWY LO and high altitude airways only AIRWY HI STRMSCP optional Pressing this softkey displays removes Stormscope lightning data on the Navigation Map NEXRAD optional Pressing this softkey displays removes precipitation data on the Navigation Map XM LING optional Pressing this softkey displays removes XM Radio lightning data on the Navigation A optional optional Default softkey is dependant on the selection made in the map setup options optional optional optional a ee NA Press the BACK Softkey on this level to return to the top softkey level The DONE Softkey changes to UNDO when the checklist item is already checked ry mm n Figure 1 7 MFD Softkeys 1 10 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 CHKLI
115. eld as shown in Figure 7 28 DIRECT T WN GGR8FT a HAR NORTH UP as SH 15H LOCATION ERG 260 DIS 161NK 257 ACTIVATE Figure 7 28 Enter VNV Offset Distance g Enter the offset or distance from the waypoint at which the selected altitude will be reached In this case three miles prior to OPSHN is entered In other words the G1000 will give vertical guidance so the aircraft will arrive at an altitude of 10 000 feet three miles prior to OPSHN h Press the ENT Key twice to activate the direct to Note in Figure 7 29 the magenta arrow in the Active Flight Plan Window indicating the direct to OPSHN after the offset waypoint for OPSHN The preceding offset waypoint indicates the offset distance and altitude that was previously entered The remaining waypoints in the loaded arrival procedure have no database specified altitudes therefore dashes are displayed Keep the CDI centered and maintain a track along the magenta line to OPSHN Note the Direct to waypoint is within the loaded arrival procedure therefore phase of flight scaling for the CDI will change to Terminal Mode and is annunciated by displaying TERM on the HSI NOTE If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database those altitudes will be displayed as white numerals This indicates the altitudes will not be used by the system for vertical guidance until manually acce
116. emental navigation guidance only If the GPS receiver cannot be used for primary guidance the appropriate 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 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 approach type will be 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 190 00567 01 Rev B Load and or Activate an Approach Procedure 1 2 3 4 5 6 190 00567 01 Rev B 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 will be 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 FM
117. ent on Localizer Glideslope Path Pari TAS 1107 HSI Set to LOC2 OAT TTF ISA 21 F 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 136 975 118 009 con 196 975 118 080 conz a ms Glideslope asf Indicator OOo a z 1l 4400 C aama CE 24 97 1N k LEL 87 25 05 Figure 6 17 Glideslope Mode 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around GA Mode Roll Modes Pushing the GO AROUND button engages the flight director in a wings level 7 pitch up attitude allowing the execution of a missed approach ora go around This mode is a both a pitch and roll mode and is annunciated as GA in both the pitch and roll active mode fields Go Around Mode disengages the autopilot and
118. eoff ATC assigns a heading of 240 2 Figure 7 11 shows the aircraft on the assigned heading of 240 TERM Terminal is the current CDI flight phase displayed on the HSI indicating 1 0 nm CDI scaling FPL ACTIVE FLIGHT PLAN 136 975 NORTH UP ACTIVE FLIGHT PLAN TFR KMKC KCOS NO DATA DTK DE Deporture KMKC ALL TIFTO2 TIFTO MCI TIFTC 287 i ee Enroute SLN 240 Airvoy V244 LAA Fas Vd Airway V263 TBE TBE 218 Arrivol KCOS TBE DBRY1 ALL CURRENT VNV PROFILE ACTIVE VNV WPT SN E aaa VS TGT FPH FPA TERRAIN VS REQ FPM TIME TO TOD V DEV _FT 1006r1 1000rr E JAn TONGOL VNV 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 Eisa ilai pt ACTIVE FL GHT PLAN TFR KMEC 7 KDOS HI DATA DTK ps Deporture KHKC ALL TIFTOATIFTO MCI TIFTO 2a 576W Enroute SLN 240 fa Airway V244 LAA aR KANSAS CITY HYS Wr IL INA F LAA 251 Cs F Ti Airwoy Y263 TBE TBE 210 F i iw Arrival KCOS TBE DBRY 1 ALL CURRENT WW PROFILE ACTIVE Wi WPT FT at VS TGT VS REQ V DEV 100r g TERAATH Figure 7 12 Assigned Heading of 290 7 6 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 7 NAVIGATION 4 V4 will now be entered
119. equencies 0 c cccccceseeeeeen 1 28 7 15 Nearest Airspace ccs 7 29 SECTION 8 FLIGHT PLANNING 00000 8 1 8 1 User Defined Waypoints 5515151111111111112 8 1 Select the User WPT Information Page scseseseeen 8 1 Create User Waypoints from the Navigation Map Page 8 1 8 2 Viewing the Active Flight Plan 8 2 8 3 Activate a Stored Flight Plan 8 2 8 4 Activate a Flight Plan Leg 8 2 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan ee 8 3 8 7 Create a New Flight Plamn 0 8 3 Create a New Flight Plan Using the MFD uu 8 3 Create a New Flight Plan Using the PFD uu 8 4 8 8 Enter an Airway in a Flight Plan 8 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 9 Load a Departure occ 8 6 8 10 Load an Arrival 8 6 8 11 Load an Approach ou cscs 8 6 8 12 Remove a Departure Arrival Approach or Airway from a Flight Plan 0 ccc 8 6 8 13 Store a Flight Plamen 8 6 8 14 Edit a Stored Flight Plan ees 8 6 8 15 Delete a Waypoint from the Flight Plan 8 7 8 16 Invert and Activate a Stored Flight Plan 8 7 8 17 Copy a Flight Plann 8 7 8 18 Delete a Flight Plann cee 8 7 8 19 Graphical Flight Plan Creation 8 8 8 20 Trip Planning 8 8 SECTION 9 PROCEDURES 00 oo
120. ertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on the indicator In Vertical Speed Mode the flight director acquires and maintains a Vertical Speed Reference Current aircraft vertical speed to the nearest 100 fpm becomes the Vertical Speed Reference at the moment of Vertical Speed Mode activation Vertical Speed Mode does not consider the relative position of the Selected Altitude in relation to the current aircraft altitude at the time of mode activation so it is possible to use Vertical Speed Mode while not climbing descending to the Selected Altitude 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 7 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Speed ae Selected ses one Mode Active Rejeven P Mode Arme Selected Altitude Vertical Speed Reference Command Bars _ i 2 Em TEE sen Vertical Speed Indicate Climb 110 Ee Reference Bug to Attain Vertical Speed 100 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 and above below the Vertical Speed Indicator flight director continuously monitors Selected Altitude a be changed by airspeed and altitude This mode acquires and maintains Using the NOSE UP NOSE DN Keys the Airspeed
121. estination altitude constraint and course Canceling Direct to Navigation 1 2 3 Press the Direct to E Key Press the MENU Key to display the Direct to options menu With Cancel Direct To NAV highlighted press the ENT Key If a flight plan is still active the G1000 resumes navigating the flight plan along the closest leg PAGE MENU OPTIONS Concel Direct To NAV Clear 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 ae ie WPT Location Facility Name 3 VNV Target Altitude aaa OFFSET 5MM Offset Distance Bearing to WPT GAIA DIS 1074N4 Distance from WE Course to Selected WPT HR ACTIVATE Figure 7 7 PFD Direct to Window Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 contraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the VNV altitude fiel
122. ex 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 00567 01 Rev B 2006 2007 Garmin Ltd or its subsidiaries
123. ey AIRPORT KTSD P PUBLIC HEH CENTURY ADRCENTER OLATHE KS DEPARTURE HIEF3 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 ENT Key A list of available transitions is displayed for the departure Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key 9 SECTION 9 PROCEDURES DEPARTURE CHIEFS RUNWAY ALL TRANSITION CATTS Figure 9 2 Select Departure Transition With LOAD highlighted press the ENT Key The departure will be active when the flight plan is active Load and Activate An Arrival Procedure 5 6 NOTE If any portion of an arrival procedure is the active leg of a flight plan the existing arrival procedure must be deleted before changing to a different arrival procedure Press the PROC Key Turn the large FMS Knob to highlight SELECT ARRIVAL Press the ENT Key If a flight plan is active the destination airport will be 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
124. 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 will declutter when the aircraft enters an unusual attitude Only the basic primary functions will be displayed in these situations 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 will be 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 GP
125. fficient GPS signal is re established System Test pass Nme TAWS System Test OK 10 16 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 Normal PFD Display The DISPLAY BACKUP Button Activates Deactivates Reversionary Mode on Both Displays SECTION 11 ABNORMAL OPERATION Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display problem The reversionary mode is activated manually by pressing the red DISPLAY BACKUP button on the bottom of the audio panel GMA 1347 Pressing the red DISPLAY BACKUP button again deactivates reversionary mode A NOTE The Cessna 350 400 Airplane Flight Manual AFM always takes precedence over the information found in this section Normal MFD Display NAVI and COMI provided by the failed PFD Flagged Invalid Figure 11 1 G1000 Reversionary Mode Failed PFD 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 11 ABNORMAL OPERATION 11 2 ABNORMAL COM OPERATION When a COM tuning
126. gation 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 or Traffic group to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page PAGE HENU OPTIONS Measure Bearing Distance Press the FMS CRSA knob to return to bose poge Figure 10 1 Page Menu HAP SETUP STRHSCP LTMG 4 n STRHSCP HODE Ce STRHSCP SHEL SD0NH HEMRAD DATA OFF 2Q 0NH MH LTNG OFF 200ANH CELL MOVEHENT 4 n Figure 10 2 Map Setup Menu MAP SETUP 1SQNH SANM Figure 10 3 Map Setup Group List SECTION 10 HAZARD 10 2 STORMSCOPE OPTIONAL 350 ONLY 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 Select the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page RAY I GAT LUN MAP IVE RLAHD PAHE HELLY Figure 10 4 In Flight Navigation Map Page Displaying Stormscope Lightning Data 190 00567 01 Rev B Garmin G1000 Cockpit R
127. gation 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 e Vectors to Final is activated 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 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 00567 01 Rev B 6 4 AUTOPILOT OPERATION NOTE Refer to the AFM for specific instructions regarding emergency procedures The autopilot operates flight control surface servos to provide automatic flight control Pitch and roll com mands are provided to the servos based on the active flight director modes The autopilot uses pitch and roll rates to stabilize the aircraft attitude during upsets and flight director maneuvers Flight director commands are rate and attitude limited combined with pitch and roll damper control and sent to the pitch and roll servo mo tors Pitch autotrim provides trim commands to the pitch trim servo to relieve any sustained effort required by the pitch servo The pitch servo meas
128. gen Outlet Gauge ell 37 6 5 44 gel OUTLET Pressure Gauge GAL USED RANGE NM Fuel 17 0 L FUEL QTY GAL R FUEL QTY GAL 0 4 o Electrical oa tall a ELECTRICAL Group me 10 1612 1437 a ee ALT AMPS BATT AMPS BUS VOLTS 1900 500 p ving Een imate uo At Trim Grou 1450 P roup 3 2 1300 1158 1000 mE A eS Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1 Z3 49 CO LVL HIGH PPM Figure 3 2 EIS Display Cessna 400 shown AILERON TRIM 190 00567 01 Rev B SECTION 3 ENGINE INDICATION SYSTEM EIS 3 22 ENGINE LEANING ASSIST DISPLAY 3 Lean the mixture until one of the cylinder s exhuast temperature peaks This is indicated by 1st being Engine Leaning for the Cessna 350 displayed below the first cylinder to peak A bar is also displayed at that point on that cylinders bar NOTE The Cessna 350 Airplane Flight Manual graph See Figure 3 3 AFM supersedes information found in this 4 Richen the mixture until the PEAK temperature is section rich by the amount indicated in the Cessna Airplane rr Flight Manual AFM Leaning for Best Power 1 Select the SYSTEM Softkey 2 Select the ASSIST Softkey Indicates Difference Between Present and Peak Temperature of the First Peaked Cylinder FFLOW GPH f TEMPERATURE x EGT F CHT F 1442 1452 1382 4 pea 394 378 380 1900 1750 1600 1414 1416 1374 6 sap 274 382 358 1950 1300 1150 1000 Figure 3
129. ght director is activated the FD Key is When operating in Pitch Hold Mode the pitch pressed Pitch Hold Mode is selected by default Pitch reference can be adjusted by Hold Mode is indicated as the active pitch mode by the e Using the NOSE UP NOSE DN Keys green annunciation PIT This mode may be used for e Pressing the CWS Button hand flying the aircraft climb or descent to the Selected Altitude shown above to establish a new pitch reference then releasing the Altimeter since Selected Altitude Capture Mode is the CWS Button automatically armed when the mode is activated In Pitch Hold Mode the flight director maintains a constant pitch attitude the pitch reference The pitch reference is set to the aircraft attitude at the moment of mode selection If the aircraft pitch attitude exceeds the flight director pitch command limitations the flight director commands a pitch angle equal to the nose up down limit Dich Hold Mode Active Selected Altitude Capture Mode Armed navi 108 08 117 95 KHCI 10 4nn bao O58 36 975 118 888 com navz 108 00 117 95 ROL PIT ALTS 136 975 118 000 cone a E Selected 13006 i Altitude mel 1 1 13100 7 wm Command Bars 13 on a Maintain Desired ep 12900 Pitch Reference 10 10 ze iji i m Buu 051 ara i af r l A ir TAS 170KT iwi v ii ce 29 9214 Ao gy IF o Di tl p ff _ Ln e 7 1 a dn
130. gnal 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 fora NAV radio a white ID indication appears to the lett of the corresponding active NAV frequency The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel 121 900 118 600 com TX COM2 Figure 4 5 Radio Status Indications 4 2 VOLUME VOLUME is displayed in place of the associated radio name i e COMI or NAV2 for two seconds after the volume level is last changed The percentage of maximum volume is displayed in place of the standby frequency selected by the tuning box COM1 135 675 35 VOLUME 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 190 00567 01 Rev B SECTION 4 NAV COM amp TRANSPONDER 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 FREQUENCY AUTO TUNING Auto tuning on the PFD NEAREST AIRPORTS 124 6 8NM VFR 122 700 RNWY 2440FT 210 10 2NM ILS 123 000 RNWY 5 QQFT 150 11 4NM ILS 133 000 RNWY 7339FT Figure 4
131. he ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan Press the FHS CRSA knob ta return to bose poge Figure 8 8 Invert Flight Plan Invert active flight plan OK or CANCEI Figure 8 9 Invert Flight Plan Confirmation CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1 2 3 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the NEW Softkey to display a blank flight plan page for the first empty storage location STORED FLIGHT PLAN Figure 8 10 Create FPL on MFD Turn the small FMS Knob to display the Waypoint Information Window Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 3 SECTION 8 FLIGHT PLANNING 8 4 4 5 8 Turn the small FMS Knob to the right enter the first character of the identifier of the departure airport Turning the knob to the left will access the FPL NRST and RECENT waypoint list Turn the large FMS Knob to move the cursor to the next character field Repeat steps 4 and 5 until the desired identifier has been entered WAYPOINT IHFORHATION IDENT FACILITY CITY ee candy HORTH UP CEN Ty Figure 8 11 Waypoint Info Window Press the ENT Key Repeat step number 3 4 and 5 to enter the identifier tor each additional flight plan waypoint When all wa
132. hes between volume and squelch adjustment by lighting VOL or SQ respectively fe RELAY ww CREW wv PILOT COPLT ICS_ISOLATION PILOT O PASS VOL Figure 5 8 Volume Squelch Control 5 7 DIGITAL CLEARANCE RECORDER AND PLAYER Fach reception of primary active COM audio is automatically recorded ina memory block When the next transmission is received it is recorded in the next memory block and so on Once the 2 5 minutes of recording time has been reached the recorder begins recording over the stored memory blocks starting from the oldest block Powering off the unit automatically clears all recorded blocks v v MAN SQ PLAY Figure 5 9 Playback e Pressing PLAY once plays the latest recorded memory block then returns to normal operation Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Pressing MKR MUTE 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 will begin 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 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL 6 1 AFCS CONTROLS The following dedicated AFCS keys are located on the bezels of the MFD Aircraft with WAAS Aircraft with non capable system WAAS system Figure 6 1
133. ht Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and both TAWS and Terrain Proximity will be disabled Additionally the accuracy of all nearest information airports airspaces and waypoints will be questionable Finally airspace alerts will continue to function but with degraded accuracy Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 11 3 SECTION 11 ABNORMAL OPERATION Blank Page 11 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 12 ANNUNCIATIONS amp ALERTS NOTE The Airplane Flight Manual supersedes information found in this document System Annunciation Red X Annunciation Window AVIONICS FAN Cooling fan for remote avionics is inoperative Alerts Window TRAFFIC FAIL Traffic device has failed GMA1 FAIL BO Meee EAEN XPDR LCL 6 46 53 Annunciation Figure 12 1 G1000 Alerting System 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 The Annunciation Window is located to the right of the Altimeter and Vertical Speed Indicator on the PFD display or the MFD if system is in Reversionary Mode Up to 12 annunciations can be displayed simultaneously A white horizontal line separates annunciations that are acknowledged 190 005
134. ht 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 8 18 DELETE A FLIGHT PLAN From the Flight Plan Catalog Page press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be deleted Press the DELETE Softkey 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 SECTION 8 FLIGHT PLANNING 8 8 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 will be inserted at the end of the flight plan The default user waypoint naming is USROOO USRO01 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
135. ical LNAV VNAV and LPV Approach CDI Scaling WAAS Systems Only 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 3 11 SECTION 2 FLIGHT INSTRUMENTS 2 12 Distance to Bearing Source Waypoint n Identifier A Bearing Pointer Source Icon Figure 2 27 BRG1 Information Window Distance to Source Waypoint Identifier a oa Icon Source Pointer Figure 2 28 BRG2 Information Window Navigation Source Change CDI navigation sources 1 2 3 Press the CDI Softkey to change from GPS to VOR1 LOC1 Press the CDI Softkey again to change from VOR1 LOC1 to VOR2 LOC2 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 will be required such as VHE LOI is also displayed during GPS position initialization Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 WARN GPS detects a position error 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
136. ide is displayed SECTION 7 NAVIGATION View Additional Details for a Listed Airspace 1 2 3 4 5 With the Nearest Airspace Page displayed press the FMS Knob to activate the cursor Turn either FMS Knob to scroll through the list highlighting the desired airspace Press the ALERTS Softkey to place the cursor in the AIRSPACE ALERTS field Turn either FMS Knob to select the desired airspace Press the FMS Knob to remove the flashing cursor View and Quickly Load the Frequency for a Controlling Agency 1 2 3 4 With the Nearest Airspace Page displayed press the FREQ Softkey to place the cursor in FREQUENCIES field Turn either FMS Knob to select the desired frequency Press the ENT Key to load the frequency into the COM frequency standby field Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1 29 SECTION 7 NAVIGATION Blank Page 7 30 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 8 FLIGHT PLANNING The following discussions pertain to the Multi Function Display unless otherwise indicated 8 1 USER DEFINED WAYPOINTS WORTH UF 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
137. ied by an annunciation and a pop up terrain alert on the display 190 00567 01 Rev B SECTION 10 HAZARD T eb D S 8 DON T SINK lt D 0b E a I 0 20 40 60 80 100 120 140 Altitude Loss Feet 1000 i gt 20 D S 5 DON T SINK D cb I 0 500 1000 1500 2000 2500 3000 3500 4000 Sink Rate Feet Per Minute Figure 10 20 Negative Climb Rate Five Hundred Aural Alert The purpose of the aural alert message Five hundred is to provide an advisory alert to the pilot that the aircraft is five hundred feet above terrain When the 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 message Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 10 13 SECTION 10 HAZARD AVOIDANCE Pop up Alerts Alert Annunciations Dia When the Navigation Map Page is displayed and a terrain or obstacle alert is issued a pop up window is displayed with the a alert NAVIGATION MAP 118 000 11 CoH C NORTH LIP TFA TERRAIN 100r jel 1000er M TERRAIN ALERT SARAS Alert Annunciation p 2 ari Press ENT TAWS PAGE s i EX cab a ao Figure 10 24 Alert Annunciation on the TAWS Page Alert Annunciation Figure 10 22
138. ies 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 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists MFD1 DB ERR MFD1 Safetaxi database error exists PFD1 DB ERR PFD1 SafeTaxi database error exists MFD1 DB ERR MFD1 Chartview database error exists MFD1 DB ERR MFD1 FliteCharts database error exists 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced The MFD and or PFD detected a failure in the basemap database The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the G1000 system should be serviced The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Re
139. iguration Softkeys PFD Press to display the additional softkeys for additional configuration of the PFD DFLTS Press to reset detault settings on the PFD WIND Displays softkeys to select wind data parameters OPTN I Longitudinal and lateral components OPTN 2 Total direction and speed OPTN 3 Total direction with headwind and crosswind speed components OFF Information not displayed 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 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 GPS Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window OFF Removes the BRG2 Information Window
140. ilable Telephone Unavailable Speaker Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio DME ADF amp AUX unavailable Manual Squelch S TN Recorded COM Audio Playback CREW w PILOT sn i ICS Isolation ICS ISOLATION PILOT O PASS VOL SQ Volume Squelch VOL Annunciation SQ Annunciation Reversionary Mode DISPLAY BACKUP Figure 5 1 Audio Panel Controls 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 SPLIT COM FUNCTION NOTE Split COM performance is affected by the distance between the antennas and the separa tion of the tuned frequencies Figure 5 3 Split COM Function Pressing the COM 1 2 Key selects and deselects the split COM function During split COM operation the COMI COMI MIC COM2 and COM2 MIC Keys are active When the COM 1 2 Key is selected COM1 is used by the pilot for transmission and COM2 is used by the copilot The COMI MIC annunciator blinks when the pilo
141. ing Bug movement even if the bug is turned more Key Heading Select Mode acquires and maintains the than 180 from the present heading e g a 270 turn to Selected Heading The Selected Heading is shown by a the right However Selected Heading changes of more light blue bug on the HSI and in the box to the upper left than 340 at a time result in turn reversals of the HSI Heading Select Mode is activated by pressing HDG Changing the Selected Heading NOTE Pressing the HDG Knob synchronizes the Selected Heading to the current heading The Selected Heading is adjusted using the HDG Knob on either display Pressing the CWS Button and hand flying the aircraft does not change the Selected Heading The autopilot guides the aircraft back to the Selected Heading upon release of the CWS Button Heading Select Mode Active Pitch Hold Mode Active nev 111 98 114 10 TETT 118 200 136 975 com 3 81 eS T au 136 975 118 000 conz Command Bars Track Selected Heading Selected Heading Selected Heading Bug OAT 7 FIISA 21 F Oe xPDR1 GARD RILCL 011550 Figure 6 21 Heading Select Mode 6 18 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B Navigation Mode GPS VOR LOC BC 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 Navigation Mod
142. ing function The target pointer is displayed at the present aircraft position 2 Move the Joystick to place the pointer at the desired position Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 8 FLIGHT PLANNING 8 2 3 4 5 6 1 8 2 Press the ENT Key The User Waypoint Information Page is now displayed with the captured position Turn the FMS Knobs to select a waypoint name Press the ENT Key to accept the selected name The first reference waypoint field is highlighted It desired turn the FMS Knobs to enter the identitier of the reference waypoint and the radial and distance to the reference waypoint Press the ENT Key to accept Press the FMS Knob to remove the flashing cursor or press the GO BACK Softkey to return to the map VIEWING THE ACTIVE FLIGHT PLAN Press the FPL Key DIK DIS Is Approoch ILS 30R pon Ane O0DS iof 12 Figure 8 3 Active Flight Plan Page on the MFD Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 3 1 2 3 4 8 4 1 ACTIVATE A STORED FLIGHT PLAN Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Figure 8 4 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 ACTIVE Softkey With OK highlighted press the ENT Key to activate the flight plan To cancel the flight
143. into the flight plan ee a Press the FMS Knob to activate the cursor ers b Turn the large FMS Knob to highlight the desired eevee es 2 entry point as shown in Figure 7 13 The V4 entry ree NORTH UF will be placed immediately above the highlighted waypoint ACTIVE FLIGHT PLAN KMKC KEUS OTK DIS Departure KMKC ALL TIFTO2 1TIFTO MCI TIFTO 266 5SQ 2NH FT Enroute SLM Ck FT Airwoy W244 LAA HYS 262 TLI ___FT LAA fol TGSI Airvay V 263 1BE TBE 217 LAM LOCATION ERG B20 N 39 08 23 DIS 22 9NH ppo 90 Press ENT to accept Figure 7 14 Entering V4 Entry Point d Press the ENT Key TOP is now inserted into the CURRENT VNU PROFILE flight plan as in Figure 7 15 VS TOT VS REG KEOS J22 TBNH ACTIVE FLIGHT PLAN KMEC KOOS Figure 7 13 Begin Adding V4 to the Flight Plan a Ss pee Enroute g TOP 146 32 3NH c Turn the small FMS Knob to display the Waypoint EEM 260 97 7 Information Window Enter the desired beginning jaia ii E E point for V4 leg in this example Topeka VOR LAA 165 TOP will be used as shown in Figure 7 14 aa Gla i n A KCOS dez TIBBNH _ FT CURRENT WNW PROFILE ACTIVE WNW WPT By Oe ee WS TGT FP FPA VS REU O FPA TIME TO TOD Figure 7 15 TOP Inserted into the Flight Plan e With SLN still highlighted as in Figure 7 15 turn the small FMS Knob to the right The Waypoint Informatio
144. ion NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B RECORD OF REVISIONS Part Number Change Summary 190 00567 00 RevA Production release Rev B Added C350 parameters TAWS changes and Stormscope 190 00567 01 Rev A Added GDU 8 10 parameters WAAS VNAV Airways and Charts Revision Date of Revision Affected Pages P 12 07 Changed Columbia references to Cessna 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 RR 1 RECORD OF REVISIONS Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 1 SYSTEM OVERVIEW 000000 00000 1 1 1 1 PFD MFD Controls 0 00 0 0 ccc 1 2 1 2 GCU 476 Controls cscs 1 5 1 3 PFD SOTKOVS iissiisssssrincaoconvorncionnascmasasen 1 7 1 4 MFD Softkeys occas 1 10 1 5 MFD Page Groups 0 ccc cece 1 11 1 6 Vertical Navigation 0 0 c cece 1 12 1 7 Backlighting 0 0 0 cccccccs estes tesserae 1 14 1 8 Database Updates seen 1 14 Jeppesen Aviation Database 1 14 Gali Data aSeS icvaccisdot deatannsceohexttorsenanenbasticns 1 15 SECTION 2 FLIGHT INSTRUMENTS 00000 2 1 2 1 Airspeed Indicator 2 3 Speed INGICATION ssi A 2 3 Speed RME aa a O 2 3 Airspeed Trend VeCtor sssssessessecssessessseesecsesseeaseesees 2 3 Vspeed Referentes co
145. ion If the problem persists NAV RMT XFR NAV2 remote the G1000 system should be serviced transfer key is stuck S E PAE I O RRE A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 G S2 FAIL G S2 is inoperative system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver G S2 SERVICE G S2 needs service may still be available The G1000 system should be serviced when possible Return unit for repair 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 G
146. ion airport and ends when the aircratt is either 0 5 nm from the runway threshold OR is at an altitude of 125 feet AGL while within 1 nm of the threshold During the final descent algorithms will set a threshold for alerting based on speed distance and other parameters Height Above Terrain Feet 12 13 14 15 unwa 1 2 3 4 5 6 7 8 9 10 11 h 7 z Distance From Destination Airport nm Figure 10 18 PDA Alerting 190 00567 01 Rev B Excessive Descent Rate Alert EDR The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing descending upon terrain at an excessive speed Figure 10 19 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 6000 5500 5000 4500 4000 3500 3000 2500 2000 Height Above Terrain Feet 1500 1000 PU LL UP 2000 4000 6000 8000 10000 12000 Descent Rate Figure 10 19 Excessive Descent Rate Negative Climb Rate After Takeoff Alert NCR The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the pilot when the system determines that the aircraft is losing altitude closing upon terrain after takeoff The aural message Don t Sink is given for NCR alerts accompan
147. ion provides information ADVISORIES regarding G1000 message advisories that may be displayed by the system Knowledge of the This section describes various G1000 system message aircraft systems flight conditions and other advisories Certain messages are issued due to an LRU existing operational priorities must be considered when responding to a message Always use sound pilot judgment The Cessna 350 400 Airplane Flight Manual AFM takes precedence over any conflicting guidance found in this section 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 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 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 softwa
148. it Reference Guide for the Cessna 350 400 NEAREST INTERSECTIONS Figure 7 62 Nearest Intersections Page Select the Nearest Intersections Page 1 2 Turn the large FMS Knob on the MFD 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 cursor Turn either FMS Knob to select the desired intersection Press the FMS Knob to remove the flashing cursor 190 00567 01 Rev B NEAREST NDB Figure 7 63 Nearest NDB Page Select the Nearest NDB Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the third rectangular page icon Access Information on a Specific NDB 1 With the Nearest NDB Page displayed press the FMS Knob to activate the cursor 2 Turn either FMS Knob to select the desired NDB The remaining information on the Nearest NDB Page pertains to the selected NDB 3 Press the FMS Knob to remove the flashing cursor 190 00567 01 Rev B SECTION 7 NAVIGATION NEAREST VO NRT m Ta HOATH LIP j ere 7 aa ra GA a Figure 7 64 Nearest VOR Page Select the Nearest VOR Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fourth rectangular page icon View Information
149. ite Code Number and XPDR 6543 STBY ENT BACK I ALERTS A Figure 4 9 Standby Mode Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 R LCL 00 12 25 Figure 4 10 ON Mode Altitude Mode Automatic or Manual Altitude Mode is automatically selected when the air craft becomes airborne Altitude Mode may also be se lected manually by pressing the ALT Softkey All transponder replies requesting altitude information are provided with pressure altitude information _ ALT Mode Mode C Altitude Reporting ML m rs Figure 4 11 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 12 Reply Indication 190 00567 01 Rev B SECTION 4 NAV COM amp TRANSPONDER Code Selection 5 Turn the small FMS Knob to enter the second two digits VFR Code Selection 6 Press the ENT Key to activate the code immediately 1 Press the XPDR Softkey to display the transponder or wait 10 seconds and the code will become Mode Selection softkeys active 2 Press the VFR Softkey to enter the VFR code Pressing the VFR Softkey again restores the previous identification code NOTE The pre programmed VFR Code is
150. itude 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 cisaaf Cross AT or BELOW 3 000 ft ae ed ei Pe i i Figure 1 10 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 9 VNAV Altitudes Bar vaio further illustrates vertical navigation in more etall 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1 13 SECTION 1 SYSTEM OVERVIEW 1 7 BACKLIGHTING y When system power is turned off all manual backlighting settings will return to the factory default settings Manually adjust the backlight for the PFD and MFD 1 4 5 6 Press the MENU Key on the PFD to display the PFD Setup Menu Window Press the small FMS Knob to activate the cursor PFD DSPL gt AUTO is now highlighted Turn the small FMS Knob to display the selection window Turn the FMS Knob to select MANUAL then press the ENT Key With the intensity value now highlighted turn the small FMS Knob to select the desired backlighting Turn the large FMS Knob to highlight MFD DSPL gt AUTO and repeat steps 3 through 5 PFD SETUP MENU AUTO AUTO 23 474 wet PFD DSPL gt MFD DSPL
151. l Up Obstacle Ahead Pull Up Imminent Obstacle Impact Warning 101 PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up OF or Obstacle Obstacle Pull Up Pull Up Reduced Required Terrain Clearance Caution AUTION TERRAIN Caution Terrain Caution Terrain Aural Message RTC or ERRAIN A Terrain Ahead Terrain Ahead Imminent Terrain Impact Caution ITI Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Reduced Required Obstacle Clearance UTIOI ACL Caution Obstacle Caution Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead Imminent Obstacle Impact Caution IOI Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Premature Descent Alert Caution PDA Altitude Callout 500 Five Hundred Excessive Descent Rate Caution EDR TERRAIN see o Sink Rate Negative Climb Rate Caution NCR DONT SINK Don t Sink or or TOOLOW TERRAIN Too Low Terrain 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 10 15 SECTION 10 HAZARD AVOIDANCE The following system status annunciations may also be issued PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert TAWS System Test Fail TAWS FAIL TAWS System Failure Aural Message No GPS position or excessively degraded TAWS N A None TAWS Not Available GPS signal TAWS Availble will be heard when su
152. layed in the Traffic Mode field 3 Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by selecting the the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Non Bearing Traffic system Proximity Traffic is unable to determine bearing 1000 above amp 4 Select the MUTE Softkey to mute aural alerts for stance is 8 0 nm 1190 above descending a and descending currently displayed Traffic Advisories Aural alerts will again be heard when a new Traffic Advisory is issued Selecting the MUTE Softkey twice will replay the aural alerts for any currently displayed Traffic Figure 10 12 Traffic Map Page Displaying Traffic on the Navigation Map Advisories 1 Ensure the TAS system is operating With the 5 Rotate the Joystick clockwise to display a larger Navigation Map displayed select the MAP area or rotate counter clockwise to display a smaller Softkey area 2 Select the TRAFFIC Softkey Traffic will now be displayed on the map 10 8 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 10 HAZARD AVOIDANCE Traffic Advisory 4 Rotate the Joystick clockwise to display a larger Wp NAVIGATION HAP 118 008 co area or rotate counter clockwise to display a smaller area 136 975 Fy ATRHAYS STRMSCP Non Bearing Traffic Off Scale Non Threat Traffic Advisories ieee Tr
153. lds the Selected Altitude shown as the Altitude Reference As Altitude Hold Mode becomes active the white ALT annunciation moves to the active pitch mode field and flashes green for ten seconds to indicate the automatic transition Altitude Reference In This Case Equal to Selected Altitude 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 350 400 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 aircraft altitude to the nearest ten feet as the Altitude Reference The flight directors Altitude Reference is shown in the AFCS Status Box and is independent of the Selected Altitude displayed above the Altimeter Altitude Hold Mode active is indicated by a green ALT annunciation in the AFCS Status Box Altitude Hold Mode is automatically armed when the flight director is in Selected Altitude Capture Mode Selected Altitude Capture Mode automatically transitions to Altitude
154. leasing the CWS Button to establish the new Airspeed Reference Flight Level Change Airspeed Altitude Hold Mode Active Reference Mode Armed DIS HRG 136 975 Airspeed Reference I OT ee ei oe E 500 Toe ea A af J 3100 Canpa i E esm Airspeed Reference Bug J a i 2380 a by egoa 2708 PRAR ZERA OAT TTFIISA 2TF R LCL 06 2916 Figure 6 9 Flight Level Change Mode 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 GPS Navigation Section for more information on VNAV flight plans The flight director may be armed for VNAV at any time but no target altitudes are captured during a climb The Command Bars provide vertical profile guidance based o
155. light continues through the arrival procedure to PYNON see Figure 7 42 At a point 31 nautical miles from the destination airport the phase of flight scaling for the CDI will change 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 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 7 NAVIGATION Turn right to 021 in 9 seconds Esiin Aa e ee ene 136 975 136 975 FPL ACTIVE FLIGHT PLAN THARRON HILLS Bt A aie ACTIVE FLIGHT PLAN GoLoreptL SPRINGS TFR KMKC KCOS KCGS NO DATA Ej EGA o OmK OIS AT RS TEE SESSA KATES F Arrival KCOS TBE DBRY 1 ALL GPSHN gt SNH OPSHN FSHER e L PYNON 352 0 7mm 10000FT Approach KCOS RNAV SSRors LPY HABUK iaf Sra 5 3Nn s000 FALUR 261 CONH 8600 CEGIX fof 1 G NH sal RHSSR aap 351 SINH CURRENT VNV PROFILE ACTIVE UNV WPT 9000FT ot HABUK lof VS TOGT 7S6FPH FPA 25 1 Q a OT 2057 In VS REQ 471FPnh TIME TOTOO 005 f v Dev 7S FT 100r1 1000r1 M 7 v61 m SBne VIEW VNV PROF CNCL VNV VNV amp 136 975 Es CY 186 975 Figure 7 42 Approaching PYNON Jel SECTION 7 NAVIGATION 21 Upon passing PYNON the approach procedure will 22 The IAF is the next waypoint
156. ltitude hold 1 4 Altitude Hold Mode 6 6 Altitude Reference 6 6 6 13 Altitude restrictions 1 13 Altitude trend vector 2 4 ALT Knob 1 4 Annunciations 12 1 Annunciation Window 2 2 AP 1 4 6 1 Approach ILS 6 30 Missed 6 32 WAAS 6 31 190 00567 01 Rev B Approaches 9 2 Approach activation 4 3 Approach markers Signal augmentation 5 3 Approach Mode 6 20 6 30 Approach Mode AFCS 6 31 AP disconnect 6 1 Arc HSI 2 9 Arrivals 9 1 Attitude Indicator 2 1 Attitude indicator 2 4 Audio alerting system 12 2 Audio panel 4 3 5 1 Audio panel controls COM 1 2 5 2 Auto tuning 4 3 Automatic Flight Control System AFCS Alerts and annunciations 6 33 6 34 Status Annunciations 6 33 Status Box 6 2 Automatic squelch 4 3 Autopilot 6 1 6 21 6 22 Autopilot disconnect 6 16 6 22 Barometric minimum 2 8 Barometric minimum descent altitude 2 2 Barometric setting Altimeter 2 1 Base reflectivity 10 4 Bearing Information Windows 2 2 BRG1 2 11 BRG2 2 11 C Carbon monoxide 3 2 Caution 12 1 12 2 CDI 2 10 2 12 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 Coast mode 10 7 Code selection 4 4 4 5 Command Bars flight director 6 2 Communication COM Frequency Box 2 1 COM Frequency Window 4 1 COM knob 4 3 Controls 1 2 4 1 Control Wheel Steering 6 1 Control Wheel Steering CWS 6 21 Create a new user waypoint 8 1 CWS 6 1 CWS Button 6 5 6 10 6
157. lure lms Obese AP and MEPT 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 servos Preflight Test 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 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 12 5 SECTION 12 ANNUNCIATIONS amp ALERTS 12 5 TAWS ALERTS Annunciations appear on the PFD and MFD Pop up alerts appear only on the MFD PFD MFD TAWS Alert Type Page MEE ep age bie Pop Up Alert Annunciation Excessive Descent Rate Warning EDR PULL UP Pull Up Reduced Required Terrain Clearance Warn PULL UP Terrain Terrain Pull Up Pull Up ing 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 PULL UP Obstacle Obstacle
158. moved from the display Lastly but at the same time a GPS NAV LOST alert message will appear on the PFD Normal navigation using GPS WAAS source data will resume automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of accurately tracking your estimated position and consequently the system may display a path that is different than the actual movement of the aircratt Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation 190 00567 01 Rev B SECTION 11 ABNORMAL OPERATION 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 will be computed based upon an estimated position and will be 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 Flig
159. n Overspeed protection is provided in situations where the flight director cannot acquire and maintain the mode reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed When an autopilot overspeed condition occurs the Airspeed Reference appears in a box above the Airspeed Indicator flashing a yellow MAXSPD annunciation Engine power should be reduced and or the pitch reference adjusted to slow the aircraft The annunciation disappears when the overspeed condition is resolved Airspeed Indicator Figure 6 40 Overspeed Annunciation Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 7 NAVIGATION SECTION 7 NAVIGATION 7 2 DIRECT TO NAVIGATION Direct to Navigation from the MFD The following discussions pertain to the Multi Function Display unless otherwise indicated I dentifier IDENT cece Geograp hic 7 1 NAVIGATION MAP PAGE a KHIA 4 SE USA Region acility Name MIAMI INTL a City Senai VNV Altitude WARNING The map display should only be uw Offset Bejore Selected N i VNV S00 GLM Direct t A used for situational awareness Any map display Target Altitude o indication should be compared with approved NIU oe Map Orientation navigation sources Map of the me S PE Selected ap kaTa aS I Select the MAP Page Group oponi M awe f pi 1 Turn the large FMS Knob until MAP is highlighted ee m in the page group box in the
160. n Page is displayed and the LD AIRWY Softkey is now available 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 7 NAVIGATION 1 8 f Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7 16 ENTRY TOF mae AN LOAD Figure 7 16 List of Available Airways for TOP 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 points is now displayed as in Figure 7 17 Figure 7 17 List of Available Exits for V4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 18 260 97 71M Figure 7 18 Ready to Load V4 k Press the ENT Key V4 is now loaded into the flight plan as shown in Figure 7 19 190 00567 01 Rev B ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS Departure KMKC ALL TIFTO2 TIFTO MCI f TIFTO 286 46 9NM Enroute TOP 146 323mm Airway V4 SLN SLN 260 97 7N Airway V244 LAA HYS t AI aaa LAA 251 Airway 263 TBE CURRENT VNV PROFILE ACTIVE VNU WPT VS TGT FPM FPA VO REM passes FPM TIME TO TOO Figure 7 19 V4 is Loaded in the Flight Plan 5
161. n in both displays type mismatch terrain database type in both displays version mismatch correct obstacle database version in both displays database mismatch correct airport terrain database in both displays GMA 1347 Message Advisories Message 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 sottware 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 PAY Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B GIA 63 Message Advisories SECTION 12 ANNUNCIATIONS amp ALERTS Message Comments o GIA1 CONFIG GIA1 contig error Contig service req d GIA2 CONFIG GIA2 contig error Contig service req d GIA1 CONFIG GIA1 audio contig error Contig service req d GIA2 CONFIG GIA2 audio contig error Contig service req d GIA1 COOLING GIA1 temperature to
162. n 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 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 fa PS ALT 3000er VPI Akt ALTS GP V Figure 6 10 Vertical Path Tracking Armed Annunciations Prior to descent path interception the Selected Altitude must be set below the current aircraft altitude by at least 75 ft For the flight director to transition from Altitude Hold to Vertical Path Tracking Mode acknowledgment is required within five min
163. nable or pressed position Press the PTT switch again to cycle its operation ca COM2 push to talk key it the problem persists the G1000 system should be serviced COM1 RMT XFR COM1 remote transter key is stuck COM2 RMT XFR COM2 remote transter key is stuck LOI GPS integrity lost Crosscheck a SE with other NAVS GPS integrity is insufficient for the current phase of flight at oe D o j oe Loss of GPS navigation due to insufficient satellites navigation Insufficient satellites ae Ay eaa B es Loss of GPS navigation due to position error navigation Position error ne mel ar i oa 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 will operate at reduced power 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 Leo Or a Do Abort approach due to loss of GPS navigation Abort approach PR DATORA DE A PIA 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 00567 0
164. 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 At 50 feet from the Selected Altitude the green ALT annunciation flashes for up to 10 seconds the autopilot transitions to Altitude Hold Mode and levels the aircraft ALT Selected Altitude of 12 000 MSL ALT Mode Figure 6 30 Departure Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial d Press the NAV Key This arms VOR Navigation Mode and the white VOR annunciation appears During climb out the autopilot continues to fly the to the left of the active lateral mode aircraft in Heading Select Mode Airway V4 to Salina VOR SLN should now be intercepted Since the MOO enroute flight plan waypoints correspond to VORs flight director Navigation Mode using either VOR or GPS as the o 2 Once the flight director calculates the proper navigation source may be used In this scenario VOR capture point the flight director transitions trom Navigation Mode is used for navigation to the first VOR Heading Select to VOR Navigation Mode and the waypoint in the flight plan VOR annunciation flashes green The autopilot Intercepting a VOR radial begins turning to intercept the Selected Course 1 Arm VOR Navigation Mode J VOR AP ALT 12000r7 a Tun
165. ng the autopilot Pressing and holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the aircraft to be hand flown At the same time the flight director is synchronized to the aircraft attitude during the 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 a ROL ICHS PIT ALTS Figure 6 26 CWS Annunciation Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 22 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 Oe ALTS Figure 6 27 Automatic Autopilot Disengagement 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 two second autopilot
166. ngs for Tornado Severe Thunderstorm and Flood conditions provided by the National Weather Service NWS The display is updated every 5 minutes 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 10 5 SECTION 10 HAZARD AVOIDANCE m Echo Top Cloud Top and Echo Top va Exclusive ct ae Sh FT ae Ve MY Figure 10 10 Weather Product aaa e City Forecast Surface Analysis Weather Product Expires After e Freezing Levels e Winds Aloft SIGMETS AIRMETS County Warnings a e Cyclone Warnings County Warnings o ee The XM Information Page in the AUX Page Group will _Liclone Warnings o O display the weather products available for the current Echo Tops subscription A green box by the weather product means Freezing Levels o o that it is available METARs a A NOTE The DONE Softkey on the AUX XM_ _Lghtning INFORMATION Page is used to save the GDL NEXRAD 69 A activation data when the XM services Radar Coverage are initially set up It is not used during normal cimen operation of the GDL 69 A and it should have no adverse effects if inadvertently selected during Surface Analysis O o flight Refer to the GDL 69 69A XM Satellite TERS o o Radio Activation Instructions 190 00355 04 Rev Winds Aloft wooo E or later for further information rs Clouds Tops Oo O Weather Product Age The age for each of the enabled products is displayed on the right side of the display Times are based on Zulu time
167. ning for the Cessna 400 NOTE The Cessna 400 Airplane Flight Manual AFM supersedes information found in this section Leaning for Best Power 1 Select the SYSTEM Softkey 2 Select the ASSIST Softkey 3 Lean the mixture to obtain peak temperature on the TIT displays See Figure 3 5 Refer to the Cessna Airplane Flight Manual AFM for more detailed procedures Indicates Peak TIT Temperature FFLOW GPH TEMPERATURE GT F TIT 1706 1571 1634 1472 wpe 1900 a 1616 1661 a T 1750 1600 1600 1450 1450 poe 1150 1668 1000 z 36 4 TIT Delta Value aras Difference from Peak 190 00567 01 Rev B F 1436 Di LEAN 4 SECTION 3 ENGINE INDICATION SYSTEM EIS Richen the mixture to obtain the desired delta values as specified in the AFM Leaning for Best Economy 4 Select the SYSTEM Softkey Select the ASSIST Softkey Lean the mixture to obtain peak temperature on the TIT displays See Figure 3 5 Refer to the Cessna Airplane Flight Manual AFM for more detailed procedures Continue leaning the mixture until the desired delta D values are obtained as specified in the AFM Selecting the ASSIST Softkey returns the MFD to the EIS Display Selecting the SYSTEM Softkey exits the Assist Display and returns the MFD to default operation h i ry HT F 347 329 334 5 356 365 320 300 200 F 100 4 5 6 Indicates Lean or Rich From Peak Figure 3 5 Engine Leaning Assist Displa
168. nt 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 ACTIVE FLIGHT PLAN NORTH UP a ACTIVE FLIGHT PLAN TFR KMKC KEOS WI DATA PYNON Approach KCOS RAMAV 3 HABUE lof CURRENT WH PROFILE ACTIVE VN WPT __FT at Figure 7 48 Missed Approach Active T Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 7 NAVIGATION 26 The aircraft continues climbing to AT or ABOVE 7 4 AIRPORT INFORMATION 10 000 feet at MOGAL A holding pattern will be established at the MAHP MOGAL as shown in seroma pptee ete 196 975 Figure 7 49 Ey WORTH UP AIRPORT FPL ACTIVE FLIGHT PLAN NORTH UP _ ACTIVE FLIGHT PLAN TFR KMKC KCOS NO DATA DTK E FSHER E E GELT PYNON Se A Approach KCOS RNAV 35Rees LPV HABUK iof FALUR CEGIX fof RH SR aap 6368FT iy fil MOGAL mahp TERRAIN s e fid Figure 7 53 Airport Information Page E 100Ff1 stack pd 1000F Lj HEET CNCL VNV Figure 7 49 Establishing the Holding Pattern Select the Airport Information Page 27 The aircraft maintains 10 000 feet while following 1 Turn the large FMS Knob to select the WPT page the magenta line through the hold as in Figure 7 ger 2 Turn the small FMS Knob to select the first mee E rectangular page icon Initially information for the wa RKC KEOS airport closest
169. ntification to Air Traffic Control ATC BACK Press to return to the previous level softkeys ALERTS Press to display the Alerts Window IDENT Press to provide special aircraft position identification to Air Traffic Control ATC TMR REF Press to display the Timer References Window NRST Press to display the Nearest Airports Window ALERTS Press to display the Alerts Window L jbyser JL f eo i oss f co JE i xor E penr irmerer _ nest acerrs MM sry f on ar f eno ver cove went J Back Jfarerrs SNnNonSonNnnNAnNAnNnANANA DNO Press the BACK Softkey to return to the top level softkeys Lo Woe Woes Woa Wos JE e JE 7 Ji menr JL ekse j Back J acerrs nRnnnnoaniornieenrnientnk sw Press the BACK Softkey to return to the top level softkeys Figure 1 6 XPDR Transponder Softkeys 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 1 1 4 MFD SOFTKEYS y SYSTEM Selecting this softkey makes available the Engine Display functions Refer to the Engine Indication System section MAP Pressing this softkey enables the following softkeys TRAFFIC Pressing this softkey displays removes Traffic on the Navigation Map TOPO Pressing this softkey displays or removes topographic information on the Navigation Map TERRAIN Pressing this softkey displays removes terrain and obstacle data on the Navigation Map return to the default page lev
170. nunciation 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 3 _ GPS AP ALT o m Cruise Altitude of 12 000 MSL 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 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 33 FLC Descent 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 27 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Path Tracking descent to VNV e Turn the ALT Knob to adjust the Selected Target Altitude Altitude 1 Select coupled VNAV e Press the VNV Key a Press the VNV Key to arm Vertical Path Tracking If the descent is not confirmed by the time of Mode The white annunciation VPTH appears interception Vertical Path Tracking Mode remains armed and the descent is not captured GPS
171. o enter the fuel flow Press the ENT Key when finished Note that in automatic page mode fuel flow is provided by the system 8 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 9 The flashing cursor moves to the calibrated airspeed field Turn the FMS Knobs to enter a calibrated airspeed Press the ENT Key when finished 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 9 SECTION 8 FLIGHT PLANNING Blank Page 8 10 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1 2 3 4 5 6 1 8 190 00567 01 Rev B 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 will be 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 K
172. o low GIA2 COOLING GIA2 temperature too low GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP CON2 over temp Reducing transmitter power The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced The system has detected an over temperature condition in COM1 and or COM2 The transmitter will operate at reduced power If the problem persists the G1000 system should be serviced 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 273 SECTION 12 ANNUNCIATIONS amp
173. o 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 these points reappear after the screen has been cleared NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condit
174. ope lightning mode between cell and strike 1 Select the Stormscope Page 2 Select the MODE Softkey The CELL and STRIKE Sottkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells 190 00567 01 Rev B SECTION 10 HAZARD AVOIDANCE Change the viewing mode between 360 and Displaying METAR and TAF information on the 120 Airport Information Page 1 Select the Stormscope Page 2 Select the VIEW Softkey The 360 and ARC Softkeys Display METAR and TAF text on the Airport are displayed Select the 360 Softkey to display Information Page a 360 viewing area or select the ARC Softkey to 1 Turn the large FMS Knob to select the WPT Page display a 120 viewing area Group Select the CLEAR Softkey to remove all Stormscope 2 Turn the small FMS Knob to select the Airport lightning data trom the display Information Page 3 Select the WX Softkey to display METAR and TAF 10 3 XM WEATHER OPTIONAL text METAR and TAF information is updated every 12 minutes WARNING XM Weather is not intended to be used for hazardous weather penetration NORTH UP a repoRt wu EHSF PUBLIC Weather information provide
175. or 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 T ee ALT Mode gt Cruise Altitude of 12 000 MSL e O D lt lt ALT Mode Selected Altitude set below VNAV Target Altitude Along track Offset 3 nm before OPSHN m 3 nm A Figure 6 34 VPTH Descent 6 28 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 altitude 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 _ GPS TAP 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 SECTION 6 AUTOMATIC FLIGHT CONTROL
176. osition with alternate navigation sources TRAFFIC FAIL Traffic device has The G1000 is no longer receiving data from the traffic system The traffic device failed should be serviced i i a i 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 criteria entered by the user 12 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B A Abnormal COM operation 11 2 Activate a flight plan 8 2 Active flight plan 8 2 ADVISORY 12 1 Advisory alerts 12 4 AFCS 1 3 6 1 6 2 6 23 12 5 AFCS Status Box 2 1 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 1 Airspeed indicator 2 3 Airspeed Reference 6 8 Airspeed trend vector 2 3 Airways 8 5 Alerting System 12 1 Alerts 12 1 Alerts Window 2 2 Alert levels 12 2 Alert Pop Up 10 14 ALT 1 4 1 9 6 4 6 6 6 13 7 19 Altimeter 2 1 Altimeter barometric setting 2 1 Altitude alerting 2 5 Altitude constraints 1 12 7 12 A
177. oss at altitudes If the procedure states Expect to cross at then the altitude will not be in the database In this case the altitude may be entered manually NOTE All arrival procedure altitudes contained in the navigation database are for turbojet aircraft only Alter or enter altitudes as desired to comply with the ATC clearance When activating or loading an arrival or approach procedure into an active flight plan the VNV ALT fields will be populated with any altitudes that can be retrieved from the navigation database Since altitudes loaded with an arrival procedure are published only for turbojet aircraft the altitudes are displayed as white text indicating that the altitudes are displayed for reference only An arrival waypoint altitude may be used or designated as is or changed to a different altitude An altitude is designated by pressing the FMS Knob and turning the large FMS Knob to place the cursor on the desired altitude and pressing the ENT Key or Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 entering a different value and pressing the ENT Key The altitude will now be displayed as light blue text indicating that the altitude is now designated to give vertical speed and deviation guidance Approach waypoint altitude constraints are automatically designated for use when the approach is loaded These altitudes will be displayed as light blue text indicating the altitudes will be used
178. ot certified for use in applications requiring a certified terrain awareness system Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually
179. ot displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south A NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Displaying Terrain on the TAWS Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS Page 3 If desired select the VIEW Softkey to access the N ARC and 360 Softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller d rea TERRAIN 100r1 O00e1 Figure 10 17 TAWS Page ARC View 10 10 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 10 HAZARD AVOIDANCE Terrain Obstacle Location Terrain Obstacle above or within 100 below or above aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Potential Impact Point Pah Projected Flight Path ae Unlighted Obstacle Enable Disable Aviation Data TAWS Inhibit 1 While the TAWS Page is displayed press the MENU Flying VFR into an area where unique terrain exists Key could cause the system to annunciate a nuisance alert 7 When TAWS is inhibited only FLTA and PDA alerts are 2
180. place data card If problem persists the G1000 system should be serviced 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 The MFD and or PFD detected a failure in the SafeTaxi database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced The MFD and or PFD detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced The MFD and or PFD detected a failure in the FliteCharts database optional feature 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 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 version mismatch correct terrain database versio
181. pressing it is stuck several times The G1000 system should be serviced if the problem persists Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 has 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
182. pted by the pilot To accept the displayed altitude place the cursor over the altitude and press the ENT Key The altitude entry will then change to light blue numerals indicating the altitude will now be used by the system for providing vertical guidance pe ACTIVE FLIGHT PLAN KMKC KCOS TFR NO DATA TRE Arriv FSHER PY NUON CURRENT VNV PROFILE ACTIVE VNV WPT 1000F t OPSHN F VS TGT Q taaan gt E TV DEV VIEH VNV PROF CNCL VNV VNV Figure 7 29 Direct to Active 12 While proceeding to OPSHN the LPV approach to runway 35R is preferred and will be used a Press the PROC Key to display the Procedures Window If the GPS system is not WAAS capable or WAAS is not available the LPV approach will not be displayed in the list of available approaches Selecting the LNAV approach for runway 35R will give vertical guidance up to the IAF Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B b SELECT APPROACH should be highlighted as shown in Figure 7 30 PROCEDURES SELECT ARRIVAL SELECT DEPARTURE LOADED 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 will be displayed as in Figure 7 31 AIRPORT KETS COLORADO SPRINGS CO APPROACH CHANNEL s CHANNEL 97799 10
183. pture mode ALTS or ALTV is armed as appropriate Vertical Path Tracking Active VNAV Target Altitude Capture Armed navi 108 00 117 95 KICT CUTIE at A IH GN JF Ji ae 118 608 Cont a VNAV Target Altitude Vertical Deviation Indicator Required Vertical Speed Bug Mirt TAS 120KT e Terminal HSI Set to GPS e a OLL a Phase of Flight OAT 77 F ISA 27 F La A ei a IMPORT 0000 ALT LCL 07 10 35 Figure 6 12 Vertical Path Tracking Mode Automatic Pitch Hold Reversion a The following circumstances cause mode reversion Several situations can occur while Vertical Path without arming Vertical Path Tracking Mode Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode Vertical Path Tracking and the e Navigation source manually changed from GPS appropriate altitude capture modes are armed for possible e CNCL VNV Softkey selected on the Active Flight descent profile recapture if the vertical deviation Plan Page MFD Exceeds 200 ft during an overspeed condition All remaining vertical waypoints deleted from the e Experiences a discontinuity exceeding 200 ft due to flight plan a flight plan change e Displays entering Reversionary Mode e Becomes invalid due to excessive cross track error Non Path Descents track angle error e Cannot be computed for a leg type such as a hold or procedure turn Pitch Hold Vertical Speed and Flight Level Change modes can al
184. r 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 8 16 1 2 190 00567 01 Rev B FLIGHT PLAN With either the Active or Stored Flight Plan displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to select the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window Remove KCRQ OK or CANCEL Figure 8 21 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 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 3 4 SECTION 8 FLIGHT PLANNING Press the INVERT Softkey Invert and activate stored flight plan will be 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 highlig
185. re 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 eel key uy A key is stuck on the PFD and or MFD bezel Attempt to tree 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 module 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 1 10 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B Database Message Advisor
186. reasing to 350 feet depending on variables see Figure 2 24 1 0 nm decreasing to a specitied course width then 0 3 nm depending on variables see Figure 2 25 Missed Approach 190 00567 01 Rev B SECTION 2 FLIGHT INSTRUMENTS O 3 E E E m E ai 2 S E v O N a Me a Refer to accompanying roa P approach CDI scaling figures 5 LL Q O L rE i Enroute Missed O Departure Terminal Oceanic if gt 200 nm Terminal Approach ADOrOacH from nearest airport ai He O Drawing not to scale N 4 Figure 2 23 Phases of Flight CDI Scaling CDI scale is set to the smaller of 0 3 nm or an angle set by the system Bearing Pointers and Information Windows Selecting the PFD Softkey provides access to the BRG1 and BRG2 Sottkeys The BRGI Pointer is a single line pointer The BRG2 Pointer is a double line pointer angle set by system CDI Full scale Deflection 350 ft an o o l 2 NMEAF Bearing 1 Bearing 2 poe Pointer CDI CDI scale varies if Vectors To Final is activated Drawing not to scale Figure 2 24 Typical LNAV and LNAV V Approach CDI Scaling Q 8 E T P S E angle based Z 5 4 on database O information imi 2 nMpAF E A E Threshold I Bearing 1 Bearing 2 Information Information Window Window CDI scale varies if Vectors To Final is activated 5 i P J PAE ee Figure 2 26 HSI with Bearing Information Figure 2 25 Typ
187. reception If no data is received after 60 seconds traffic will be removed from the display 190 00567 01 Rev B SECTION 10 HAZARD AVOIDANCE Traffic Advisory aircraft is 400 above amp Traffic out o Traffic Mode descending moving in the direction of the line o j Last data update is older than 6 altitude level flight amp moving climbing moving in the Proximity Traffic at same Traffic 1600 above amp sec resulting in in the direction of the line Coast mode direction of the line Figure 10 11 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic will now be displayed on the map TIS Audio Alert When a Traffic Advisory TA is displayed an audio alert Traffic is given Traffic Not Available will be heard whenever TIS service becomes unavailable Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 SECTION 10 HAZARD AVOIDANCE 136 975 10 5 RYAN 9900BX TRAFFIC ADVISORY aa o ned SYSTEM TAS OPTION AL Traffic Mode Altitude oe i climbing Range Refer to the Ryan 9900BX pilots guide for a detailed discussion and an explanation of the aural alerts 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 Traffic Map Page OPERATING is disp
188. rence Guide for the Cessna 350 400 K Key s 1 4 1 6 L Lighted obstacle 10 14 Lightning 1 7 1 10 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 12 LOW ALT 2 6 Low Altitude 2 5 2 6 LPV 2 6 6 23 7 5 7 20 Manual Electric Trim 6 1 Manual Electric Trim MET 6 21 MAP 7 1 Map panning 10 5 Marker beacon 2 7 Marker Beacon Annunciations 2 2 messages 12 1 Message advisories 12 2 12 10 12 12 12 14 12 15 12 17 12 22 MET 6 1 METAR 10 3 10 5 MFD 1 1 4 3 Minimum descent altitude 2 2 Missed approach 6 32 Mixture 3 3 3 4 3 5 MKR MUTE 5 2 5 3 5 4 Mode S 4 4 Mode selection softkeys 4 5 Morse code identifier 4 3 Nav Com controls 4 1 NAV1 5 3 NAV2 5 3 Navigation 7 1 Navigation NAV Frequency Box 2 1 Navigation database 1 12 1 13 7 5 Navigation Mode 6 19 6 20 6 25 6 26 Navigation Status Box 2 1 Navigation status window 2 2 NAV Frequency Window 4 1 NCR 10 13 Nearest Airports Page 7 21 7 25 7 26 7 29 8 1 Nearest ARTCC amp FSS frequencies 7 28 Negative Climb Rate After Takeoff 10 13 NEXRAD 1 10 10 3 10 4 10 5 10 6 Non path descent 6 12 6 29 6 30 0 OBS 2 12 Obstacles 10 14 12 12 12 16 Operation 5 2 Outside Air Temperature OAT 2 1 Oxygen 3 2 P Page group icon 1 11 PDA 10 12 PFD 1 1 4 1 4 3
189. rinae 2 3 2 2 Attitude Indicator 0 0 0 ccs 2 4 23 Alime ti ansann 2 4 Altitude Select BUG szessinsevndctessssaatuneacctescsscaeentnsteatty 2 4 Altitude Trend Vector asusin n 2 4 Barometric Setting BOX sisri 2 5 Altitude Aleni aaien aE 2 5 Metric Display izsista a 2 5 Low Altitude Annunciation WAAS Only csesesees 2 6 2 4 Vertical Deviation Glidepath Glideslope Indicator canana 2 6 2 5 Marker Beacon Annunciations 2 7 2 6 Vertical Speed Indicator ccees 2 7 2 7 Barometric Altitude Minimume 2 8 2 8 Horizontal Situation Indicator HSI 2 9 Are H Sliesnia aE oattots ecm pnt Seas aa 2 9 Turn Rate Indicator and Heading Trend Vector 2 10 COE FOTO aiian 2 10 Course Deviation Indicator CDI 2 10 Bearing Pointers and Information Windows 2 11 Navigation OUE erone S 2 12 2 9 Wind Dat cece eesteeseesteaseeseaees 2 13 2 10 Generic Timer 00 cece cesses testes reaees 2 13 190 00567 01 Rev B TABLE OF CONTENTS SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 3 1 EIS DISDla Vioara aan 3 2 Oxygen System Optional cccsseseseeseseeseeen 3 2 THIN sete E TT 3 2 Carbon Monoxide Detection c sccscssesesesreeeeseean 3 2 3 2 Engine Leaning Assist Display 0 3 3 Engine Leaning for the Cessna 350 sss 3 3 Engine Leaning for the Cessna 400 3 5 3 3 Fuel Calculations 0 ccs 3 6
190. rom the HSI and the CDI will be positioned on the last dot indicating a 2 0 nm distance from the centerline of the next course 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 7 9 SECTION 7 NAVIGATION 7 As the CDI approaches center the aircraft turns onto the active leg as seen in Figure 7 22 136 975 ACTIVE FLIGHT PLAN KMKC KCOS FPL ACTIVE FLIGHT PLAN NORTH UP aS TFR NO DATA 69K MCI TIFT Enroute TOP aro V4 SLN SLN Airway 244 LAA e a HYS LAA Alrvoy V263 TBE TBE CURRENT VNV PROFILE ACTIVE UNV WPT VS TGT s s PH FPA i F 0 Taman PM TIME TO TOD i P 100r ha as Vee ee a Tsay i Figure 7 22 Turn on to Active Leg 7 10 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 At SLN Victor Airway 244 V244 will be intercepted Turn prompts will be displayed in the PFD Navigation Status Box as seen in Figure 7 23 136 975 Fa Figure 7 23 Turn to Intercept V244 9 As seen in Figure 7 24 V244 is now the active flight plan leg 136 975 ACTIVE FLIGHT PLAN KHKC KCOS __FPL ACTIVE FLIGHT PLAN NORTH UP Enroute TOP Airway V4 SUN SLN i V244 LA4 HYS 262 LAA 251 z n Airwoy V263 TBE TBE KOOS 322 Arrival KOOS TBE DBRY1 ALL CURRENT VNV PROFILE ACTIVE VNU WPT VS TGT V F tennan y gt RE T Vv DEV KSLNS 100F1 1000F t
191. s ot GPS Loss of GPS navigation due to GPS failure navigation GPS tail ABORT APR Loss or GPS navigation 4b 4 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 GPS1 FAIL GPS1 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is GPS2 FAIL GPS2 is inoperative unavailable The G1000 system should be serviced 12 14 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Message Comments 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 The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed transfer key is stuck 5 state Press the transter switch again to cycle its operat
192. sengaging the AUtOPIOt scesesesesseesessesseeen 6 22 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 TABLE OF CONTENTS 6 5 Example Procedures Using AFCG 0 6 23 PLE oela tE y aA E AE TN VEE 6 24 Intercepting a VOR Radial 6 25 Flying a Flight Plan GPS COUrSE scssessecseesesseeen 6 26 DESEE E EA EE E E E E EE 6 27 AU NE E E E O 6 30 Go Around Missed Approach ssssessecsessesseesneerees 6 32 6 6 AFCS Annunciations and Alerts 6 33 AT CS otai Ae e e 6 33 Overspeed ProtectiOn c sccssessesssesssessessesseaseesseesees 6 34 SECTION 7 NAVIGATION 7 1 7 4 Navigation Map Pag cccccccseeeceen 7 1 7 2 Direct to Navigation 7 1 Direct to Navigation trom the MFD 7 1 Direct to Navigation trom the PFD s s s 7 3 7 3 Navigating an Example Flight Plan 7 5 7 4 Airport Information 0 0 eee 7 21 7 5 Intersection Information 0 0 0 0 08 7 23 7 6 NDB Information 0 0 c cesses 7 24 7 7 VOR Information cece ees 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 ess0ee 7 25 Nearest Airports Information on the PFD 7 26 7 10 Nearest Intersections 7 26 7 11 Nearest NDB ucts 1 21 7 12 Nearest VOR ccc 1 21 7 13 Nearest User Waypoint 111111eeesseeeeen 1 28 7 14 Nearest Fr
193. set at the factory to 1200 Enter Code Using Softkeys 1 Press the XPDR Softkey to display the transponder Mode Selection softkeys 2 Press the CODE Softkey to display the transponder Code Selection softkeys which includes the digit softkeys 3 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 Press the XPDR Softkey to display the transponder Mode Selection softkeys 2 Press the CODE Softkey to display the transponder Code Selection softkeys which includes the digit softkeys 3 Turn the small FMS Knob to enter the first two digits 4 Turn the large FMS Knob to place the cursor in position to change the second two digits 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 4 5 SECTION 4 NAV COM amp TRANSPONDER Blank Page 4 6 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 5 AUDIO PANEL oo Be ai COMI MIC B ai COM2 MIC Transmitters COM3 MIC is unavailable Split COM Passenger Address Marker Beacon Mute Aircraft Navigation Radio Audio SECTION 5 AUDIO PANEL E COM1 Transceiver Audio COM 3 is unava
194. so be used to fly non path descents while 6 12 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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 20k ALTS VPTH Figure 6 13 Flight Level Change VNAV Non Path Descent To prevent immediate profile re capture the following must be satished e Atleast ten seconds have passed since the non path transition was initiated e Vertical deviation from the profile has exceeded 250 ft but is now less than 200 ft Pressing the VNV Key twice re arms Vertical Path Tracking for immediate profile re capture VNAV Target Altitude Capture Mode ALTV NOTE Armed VNAV Target Altitude and Selected Altitude capture modes are mutually 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 Altitude interception VNAV Target Altitude Capture is analogous to Selected Altitude Capture Mode and is armed automatically after the VNV Key is pressed and the next VNAV Target Altitude is to be intercepted before the Selected Altitude The annunciation ALTV
195. ssna 350 400 190 00567 01 Rev B 6 3 FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes Unless otherwise specified all mode keys are alternate action i e press on press off In the absence of specific mode selection the flight director reverts to the default pitch and or roll mode s Armed modes are annunciated in white and active in green in the AFCS Status Box Under normal operation when the control for the active flight director mode is pressed the flight director reverts to the default mode s for the axis es Automatic transition from armed to active mode is indicated by the white armed mode annunciation moving to the green active mode field and flashing for ten seconds A flashing yellow mode annunciation and annunciator light indicate loss of sensor AHRS ADC IAU or navigation data VOR LOC GPS VNAV WAAS required to compute commands When such a loss occurs the system automatically begins to roll the wings level or maintain the pitch angle depending on the affected axis The flashing annunciation stops when the affected mode key is pressed or another mode for the axis is selected If after ten seconds no action is taken the flashing annunciation stops and the flight director enters the default mode for the affected axis Figure 6 4 Loss of VOR Signal 190 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL If the information required to compute
196. stem should be serviced 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 possible Comments The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced The 1 GEA 71 has incorrect software installed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B GTX 33 Message Advisories SECTION 12 ANNUNCIATIONS amp ALERTS XPDR1 CONFIG XPDR1 config error The transponder configuration settings do not match those of backup Contig service req d MANIFEST GTX1 software mismatch communication halted XPDR1 SRVC XPDR1 needs service Return unit for repair configuration memory The G1000 system should be serviced The transponder has incorrect software installed The G1000 system should be serviced The 1 transponder should be serviced when possible XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder GRS 77 Message Advisories AHRS1 TAS AHRS1 not receiving airspeed AHRS1 GPS AHRS1 using backup GPS source AHRS1 GPS AHRS1 not receiving any GPS information AHRS1 GPS AHRS1 not receiving backup GPS information AHRS1 GPS AHRS1 operating exclusively in no GPS mode AHRS MAG DB AHRS magnetic model da
197. t Roll servo providing sustained force in the indicated direction Aileron Mistrim Left Elevator Mistrim Down Pitch servo providing sustained force in the indicated direction Elevator Mistrim Up Pitch Trim Failure PTRM lf AP engaged take control of the aircraft and disengage AP ae stuck MEPT Switch ae io disengaged move MEPT switches separately to unstick RollFailure Failure E roi 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 lm Ooo AP and MEPT 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 servos Preflight Test fail their power up tests Power must be cycled to the servos to remedy the situation Preflight system test failed aural alert sounds at failure Table 6 4 AFCS Status Alerts 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 33 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 34 Overspeed Protection While Pitch Hold Vertical Speed Flight Level Change Vertical Path Tracking or an altitude capture mode is active airspeed is monitored by the flight director and pitch commands are limited for overspeed protectio
198. t Initially a flight plan waypoint list is displayed as in Figure 7 8 The list is only populated when navigating a flight plan N A a RIAMT FL a OFFSET SNH KIXD i Ds 1074NH 51K Figure 7 9 Nearest Airport List PFD 190 00567 01 Rev B 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 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 ENT again to activate a Direct to Select a Direct to Destination to a Recently Entered Identifier 1 Press the Direct to GX 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 3 Turn the small FMS Knob to the right to display the RECENT waypoints as shown in Figure 7 10 OFFSET SHH DIS 1074H ACTIVATE Figure 7 10 Recently Entered Waypoints List PFD 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 ENT again to activate a Direct to 190 00567 01 Rev B SECTION 7 NAVIGATION Cancelling Direct to Navigation 1 Press the Direct to RJ Key 2 Press the MENU Key to display the Options Window The cursor will be tlashing on Cancel Direct to NAV 3 Press the ENT Key to c
199. t is displayed as in Figure o 3 Press the ENT Key The list is populated only when navigating a flight Select an Airport by Facility Name or City plan Location 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 55 4 Turn the large FMS Knob to select the desired 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to select the facility name or location city field AIRPORT 3 Enter the desired facility name or city 4 Press the ENT Key 5 To remove the flashing cursor press the FMS Knob Figure 7 55 Nearest Airport List 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 13 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B 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
200. t 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 3 IDENT FACILITY CITY KELN H CEN USA so 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 ENT again to activate a Direct to Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 NORTH UP 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 ENT 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
201. t 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 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 alt
202. tabase version mismatch The 1 AHRS is not receiving true airspeed trom the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced The 1 AHRS and 2 AHRS magnetic model database versions do not match 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 South no magnetic compass MANIFEST GRS1 software mismatch communication halted 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid The 1 AHRS has incorrect software installed The G1000 system should be serviced SECTION 12 ANNUNCIATIONS 12 20 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 fa
203. ted to values established during AFCS certification The flight director also provides commands to the autopilot Activating the Flight Director Pressing the FD or AP Key when the flight director is not active activates the flight director in default pitch roll modes Pushing the GA Switch or any flight director mode key activates the flight director in the respective mode s The flight director may be turned off by pressing the FD Key Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL Active Mode Mode Reference Armed Mode Autopilot Status Active Mode Armed Mode Ce AP ALTS VPTH Roll Axis Modes OO i o o Axis Modes AFCS Status Box 138 975 118 000 con ALTS VPTH 136 975 core Selected Altitude Box Aircraft Attitude Symbol Flight Director Command Bars Figure 6 2 PFD AFCS Display Command Bars AFCS Status Box Upon activation of the flight director Command Bars Flight director roll modes are shown on the left and are displayed on the PFD as a single cue If the attitude pitch on the right Armed modes are annunciated in information sent to the flight director becomes invalid or White and active in green Autopilot status is displayed in unavailable the Command Bars are removed from the _ the center of the AFCS Status Box display The Command Bars do not override the aircraft symbol Figure 6 3 Command Bars 6 2 Garmin G1000 Cockpit Reference Guide for the Ce
204. ted 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 00567 01 Rev B CELL MOV Selecting 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 Selecting the SIG AIR Softkey shows SIGMET and AIRMET information The display is updated every 12 minutes METAR Select 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 Select the MORE WX Softkey to display the following group of softkeys for additional weather control SFC Selecting the SFC Softkey for Surface Analysis shows current or forecast conditions Forecasts are available for intervals of Current 12 24 36 and 48 hours Select 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 Select the FRZ LVL Softkey to display contour lines for freezing levels The display is SECTION 10 HAZARD AVOIDANCE CYCLONE Selecting the CYCLONE Softkey shows the current location of cyclones hurricanes and tropical storms and their projected track at various time intervals The updat
205. the flashing 1 2 cursor 7 14 NEAREST FREQUENCIES Figure 7 66 Nearest Frequencies Page Select the Nearest Frequencies Page Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to select the sixth rectangular page icon Select and Load the Nearest ARTCC FSS or Weather Frequency 1 2 3 4 With the Nearest Frequencies Page displayed press the ARTCC FSS or WX Softkey to place the cursor in the appropriate field Turn the FMS Knobs to select the desired facility or frequency Press the ENT Key to load the frequency into the COM frequency standby field Press the FMS Knob to remove the flashing cursor 190 00567 01 Rev B VERTICAL LIHITS JE0OFT mel Figure 7 67 Nearest Airspaces Page Select the Nearest Airspaces Page 1 2 Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to select the seventh rectangular page icon Airspace Alerts Box e Ifthe projected course takes the aircraft inside an 190 00567 01 Rev B airspace within the next ten minutes Ahead is displayed If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside Ahead lt 2 nm is displayed If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside Within 2 nm is displayed If the aircraft has entered an airspace Ins
206. trol Mode The FMS Knob will now control the NAV radios 15 COM Key Selects COM Radio Control Mode The FMS Knob will now control the COM radios Frequency Transfer Key Switches between active and standby selected COM or NAV tuning frequencies Pressing and holding this key while in COM radio control mode tunes the COM radio to 121 50 MHz the emergency COM frequency 17 PFD Key Selects PFD Control Mode The FMS Knob will now control PFD functions MED Key Selects MFD Control Mode The FMS Knob will now control MFD functions Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Dual FMS NAV COM Knob Multifunction Control Knob With the MFD indicator illuminated the FMS NAV COM Knob performs the same functions as a the FMS NAV and COM Knobs on the MFD With the PFD indicator illuminated the FMS NAV COM Knob performs the same functions as a the FMS NAV and COM Knobs on the PFD 190 00567 01 Rev B SECTION 1 SYSTEM OVERVIEW TERRAIN Softkey ON Softkey OFF 1 3 PFD SOFTKEYS eS SS A A A e o TN rr ON Mn A VOR1 on HSI VOR2 on HSI GPS on HSI Figure 1 3 PFD Top Level Softkeys he TnHoanonon ames a d A D n i n n nT A n Tw Press the BACK or OFF Softkey to return to the top level softkeys Figure 1 4 INSET Softkeys INSET Press to display the Inset Map in the lower TOPO Press to display topographical data Q e left corner of the
207. ts Push to talk is pressed and the COM2 MIC annunciator blinks when the copilot s Push to talk is presssed Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 In this mode both the pilot and the copilot can transmit simultaneously over separate radios The pilot can still monitor NAV1 NAV2 and MKR audio as selected but the copilot is only able to monitor COM2 5 3 MARKER BEACON RECEIVER The marker beacon receiver is always on Only the marker beacon audio can be turned off Figure 5 4 shows the marker beacon annunciators on the PFD When the MKR MUTE Key is pressed the key annunciator 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 annunciator 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 present or press twice when an indication is present The key annunciator will be extinguished when the marker beacon audio is turned off Middle Marker Inner Marker my 1800 Altimeter Figure 5 4 Marker Beacon Annunciators on the PFD Outer Marker 190 00567 01 Rev B Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity al al MKR HI SENS MUTE Figure 5 5 Marker Beacon 5 4 NAV RA
208. ult 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 GDL69 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 MANIFEST GDC1 software The GDC 74A has incorrect software installed The G1000 system should be mismatch communication halted serviced GCU 476 Message Advisories GCU CNFG GCU Contig error GCU 475 contiguration settings do not match those of backup contiguration Contig service req d memory The G1000 system should be serviced GCU FAIL GCU is inoperative A failure has been detected in the GCU 475 The GCU 475 is unavailable ANIFEST GCU software mismatch The GCU 475 has incorrect software installed The G1000 system should be communication halted serviced GCU KEYSTK GCU key name Key A key is stuck on the GCU 475 bezel Attempt to free the stuck key by
209. ures the output effort torque and provides this signal to the pitch trim servo The pitch trim servo commands the motor to reduce the average pitch servo effort When the autopilot is not engaged the pitch trim ser vo may be used to provide manual electric trim MET This allows the aircraft to be trimmed using a control wheel switch rather than the trim wheel Manual trim commands are generated only when both halves of the AP TRIM Switch are operated simultaneously Trim speeds are scheduled with airspeed to provide more consistent response Servo motor control limits the maximum servo speed and torque The servo mounts are equipped with slip clutches allowing the servos to be overridden in case of an emergency 190 00567 01 Rev B SECTION 6 AUTOMATIC FLIGHT CONTROL 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 ROL APP ALTS Figure 6 25 Autopilot Engaged Control Wheel Steering During autopilot operation the aircraft may be hand flown without disengagi
210. ust 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 anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING Itis very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 t
211. utes of descent path capture by Pressing the VNV Key e Adjusting the Selected Altitude If acknowledgment is not received within one minute of descent path interception the white VPTH annunciation starts 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 00567 01 Rev B 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 Altitude Hold Mode Active Indicates Acknowledgment Required navi 108 08 gt 117 95 E 136 975 118 A0A com NAVZ 117 9 136 975 comz VNAV Target Altitude Selected Altitude Belon VNAV Target 4108 cw T Vertical Deviation E scan E Indicator E Required Vertical Speed Bug 38nd Enroute Phase of HSI Set to GPS Flight OAT JF ISA 27 F Figure 6 11 Vertical Path Capture 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 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 profile An altitude ca
212. viation 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 VNV Target Ap Altitude K 2700 Vertical Speed Indicator Vertical Deviation A Indicator Seed Pointer Required Vertical Speed Figure 2 11 Vertical Speed and Devia tion Indicators VSI and VDI 190 00567 01 Rev B SECTION 2 2 5 MARKER BEACON ANNUNCIATIONS Outer Marker Middle Marker Inner Marker Altimeter Figure 2 14 Marker Beacon Annunciations Glidepath Indicator Figure 2 12 Glidepath Indicator 2 6 VERTICAL SPEED INDICATOR The Glideslope Indicator appears when an ILS is tuned in the active NAV receiver field see Figure 2 13 Marker Beacon Annunciation Vertical Speed Pointer Glideslope Indicator Figure 2 15 Vertical Speed Indicator The actual vertical speed is displayed inside the pointer Figure 2 13 Glideslope Indicator 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 2 7 SECTION 2 FLIGHT INSTRUMENTS 2 7 BAROMETRIC ALTITUDE MINIMUMS Alerting is inhibited while the aircraft is on the ground If the aircraft climbs after having reached the MDA once it The desired barometric altitude minimums can be set in reaches 50 feet above the MD
213. vigation Backcourse or Approach Rolls wings level modes The autopilot guides the aircraft back to the 5545598 aeea arid Selected Heading Course upon release of the CWS aoe aaa gt 22 Table 6 3 Roll Hold Mode Responses Button Roll Hold Mode ROL Changing the Roll Reference NOTE If Roll Hold Mode is activated as a result The roll reference can be changed by pressing the CWS of a mode reversion the flight director rolls the Button establishing the desired bank angle then releasing wings level the CWS Button When the flight director is activated the FD or AP Key is pressed Roll Hold Mode is selected by default This mode is annunciated as ROL in the AFCS Status Box The current aircraft bank angle is held subject to the bank angle conditions listed in Table 6 3 Roll Mode Roll Hold default Heading Select HDG Key Navigation GPS Arm Capture Track GPS Langaton VOR Enroute Arm Capture Track NAV Key VOR Navigation LOC Arm Capture Track LOC No Glideslope Approach GPS Arm Capture Track GPS Approach VOR Arm Capture Track APR Key VAPP Approach ILS Arm Capture Track LOC Glideslope Mode automatically armed Go Around in air GA Switch Table 6 2 Roll Modes 190 00567 01 Rev B Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 6 17 SECTION 6 AUTOMATIC FLIGHT CONTROL Heading Select Mode HDG Turns are commanded in the same direction as Selected Head
214. y Cessna 400 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 J3 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 3 FUEL CALCULATIONS Fuel Quantit Indicates Selected Fuel Quantity Fuel Fuel Used Gauge Left Fuel Tank Gauge Right Remaining Calculation FUEL _ z Endurance Calculation GAL USED RANGE NM Range L FUEL QTY GAL R FUEL QTY GAL 8 4 8 aia an Figure 3 6 EIS Display Fuel Calculations Group Fuel used GAL USED endurance ENDUR and range RANGE NM are all calculated based on the last manual adjustment of the fuel remaining GAL USED Measured fuel quantity hasno effect on fuel calculations Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining NOTE Refer to the POH for usable fuel quantity The following softkeys allow for adjustment of the remaining fuel quantity DEC FUEL Allows the pilot to decrease the gallons of fuel remaining GAL REM in 1 gallon increments INC FUEL Allows the pilot to increase the gallons of fuel remaining in 1 gallon increments RST FUEL Resets the fuel remaining to 98 gallons 3 6 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 01 Rev B SECTION 4 NAV COM amp TRANSPONDER SECTION 4 NAV COM AND TRANSPONDER The NAV COM controls and frequency boxes are located on the Primary Flight Display and the Multi Function Display in the same locations
215. y 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 SECTION 1 SYSTEM OVERVIEW tuning box light blue box between the COM1 and COM2 fields COM Frequency Transfer Key Transfers the standby and active COM frequencies Pressing and holding this key for two seconds automatically tunes the emergency frequency 121 5 MHz in the active frequency field COM VOL SQ Knob Controls COM audio level Pressing this knob turns the COM automatic squelch ON and OFF Audio volume level is shown in the field as a percentage Direct to Key Allows the user to enter a destination waypoint and establish a direct course to the selected destination specified by the identifier chosen from the active route or taken from the map pointer position FPL Key Displays the active Flight Plan Page for creating and editing the active flight plan or for accessing stored flight plans CLR Key DFLT MAP Erases information cancels an entry or removes page menus To display the Navigation Map Page immediately press and hold CLR MFD only Dual FMS Knob Used to select the page to be viewed only on the MFD The large knob selects a page group MAP WPT AUX NRST while the small knob selects a specific page within th
216. ypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Create a New Flight Plan Using the PFD 1 2 3 NOTE A flight plan cannot be entered using the PFD if another flight plan is active NOTE After the first leg is entered using the PFD only it is immediately activated Press the FPL Key then press the FMS Knob to activate the cursor Turn the small FMS Knob to enter the first letter of the departure airport identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 2 to spell out the rest of the waypoint identifier Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 8 8 1 Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 2 through 4 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active Figure 8 12 Creating Flight Plan on the PFD ENTER AN AIRWAY IN A FLIGHT PLAN Press the FPL Key to display the active flight plan or display a stored flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the waypoint before which the airway will be entered Figure 8 13 Airway Insertion Point 190 00567 01 Rev B SECTION 8 FLIGHT PLANNING

Garmin Software Version 0530.04 Cockpit Reference Guide

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