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Garmin Software Version 0534.11 Cockpit Reference Guide

1. 2 Generic TIME icia t ehe ar ic a n eara d c XR 2 Configure Vspeed Bugs 2 Set Barometric Minimum Descent Altitude sss 3 Displaying Wind Data 3 Changing HSI 7 5 nennen 3 ENGINE INDICATION SYSTEM 5 oce naa cued Lean nde nba SR ms 6 Engine Leaning Assist Mode sss 0 NAV COM TRANSPONDER AUDIO PANEL 3 ADF Tuning Optional ssssssseetnnntnnnntnn 3 DME Tuning Optional c ccccuscssscsssssssssscssssssssssscsssssssssscesssssssssscesssssssssecesssssessnsees 3 Enter a Transponder Code sss 3 Selecting a COM Radio sse 4 Selecting 4 NAV COM Tuning 5 4 Digital Clearance Recorder and Player 4 Intercom System ICS Isolation seen 5 GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM 7 Flight Director Activation sss 7 Vertical Modes nnne 8 Lateral Modes rictu ot RR Hd 9 GPS NAVIGATION isc cede ce olt id jv tacitae dali to 21 Direct to Navigation ssssssseseeeee nnne 21 Activat
2. Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain utente TERRAIN EAD i Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AFAD Terrain Ahead Terrain Impact Caution ITI or Ahead TERAN 9 d Caution Terrain Caution Terrain 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 61 sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix sed Annunciations amp Alerts A GARMIN PFD MFD MFD Alert Type 1 TAWS B Page Aural Message Pop Up Alert Annunciation Reduced Required TERRAIN CAUTION OopsTACLE Caution Obstacle Cau Obstacle Clearance or tion Obstacle Caution ROC o Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution 101 or Ahead CAUTION OBSTACLE d x Caution Obstacle Cau tion Obstacle Premature Descent TERRAIN 00 TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred
3. 9900 Large White Text Large Light Blue Text _ Small Lig Blue Text Small Light Blue Subd Text Small Wh t ed with Altitude Restrictio Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Bar ite Text siu uinnsu sub 59 oipny uadx 0105 AEN suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Nav Com XPDR Audio GPS Nav AFCS Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS Procedures Appendix Alerts Operation Features Index A GARMIN Altitudes associated with approach procedures are auto designated This means the system automatically uses the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small light blue text Altitudes associated with arrival procedures are manually designated This means the system does not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical navigation may
4. Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix m Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 Chartview database error exists Comments The MFD and or PFDs 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 MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs 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 DB MISMATCH Aviation database version mismatch Xtalk is off The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays DB MISMATCH Aviation database type mismatch Xtalk is off The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Install correct aviation database type in all displays DB MISMATCH Terrain database version mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays DB MI
5. 500 Excessive Descent TERRAIN SKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN mE Don t sink Rate Caution NCR or or E ere TAWS System Status Annunciations Alert Type TAWS System Test Fail TAWS Alerting is disabled No GPS position or excessively degraded GPS signal System Test in progress System Test pass 62 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 TAHS FAIL TAWS INHB TAWS N A TAWS TEST TAN System Test PFD MFD TAWS B Page ir Aural Message Annunciation TAWS System Failure None TAWS Not Available TAWS Available will be heard when sufficient GPS signal is re established one OK 190 00567 03 Rev A A GARMIN Annunciations amp Alerts VOICE ALERTS Voice Alert Description Minimums minimums The aircraft has descended below the preset barometric minimum descent altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Played when a Traffic Advisory TA is issued Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued TAS system Traffic Advisory System Played when the TAS system passes a pilot initiated self test Test Passed Traffic Advisory System Playe
6. DCLTR Removes displays the EGT and CHT readouts from the display ASSIST Accesses the Engine Leaning Assist Mode 8 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN Engine Indication System Cylinder Head lemperature Sjueuingjsu UATE Exhaust Gas TEMPERATURE EGT F CHT F Temperature 174616141726 370 366 354 16801658 1702 1988 1750 1500 1450 1300 1150 1000 E R Engine Temperature Group Cessna 350 3g BO 84 52 AEN 540 Turbine Inlet Cylinder Head Temperature Temperature Duruue d nubi HE Temperate E T DUM 1626 1428 1428 378 348 374 1 a 1900 1642 1740 1674 508 364 360 366 H 1750 1600 1450 a d 1300 1150 ge Engine Temperature Group Cessna 400 xipuaddy suelv uoneiedo junuuy jeuuouqy x pul 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 9 GARMIN ENGINE LEANING ASSIST MODE NOTE Consult the Cessna 350 400 Aircraft Flight Manual AFM for leaning procedures From the Engine Page the Engine Leaning Assist Mode may be accessed by selecting the ASSIST Softkey Selecting the ASSIST Softkey again returns the MFD to the Engine Page Use the SYSTEM Softkey to exit the Engine Page While in Assist Mode the EIS Display is shown along with the Fuel Flow Gauge and an expanded Engine Temperature Group Cessna 350 When the ASSIST Softkey is se
7. waypoint 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 33 oipny uddx 59 sjuauimnasu U10 AEN 16114 52 2 Buluuejd AEN Sd5 nubi sual uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul GARMIN Flight Planning Ssjueuinijsu fila 59 U105 AEN s24v AeN Sd5 4 34 Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00567 03 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna 350 400 34 A GARMIN Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A
8. 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu XM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 50 1 2 3 Turn the large FMS Knob to select the Auxiliary Page Group Turn the small FMS Knob to select the displayed AUX XM Information Page Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN 0 Additional Features Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available c
9. CAUTION Alerts ssssennnnnnn nnns Annunciation Advisory Message Advisory Alerts 58 CO Guardian Messages nennen 58 APCS Alerts 000000 0 00000 0 000 00 rie 59 Terrain SVS Alerts etre i te toga nU od Rod bod d 60 TAWS Alerts 5 SUUM 61 do BOLA eoo adio 63 MFD amp PFD Message Advisories 63 Database Message Advisories 64 GMA 1347 Message Advisories sssssssssssee ne 67 GIA 63 Message Advisories sssssssee nnn GIA 63W Message Advisories GEA 71 Message 5 GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GDC 74A Message Advisories GCU 476 Message Advisories Miscellaneous Message Advisories sssssss 16 APPENDIX s r PFD Softkey Map MFD Softkey Map 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 iii Table of Contents GARMIN Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92
10. INC FUEL RST FUEL The DONE Softkey changes to UNDO when the checklist item is already checked SYSTEM DONE EXIT EMERGCY nnn VS MFD Softkeys Access the EIS functions Returns to the top level EIS display Turns the oxygen system on or off optional Cycles the EGT and CHT cylinder temperatures on and off Accesses the Engine Leaning Assist Mode Resets the CO Guardian and acknowledges an alert Decreases the gallons of fuel remaining GAL REM in 1 gallon increments Increases the gallons of fuel remaining GAL REM in 1 gallon increments Resets the fuel remaining to 98 or 102 gallons Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN MAP TRAFFIC TOPO TERRAIN AIRWAYS NEXRAD XM LING BACK DCLTR 3 SHW CHRT CHKLIST Appendix Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays NEXRAD weather and coverage information on Navigation Map optional Displays XM lightning information on Navigation Map optional Retur
11. Wfl unuuy Flight Instruments Nav Com AFCS XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VORT LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field DIGITAL CLEARANCE RECORDER AND PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC Pressing the PLAY Key once plays the latest recorded memory block then returns to normal operat
12. and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glide e AFCSAnnunciaions PFD Setup Menu path and Vertical Flight director Com Windows displayed in Deviation Indicators mand Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports VNV Target Altitude Window Flight Plan Wind Data Messages Selected Heading Box Procedures Selected Course Box ADF DME Tuning Transponder Status Barometric Minimum Box Descent Altitude Box Extreme Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position 54 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Abnormal Operation A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating i
13. bid paezey Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Engine Indication System GARMIN Fuel Calculations Group NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset Fuel used GAL USED endurance ENDUR and range RANGE NM are all calculated based on the displayed fuel remaining GAL REM and the fuel flow totalizer The fuel remaining can be adjusted using the following softkeys DEC FUEL Decreases totalizer based fuel remaining in one gallon incre ments INC FUEL Increases totalizer based fuel remaining in one gallon increments RST FUEL Resets totalizer based fuel remaining to the aircrafts fuel capacity 98 gal or 102 gal usable and sets the GAL USED display to zero Fuel Endurance Remaining ENDUR Calculation 79 6 4 40 Fuel Used R calan 7 NH Calculation Fuel Calculations Group Engine Temperature Group The temperature group displays the Cylinder Head Temperature CHT and Exhaust Gas Temperature EGT in degrees Fahrenheit for each cylinder using bar graphs and digital readouts For the Cessna 400 Turbine Inlet Temperature TIT is shown on a sliding bar scale The following softkeys can be used to modify the display of engine temperature information
14. mal ED g 2 a 1 Select the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or select the TMR REF Softkey 593 olpny uqax 0105 AEN 52 DISPLAYING WIND DATA AEN Sd5 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data to the left of the HSI 3 Select one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window select the OFF Softkey Duruue d SeJnpa20Jd CHANGING HSI FORMAT 1 Select the PFD Softkey 2 Select the HSI FRMT Softkey 3 Select the 360 HSI Softkey to display the full size HSI Or Select the ARC HSI Softkey to display the arc style HSI sual uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy x pul 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 3 Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Flight Instruments Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 A GARMIN 190 00567 03 Rev A GARMIN ___Engine Indication Syste
15. Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix end Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES CONT Message Comments MFD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced The MFD and PFDs have different software versions installed The G1000 system should be serviced PFD1 COOLING PFD1 has poor MFD1 COOLING MFD1 has poor cooling Reducing power usage cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G1000 system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The G1000 system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage R
16. Fax 886 02 2642 9099 ovided herein no part of this manual may be reproduced copied transmitted to this eg sion this m provided text a of this manua istered s of Garm of Gar that such electronic o hereby grants perm nual onto a hard driv copyright notice and or any revision here trademarks of Garm provided furth to is strictly pro in any storage medium for any purpose without the express ission to down e or other elect printed copy of this manual or revision oad a single copy of this ronic storage medium to er that any unauthorized hibited in Ltd or its s min 190 00567 03 Rev A in Ltd or its subsidiar ubsidiaries FliteCharts ies These trademarks may not be used ademark of Jeppesen Inc XM is a registered trademark of XM Printed in the U S A Warnings Cantans amp Notes GARMIN WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The disp
17. Key Approach VAPP Glidepath GP LOC Glideslope GS HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 17 sia sjueunasu oipny uadx u102 AEN ARN Sd5 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d Junuuy jeuuouqy jeuonippy xipueddy x pul ii Wfil4 paezey Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch Pitch Hold attitude may be used to dimb default PIT descend to the Selected Altitude 7v77 77 Captures the Selected Altitude ALTS Armed Altitude Hold Holds the current Altitude Key AUT Reference Holds aircraft vertical speed may Vertical Speed be used to climb descend to the VS Key VS nnnn rem Selected Altitude Holds aircraft airspeed while aircraft Flight Level Change 1 is climbing descending to the FLCKey FLC nnnkr Selecte
18. also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give vertical flight path guidance 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 GPS Navigation White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the Altitude has been entered The system cannot system estimating the by the pilot Altitude is use this altitude in altitude of the aircraft as it designated for use in determining vertical passes over the navigation giving vertical flight path flight path guidance point This altitude is guidance Altitude does provided as a reference not match the published and is not designated to altitude in navigation be used in determining database or no published vertical flight path altitude exists guidance Small Text Altitude is not designated Altitude is designated The system cannot to be used in determining for use in giving vertical use this altitude in vertical flight path flight path guidance determining vertical 24 guidance Altitude has been retrieved from the navigation database and is provided as a reference Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published
19. failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR 1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 65 s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy 3 5 x pul
20. field Enter the desired radial from the reference waypoint 8 Press the ENT 190 00567 03 Rev A Key Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 oipny uddx 59 sjuauimnasu U105 AEN 16114 52 2 AEN 540 nubi sual uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 9 A GARMIN The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 10 Press the ENT Key The cursor is now placed for entering another reference waypoint if desired 11 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Tum the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Select the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A NEW FLIGHT PLAN 28 NOTE When creating a new flight plan
21. highlight the desired flight plan d Select the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window 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 32 1 2 3 4 5 6 Press the FPL Key on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the INVERT Softkey Invert and activate stored flight plan is displayed With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Flight Planning COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS 4 Turn the large FMS Knob to highlight the flight plan to be copied Knob to activate the cursor 5 Select the COPY Softkey A Copy to flight plan confirmation window is displayed 6 With
22. select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 If desired select the VIEW Softkey to access the 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 area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 45 AeN 540 S24V oipny uddx sia Sjueumajsul Tuo2 AEN iui Duruue d ni e uepioAy s mp oold paezey Suelv uoneiedo s m Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Enable Disable Aviation Data 1 While the TAWS B Page is disp
23. system are found in the G1000 Pilot s Guide for this aircraft 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 amp Notes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN Recent of Beyini Change Summary 190 00567 00 Rev A 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 Rev B Changed company references to Cessna 190 00567 02 Reformatted manual Added GDU 9 03 parameters 190 00567 03 Added GDU 9 05 with Synthethic Vision System SVS Removed Stormscope edd Date of Revision Affected Pages 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 RR 1 Record of Revisions GARMI Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN table of Contents FLIGHT s s s s 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 1 Change Navigation Sources sssssssseenennnnnnnens 1 Enable Disable OBS Mode While Navigating with 6 5
24. system should be serviced when possible GIA 63 MESSAGE ADVISORIES Message GIA1 CONFIG GIA1 config error Config service req d Comments The GIA1 and or GIA2 configuration settings do GIA2 CONFIG GIA2 config error Config service req d not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio GIA2 CONFIG GIA2 audio config error Config service req d configuration The G1000 system should be serviced GIA1 COOLING GIA1 temperature The GIA1 and or GIA2 temperature is too low 00 low to operate correctly Allow units to warm up to 2 COOLING GIA2 temperature operating temperature oo low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be GIA2 COOLING GIA2 over serviced temperature 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 67 so1njeoJ 2 Bujuuejd AEN 5649 2 oipny uadx sia syu unysu paezey ESTE JUI05JAEN Wil jeuonippy uoneiedo Jeuuouqy 3 c x pul Flight Instruments Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Additional Abnormal Operation Index Append
25. the large FMS Knob to highlight the LEG field d 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 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 25 oipny uddx 59 sjuauimnasu U105 AEN 16114 52 2 AEN 540 nubi sual uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 26 6 7 8 9 10 11 12 13 A GARMIN Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM is an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps 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 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings The flashing cursor moves
26. waypoint 8 Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint i 4 Turn the small FMS Knob The Waypoint Information Window is now displayed s inserted before the highlighted waypoint 5 Enter the new flight plan waypoint by one of the following a Enter the u b Press the E Or ser waypoint identifier facility or city NT Key a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 oipny uddx 59 sjuauimasu U10 AEN 1614 52 2 4 AEN 540 nubi uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning GARMI N Turn the large FMS Knob to select the desired waypoin
27. waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an aviation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed 16 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message FPL TRUNC Flight plan has been truncated Comments This occurs when a newly installed aviation database eliminates an obsolete 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 locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriv
28. 00 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ALERTS Annunciation Window Alerts Window Message Audio Alert Voice Text Message Repeating Door not secured Chime Door Open Fuel tank is not correctly selected or in OFF position Chime Fuel Valve No power on the left bus Chime No power on the right bus Carbon Monoxide level is too high Chime Chime Carbon Monoxide Low oil pressure Chime Oil Pressure Low CAUTION ALERTS Annunciation Window Alerts Window Message Audio Alert Voice Text Message Left Alternator offline Single Chime Left Alternator Out Right Alternator offline Single Chime Right Alternator Out Cessna 350 only 190 00567 03 Rev A Fuel pump is operating Single Chime Fuel Pump Low fuel in the left tank Single Chime None Low fuel in the right tank Single Chime None Rudder limter is engaged Single Chime None Starter relay has power applied Single Chime None Oxygen system needs attention Single Chime None or is off Oxygen quantity below 250 psi Single Chime None Pressure above 12000 ft and Single Chime None oxygen system off Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 sainjea4 2 Duruue d
29. 2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced COM1 SERVICE COM1 needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 1 and or COM2 may still be usable The G1000 system should be serviced when possible COM1 PTT 1 push to talk key is stuck COM2 PTT COM2 push to talk 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 COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM and or COM 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 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 71 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey 346 UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix o
30. 67 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 81 Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Appendix Index A Appendix GARMIN TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coast lines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional feature D n nN S OODD n 75 75 79 n synvis T pets wmo DME BRet ctunrr sto BARo Back ALERTS n n T LA m Select the BACK Softkey to return to the top level softkeys r mon r en zen BL HE ML r ooo r PFD Configuration Softkeys 82 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN PFD SYN VIS PATHWAY SYN TERR HRZN HDG APTSIGNS DFLTS WIND OPIN I OPTN 2 OPTN 3 OFF DME BRGI HSI FRMT 360
31. A list of available transitions for the selected approach procedure is now displayed 6 Turn either FMS Knob to select the desired transition 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 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO UJ sjueumasu olpny uqax 59 U105 AeN 52 AEN 540 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach buluueld s mp old procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key eouepioAy soJnjeoJ jeuonippy ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN uoneiedo Jeuuouqy 1 Press the PROC Key 34 nu paezey 2 Tum the larg
32. AEN Sd5 52 olpny uqax sia sjuauimasu 2 ni uio AeN Yid jeuonippy uoneiedo jJeuuouqv 5 PE x pul Annunciations amp Alerts A GARMIN 2 ANNUNCIATION ADVISORY t Annunciation Window Alerts Window Message Audio Alert Text 8 AP TRIM OFF AP TRIM master switch is in the OFF position None OXYGEN ON Reminder Turn off oxygen None E RUDR HOLD Rudder hold is engaged None 2g SPEED BRAKES Speed brakes are active None Cessna 400 only MESSAGE ADVISORY ALERTS 8 Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative one 2 MED FAN FAIL The cooling fan for the MFD is inoperative one AVIONICS FAN The cooling fan for remote avionics is inoperative one TIMER ZERO Timer has counted down to zero Timer Expired Procedures FUEL IMBAL Fuel imbalance is greater than 10 gallons one LOW MAN PRES Manifold pressure is below 15 in one VAPOR SUPPR Turn on Vapor Suppression one Hazard Avoidance Cessna 400 only Additional Features CO GUARDIAN MESSAGES zs Alerts Window Message Comments f 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 Ind
33. AeN Sd5 Duruue d qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00567 03 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna 350 400 A GARMIN 5 GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Switch Roll Hold default ROL Pitch Hold default PIT Takeoff on ground TO Takeoff on ground Go x GA Go 7 pa ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold default ROL Vertical Speed VS VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS NAV Key Navigation Pitch Hold default PIT BC GPS Pitch Hold default PIT APR
34. 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 uoneiedo Jeuuouqy Sue v unuuy EDIT A STORED FLIGHT PLAN xipueddy 1 Press the FPL Key on the MFD 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 flight plan x pul 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 31 Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 4 5 6 7 A GARMIN Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to
35. Audio Hazard Avoidance Additional Features Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 52 A GARMIN Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 2 3 4 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Selecting the MORE Softkey repeatedly cycles through the preset channels Select any one of the PS1 PS15 softkeys to assign a number to the active channel Select the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 1 2 3 4 On the XM Radio Page select the RADIO Softkey Select the VOL Softkey to access the volume control softkeys Select VOL or VOL softkeys to adjust the volume level Select the MUTE Softkey to mute the radio audio Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMI N mal n n ABNORMAL OPERATION 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 engin
36. DEPARTURE LEG 1 Press the FPL Key on the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure 4 Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 oipny uddx 59 sjuauimasu U105 AEN 346 3 52 AEN 540 Duruue d wold s mp old uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 4 5 6 1 8 3 10 11 12 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired
37. Ensure TAS is operating 2 With the Navigation Map displayed select the MAP Softkey 3 Select the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turnthe small FMS Knob to select the last rectangular page icon Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN Hazard avoidance 3 If desired select the VIEW Softkey to access the 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 area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude 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 TERRAIN SVS NOTE Terrain SVS is only availabl
38. FMS Knob to select the next desired field 4 Turn the small FMS Knob to enter the desired number 5 Repeat steps 3 and 4 until the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 Press the ENT Key again to transfer the frequency to the active field 8 Turn the large FMS Knob to select the MODE field 9 Turn the small FMS Knob to select ANT ADF ADF BFO or ANT BFO 10 Press the ENT Key to complete the selection DME TUNING OPTIONAL 1 Select the ADF DME or DME Softkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 Select the XPDR Softkey to display the transponder mode selection softkeys 2 Select the CODE Softkey to display the transponder code selection softkeys for digit entry 3 Select the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 sjueumasu S24V olpny 4adX si JUI05 AEN uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 Jeuuouqy Jeuonippy paezey xipuaddy x pul iui
39. G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna 350 400 System Software 0534 11 or later A GARMIN Copy This manual ight 2006 2009 Garmin Ltd or its subsidiaries All rights reserved reflects the operation of System Software version 0534 11 or later for the Cessna 350 400 Some differences in operation may be observed when comparing the information in this manual to ear m 9 Ga Tel 913 397 8200 m 5 n Ga Tel AT n 03 391 3411 m tha n Ga Sou Tel n Garmi 44 0870 8501241 Corporation No 68 Jangsh Tel 886 02 2642 9199 Web Si Except as expressly p disseminated downloaded or stored en permission of Garmin Garm ual and of any revision al use n the complete writt man be v must contai iewed for person commercial Garmin an and with 0 NavData is a registered t Satellite Radio Inc March 2009 distribution of d G10009 are SafeTaxi are tradema ut the express permis te Address www garmin com lier or later software versions Fax 9 13 397 8282 c 2345 Turner Road SE Salem OR 97302 U S A Fax 503 364 2138 in International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park mpton 5040 ORB U K Fax 44 0870 8501251 u 2nd Road Shiir Taipei County Taiwan
40. HPERATURE ELECTRICAL N F CHT F 1650 1706 1754 358 368 368 ALT AMPS AMPS Dx 172818721614 soo 352 368 378 4 4 a 1750 1 1600 va mi Tin 1300 R 2001 AILERON TRIM Big Y Carbon rsaese j Monoxide OXYGEN DCLTR 1 ASSIST Warning Engine Page Cessna 350 O Oil Temperature Pressure Gauge O Electrical Group Engine Manifold Pressure Gauge Trim Group 0 Tachometer Engine Temperature Group Fuel Calculations Group Fuel Quantity Gauges Oxygen Quantity Gauge n Fuel Flow Gauge Oxygen Outlet Pressure Gauge 6 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A amp GARMIN ____ Baal indication System L FUEL QTY GAL R FUEL QTY GAL 100 OXYGEN DEC FUEL FUEL RST FUEL Engine Page Cessna 400 Carbon Monoxide Detection If carbon monoxide CO in the cabin becomes too high exceeds 50 ppm a flashing red annunciation and the current level of CO in parts per million ppm are displayed in the lower right corner of the Engine Page When a warning is generated the CO RST Softkey becomes available to reset the CO Guardian and acknowledge the alert 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 7 sjueuinasu x Suelv uoneiedo saunjea4 SoJnpa20Jd buluueld AEN 540 S24V junuuy jeuuouqy feuonippv xipuaddy x pul sufi t a 3
41. HSI ARC HSI Appendix Displays second level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction Displays compass heading along the Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings includ ing changing units to standard Displays softkeys to select wind data parameters Wind direction arrows with headwind and crosswind components Wind direction arrow and speed Wind direction arrow with headwind tailwind and crosswind components Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 83 s n e 4 auepiony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sia sjuauimasu jeuonippy 2 nubi Tuo2 NeN sub uoneiedo Jeuuouqy Sue v unuuy Est Flight Instruments Additional Hazard Flig
42. IN HG 1 Select the PFD Softkey 2 Select the STD BARO Softkey to set standard barometric pressure CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Select the HPA Softkey to display the barometric pressure setting in hectopascals 4 Select the BACK Softkey to return to the top level softkeys CHANGE NAVIGATION SOURCES 1 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency 3 Select the CDI Softkey a third time to return to GPS 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 1 xipueddy Suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 913 unuuy Jeuuouqy Jeuonippy paezey nu U10 AEN x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Planning AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Flight Instruments A GARMIN ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Select the OBS Softkey to se
43. 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 DELETE A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS 4 Turn the large FMS Knob to highlight the flight plan to be deleted Knob to activate the cursor 5 Select the DELETE Softkey A Delete flight plan amp confirmation window is displayed 6 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 GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flight Plan Page on the MFD 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 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point 4 Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so on 5 To change the user waypoint name follow the procedure for modifying a user
44. SMATCH Terrain database type mismatch The PFDs and MFD have different terrain database types installed Install correct terrain database type in all displays DB MISMATCH Obstacle database version mismatch The PFDs and MFD have different obstacle database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays 66 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts GMA 1347 MESSAGE ADVISORIES Message GMAT FAIL GMAT is inoperative Comments The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA1 CONFIG GMAT config error Config service req d The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The G1000 system should be serviced GMAT SERVICE GMAT needs Service Return unit for repair Fg The audio panel self test has detected a problem in the unit Certain audio functions may still be avail able and the audio panel may still be usable The G1000
45. THWAY Softkey 5 Select the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 If not already enabled select the SYN TERR Softkey 4 Select the HRZN HDG Softkey 5 Select the BACK Softkey to return to the previous page Displaying Airport Signs 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 If not already enabled select the SYN TERR Softkey 4 Select the APTSIGNS Softkey 5 Select the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts in electronic form it is still advisable to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Selecting the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Selecting the DCLTR Softkey twice removes VOR station 48 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN 0 Additional Features ID the VOR symbo
46. VAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe 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 POH 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 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Warnings 2 Notes GARMIN WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of anomalies in the earth s magnetic field operating the G1000
47. acks a Navigation Backcourse 00 E localizer signal for backcourse BC Capture Track approaches Approach GPS TP GPS Approach VOR Capture Track aplures and traks thej App VAPP selected navigation source Approach LOC Glideslope 1 GPS VOR LOC Key PEY N LOC Mode automatically armed Disengages the autopilot and GA Go Around commands a constant pitch GA Switch angle and wings level 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 19 s tin sul sub 59 oipny uadx U105 AEN ARN Sd5 52 suelv uoneiedo SaJnjeaJ aoueplony SoJnpa204d Duruue d Tunuuy Jeuuouqy Jeuonippy paezey Wfi l4 x pu ddy x pul GARMIN AFCS Sjueuinijsu fila 59 U105 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00567 03 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna 350 400 20 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to E Key 2 Enter the 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 constraint proceed to step 5 5 Turn the large FMS Knob to place the
48. al deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation Doox The selected waypoint box does not use the WGS 84 datum Cross check position with alternate navigation sources TRAFFIC FAIL Traffic device has failed The G1000 is no longer receiving data from the traffic system The traffic device should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed 78 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message MAG VAR WARN Large magnetic variance Verify all course angles Comments The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER f message Message criteria entered by the user 190 00567 03 Rev A Garmin G1000 Cockpi
49. altitude in the navigation database Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 flight path guidance 190 00567 03 Rev A GARMI N LLL RHlght Planning FLIGHT PLANNING 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 select the AUTO or MANUAL Softkey 4 For Direct to planning a Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position b If necessary press the MENU Key and select Set WPT to Present Position to display P POS c Press the ENT Key and the flashing cursor moves to the ending waypoint field d Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For point to point planning a Enter the identifier of the starting waypoint b Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint d Press the ENT Key to accept the waypoint Or For flight plan leg planning a Press the FPL Softkey at the bottom of the display b Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn
50. ay still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operation If the problem persists the G1000 system should be serviced G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced 72 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments 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 GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEAT config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G1000 system should be
51. ce Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Flight Planning CREATE A NEW USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Select the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 6 Thecursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Use one of the following methods to enter the reference waypoint a Turn the small FMS Knob to the left to display a list of flight plan waypoints This list is populated only when there is an active flight plan b Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 7 After pressing the ENT Key the cursor is displayed in the RAD radial
52. cept any interference received including interference that may cause undesired operation 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 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A amp GARMIN s n n Notes 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 condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the
53. cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Tum the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key 8 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 sjuauimasu wp 59 oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance A
54. d INVERT AN ACTIVE FLIGHT PLAN 1 2 30 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN ri htrtaning 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN sjuaumasu nubi 59 olpny uqax 0105 AEN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor 52 Or for a stored flight plan a Press the FPL Key on the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 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 procedure s waypoints AEN Sd5 gt e SeJnpa20Jd 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN eouepioAy paezey saunqea4 jeuonippy 1
55. d Altitude Vertical Path Tracking Capturas 15 d VNV Key VPTH an active vertical profile VNAV Target Altitude Captures the Vertical Navigation T ATV Capture VNV Target Altitude Glidepath Cap ures and tracks the WAAS GP glidepath on approach m Captures and tracks the ILS Glideslope GS glideslope on approach Disengages the autopilot and GA Go Around commands a constant pitch attitude GA Switch and wings level in the air ALTS armed automatica ly when PIT VS FLC or GA active and under VPTH w is to be captured instead of VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude GP is available in installations with GIA 63W IAUs when WAAS is available 18 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 en Selected Altitude 190 00567 03 Rev A A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds the current aircraft roll Roll Hold attitude or rolls the wings default ROL level depending on the commanded bank angle Captures and tracks the HDG Selected Heading Key a Navigation GPS GPS Navigation VOR Enroute Captures and tracks the m VOR Capture Track selected navigation source Navigation LOC Capture Track GPS VOR LOC NAV LOC No Glideslope Key en Captures and tr
56. d after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative The remote NAV1 and or NAV2 transfer Switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cess
57. d when the TAS system fails a pilot initiated self test Test Failed MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings XTALK ERROR A flight display crosstalk error has occurred The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired The MFD and PFDs are not communicating with each other The G1000 system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The G1000 system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The G1000 system should be serviced PFD1 CONFIG PFD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 soJnjeoJ 2 Buruuejd AEN 5649 24V oipny uadx sia syu unysu paezey nubi Wil jeuonippy uoneiedo Jeuuouqy A x pul Hazard Flight Nav Com Flight Features
58. e FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 xipueddy suelv junuuy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index A Procedures GARMIN ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL Press the ENT Key The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 38 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the Go around Switch Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the displa
59. e a Stored Flight Plan 22 Activate a Flight Plan Leg 22 Stop Navigating a Flight Plan 23 Vertical Navigation VNAV s s s s s s s s s s s si 23 FLIGHT PLANNING Re d A ua 25 Trip Planning inco ten ore Ro err e Mets e aar a e den 25 Create a New User Waypoint 2 Delete a User Waypoint sssssseenn nnne 28 Create a New Flight Plan sssssssee nnn 28 Insert a Waypoint in the Active Flight Plan sss 29 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 TbleofCoens GARMIN Enter an Airway in a Flight Plan 30 Invert An Active Flight Plan 30 Remove a Departure Arrival Approach or Airway from a Flight Plan 31 Store a Flight Plan nennen 31 Edit a Stored Flight Plan 31 Delete a Waypoint from the Flight Plan sss 32 Invert and Activate a Stored Flight 32 Copy a Flight Plan 33 Delete a Flight Plan 33 Graphical Flight Plan Creation ssssssssen 33 PROCEDURES cei meter mati uten ise odd uc t ad 35 Load and Activate a Departure Procedure sss 35 Activate A Departure Leg sssssessseeeenennnnnnnnnns 35 Load An Arrival Proc
60. e backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information AHRS1 GPS AHRS1 not receiving backup GPS information 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 AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS1 SRVC AHRS 1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The G1000 system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect softwa
61. e instrumentation on the remaining display Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel NOTE The Cessna 350 400 Airplane Flight Manual AFM always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established anuuuu Loss of Hazard Functions with Loss of GPS Position 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 53 eoueproAy Senpa204d AEN 540 52 oipny uddx 53 5149 11 15 puezey 34 U10 AEN 3461 saunqea4 jeuonippy Sue v unuuy xipueddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD
62. e when the Synthetic Vision System SVS option is installed and the TAWS option has not been installed NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Display Terrain on the TERRAIN SVS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired select the VIEW Softkey to access the 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 area 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 43 AEN 540 52 orpnyyuqdax sia Sjueumajsul Tuo2 AEN fid buluueld ni e uepioAy s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enab
63. educing power usage The MFD voltage is low The G1000 system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists The MFD and or PFD detected a failure in the basemap database 64 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists Comments 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 MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The MFD and or PFD detected a
64. edure 35 Activate An Arrival Leg 36 Load and or Activate an Approach Procedure 36 Activate An Approach in the Active Flight Plan 37 Activate a Vector to Final Approach Fix sss 38 Activate A Missed Approach in the Active Flight Plan 38 HAZARD iine itte asi aq ai 39 Customizing the Hazard Displays on the Navigation 39 XM Weather Optional seen Traffic Systems 5 d te Pe UU e t eit Terrain And Obstacle Proximity Terrain SVS screened ede pod te Deer pdt e pa Terrain Awareness amp Warning System TAWS Display Optional 45 ADDITIONAL FEATURES 5 AAA A ARAYA RA AA Y RA etat 47 Synthetic Vision ass eaten Zad s s aaa 47 Terminal Procedure Charts seen 48 XM Radio Entertainment ABNORMAL OPERATION Reversionary Abnormal COM Operation Hazard Displays with Loss of GPS Position 53 Unusual Attitudes eub t ttt tct tct tin bcr 54 Dead Reckoning sssssssseeennen nennen 54 ii Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN table of Contents ANNUNCIATIONS amp ALERTS 57 WARNINGAlerts ioni aee nb d e d o be eee
65. em persists the G1000 system should be serviced COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM and or in the enabled or transfer switch ag problem persists serviced engl the G1000 system shou COM transfer switch is stuck pressed position Press the ain to cyde its operation If the d be RAIM UNAVAIL RAIM is not available from FAF to MAP waypoints LOI GPS integrity lost Crosscheck with other NAVS GPS satellite cove Receiver Autonom RAIM from the F Loss of GPS integ rity monitoring rage is insufficient to perform ous Integrity Monitoring AF to the MAP waypoints 68 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts GIA 63 MESSAGE ADVISORIES CONT Message Comments GPS NAV LOST Loss of GPS naviga tion Insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to insufficient satel lites Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail f Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation TRUE APR True north approach Change hdg reference to TRUE Displaye
66. ex Appendix Ea 58 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN AFCS ALERTS Annunciations amp Alerts Description Pitch Failure PTCH MET Switch Stuck or PTRM Pitch Trim Axis Control Failure Elevator Mistrim Up System Failure EE AP and MET are unavailable FD may still be eme HR available TELE Elevator Mistrim Down Aileron Mistrim Left f Pitch axis control failure AP is inoperative Roll Failure ROLL Roll axis control failure AP is inoperative If annunciated when AP is engaged take control e aircraft and disengage the autopilot If nunciated when AP is not engaged move each of the MET switch separately to check if a Switch is causing the annunciation A condition has developed causing the pitch rvo to provide a s rvo to provide a s apply nose down ot disconnect ustained force Be prepared apply nose up control wheel force upon topilot disconnect ndition has developed causing the pitch ustained force Be prepared control wheel force upon A condition has developed causing the roll servo to provide a sustained left force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits seimpeooid AEN 549 52 oipny uadx si syuaumasul paezey uo2 AEN nubi saunqea4 jeuonippy Aileron Mistrim Right A condition has developed causing the r
67. ey is stuck A key is stuck on the GCU 476 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Sonje24 e uepioAy s mp oold Buruue d AEN Sd5 2 oipny uddx sia Sjueumasu paezey Wfila JUl05JAEN Wil jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct
68. hannels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT Softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 While on the XM Radio Page select the CHNL Softkey 2 Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Select the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 51 xipueddy suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 52 olpny uqax sia s tin sul unuuy Jeuuouqy jeuonippy paezey U10 AEN 1uBi 4 x pul Nav Com XPDR
69. ht Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Abnormal Operation Annun Alerts Appendix BRG2 ALT UNIT STD BARO METERS IN HPA A GARMIN Cycles the Bearing 2 Information Win dow through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Select to display the BARO setting as inches of mercury Select to display the BARO setting as hectopacals Sets barometric pressure to 29 92 in Hg 1013 hPa E n nnn mn n Press the BACK Softkey to return to the top level softkeys eee eee Press the BACK Softkey to return to the previous level softkeys Transponder Softkeys Appendix Index XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does not reply to any interrogations ON Selects Mode A transponder replies to interrogations 84 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN ALT GND VFR CODE 0 7 BKSP IDENT TMR REF NRST ALERTS Appendix Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discre
70. ight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint On the MFD select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN STOP NAVIGATING A FLIGHT PLAN GPS Navigation 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This does not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN 190 00567 03 Rev A 221 221 11 7NM 13000FT 9 2 12400FT 8 0NH Approach KDFH RNAV 17LePs LPV RIVET iof DRAAK TNWOD RW17L map 930FT POLKE RISE Cross AT or ABOVE 5 000 ft Fac Cross AT 2 300 ft Cinn 11 Cross AT or BELOW 3 000 ft 259 176 176 176 176 174
71. in the Active Flight Plan Window the first leg is activated automatically after it is created Using the MFD 1 Press the FPL Key 2 Turn the small FMS Knob to display the Flight Plan Catalog Page 3 Select the NEW Softkey to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window 5 Enter the identifier of the departure waypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter the identifier for each additional flight plan waypoint 8 When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Using the PFD A NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD Flight Planning 1 Press the FPL Key 2 Turn the small FMS Knob to display the Waypoint Information Page 3 Turn the small FMS Knob to enter the first letter of the destination waypoint identifier 4 Turnthe large FMS Knob to the right to move the cursor to the next character position 5 Repeat step 3 and 4 to spell out the rest of the waypoint identifier 6 Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint 7 Repeat steps 3 through 6 to enter the identifier for each additional flight plan
72. ing at waypoint boxx 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 than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm 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 SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 71 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey 346 UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy PE x pul Hazard Flight Nav Com F
73. ion Pressing the MKR MUTE Key while playing a memory block stops play Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select those isolated from hearing the Nav Com radios and music PILOT KEY COPLT KEY Pilot Hears Copilot Passenger ANNUNCIATOR ANNUNCIATOR Hears Hears PILOT Selected radios pilot copilot passengers music radios pilot Selected radios pilot OFF ON passengers music Selected CREW ON ON radios pilot copilot 190 00567 03 Rev A Selected radios pilot copilot passengers music Copilot passengers music Copilot Selected radios pilot copilot Selected radios pilot copilot passengers music Copilot passengers music Selected radios pilot passengers music Passengers music Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Nav Com XPDR Audio Panel Sjueuinajsu UATE 59 S24V oipny uddx JUI05 AEN SH lV uonesado s n e 4 eouepioAy s mp oold Buruue d AEN Sd5 junuuy jeuuouqy Jeuonippy paezey nubi xipueddy x pul GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila 59 oipny uadx U10 AeEN S2dV
74. ix d A nnunciations amp Alerts GIA 63 MESSAGE ADVISORIES CONT A GARMIN Message Comments GIA1 SERVICE GIA1 needs service The GIA1 and or GIA2 self test has detected a Return the unit for repair l problem in the unit The G1000 system should GIA2 SERVICE GIA2 needs service Return the unit for repair MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software MANIFEST GIA2 software mismatch installed The G1000 system should be serviced communication halted COM1 TEMP COM over temp The system has detected an over temperature Reducing transmitter power condition in COM1 and or COM2 The transmit COM2 TEMP COM over temp ter is operating at reduced power If the problem Reducing transmitter power persists the G1000 system should be serviced COM1 SERVICE COM needs service The system has detected a failure in COM1 Return unit for repair and or COM2 COM1 and or COM2 may still be COM2 SERVICE COM2 needs service usable The G1000 system should be serviced Return unit for repair when possible COMI PTT COM push to talk key is The COM1 and or COM2 external push to talk stuck switch is stuck in the enable or pressed COM2 PTT CON2 push to talk key is position Press the PTT switch again to cycle its stuck operation If the probl
75. keys 13 COM 14 53 Cylinder Head Temperature CHT F 5 8 D DCLTR Softkey 48 Dead Reckoning 54 Dedutter 54 81 87 Declutter EIS 8 Direct to 21 DME 13 14 DR mode 54 55 56 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 Index E Edit a flight plan 31 Enable Terrain 44 Endurance calculated ENDUR 8 Engine leaning assist 10 12 Engine Manifold Pressure MAN IN HG 5 6 Exhaust Gas Temperature EGT F 5 8 10 11 F FD 59 Flight Director 17 Flight path marker 47 FliteCharts 48 49 Frequency Transfer 14 Fuel calculations 8 Fuel Flow FFLOW GPH 5 6 10 Fuel flow totalizer 8 Fuel quantity FUEL QTY GAL 5 6 Fuel remaining 86 Fuel remaining calculated GAL REM 8 Fuel used calculated GAL USED 8 H Horizon heading 47 Inhibit TAWS 46 Inhibit Terrain 44 Inset Map 81 82 IOI 60 61 62 J Jeppesen 49 Index 1 sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax Sia sjuauimasu Jeuonippy 2 nf Tuo2 NeN ui uoneiedo Jeuuouqy Sue v unuuy Additional Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts ES Appendix Index M Map panning 40 Message advisories 63 79 MET 59 METAR 39 Minimums 63 Mistrim 59 MKR MUTE 14 Mode S 85 Mode selection softkeys 13 Multi Function Display MFD Soft
76. keys 86 N NACO 49 NAV 14 NAV1 1 14 NAV2 1 14 Navigation database 23 24 NEXRAD 39 40 82 87 0 OBS 2 Obstacles 66 71 Oil Pressure OIL PSI 5 6 Oil Temperature OIL F 5 6 Overspeed Protection 18 Oxygen Outlet Pressure OXY OUTLET PSI 6 Oxygen Quantity OXY QTY PSI 6 P Pathways 47 48 R Reversionary mode 53 ROC 60 61 62 Index 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 A GARMIN S SafeTaxi amp 48 Store Flight Plan 31 SVS 47 79 SVS Terrain 47 Synthetic Vision System 47 T TA 63 Tachometer RPM 5 6 TAF 39 TAS 42 63 74 TAWS 45 46 60 61 62 Terrain 42 43 45 66 82 87 Terrain SVS 43 44 Timer 76 Topographical data 82 87 Traffic 39 41 87 Traffic advisory 41 63 Traffic map page 41 42 43 Transponder 13 84 85 Trim 5 6 Turbine Inlet Temperature TIT F 5 12 V Vertical speed guidance 24 Vertical track 63 VNV 21 54 78 Vspeed 2 W WAAS 71 Weather data link page 39 Wind data 83 X XM lightning 82 87 XM weather 39 190 00567 03 Rev A A GARMIN Garmin International Inc 1200 East 1 51 st Street AS 66062 U A ud AU a 5040 9RB n No 68 Jangshu 2nd Shiir Taipei County 2006 2009 Garmin Ltd or its subsidiaries 190 00567 03 Rev A
77. l and intersection names if within the airport plan view Selecting the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Selecting the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of National Aeronautical Charting Office NACO terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expira
78. layed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN 0 Additional Features ADDITIONAL FEATURES SYNTHETIC VISION WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational aware ness only and may not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic WARNING Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper a
79. layed 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 the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather penetration Wea
80. le Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed select the INHIBIT Softkey Or 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key NOTE If Terrain SVS alerts are inhibited when the Final Approach is the 44 active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Hazard Avoidance TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to
81. lect OBS Mode 2 Turn a CRS Knob to select the desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Select the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Select the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 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 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS 1 Select the TMR REF Softkey 2 Turn the large FMS Knob to highlight the desired Vspeed 3 Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed 4 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF Softkey 2 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN T htinstruments SET BAROMETRIC MINIMUM DESCENT ALTITUDE
82. lected the system initially highlights the number and EGT readout of the cylinder with the hottest EGT Fuel Flow Gauge nav1188 88 113 00 TRK357 134 888 118 800 con navz 108 00 118 68 S ENGINE 193 800 118 000 conz FFLOW GPH EGT Deviation 1 2 from Peak TEMPERATURE EGT CHT F F 1562 1382 1202 356 338 320 16521472 92 500 292 320 374 1900 1750 1600 Pod 400 1950 300 ME 200 1150 1000 s t 100 572 3456 DCLTR DEC FUEL INC FUEL RST FUEL Engine Leaning Assist Mode Cessna 350 10 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Engine indieation System When the first peak is detected the cylinder numbers disappear Ist isannunciated in light blue below that cylinders EGT bar the temperature is marked in light blue on the graph and the EGT readout is outlined m E qom r 39 gt oe 3 B a Temperature Deviation from Peak First Cylinder TEMPERATURE x EGT F cone SE 1442 1452 1382 A peak 394 378 380 25 opg 14141416374 6 son 374 382 358 RB Light ou pp Blue Bar ix Dum uk a gt Represents Peak Indicates 22 2 First Oylinder 1007 B3456 lt to Peak Assist Mode First Peaked Cylinder Cessna 350 zs The system continues to detect peak EGTs for each cylinder as the fuel flow is decreased and the peak of each cylinders EGT is indicated by a light blue marker The last cyli
83. light Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message bad geometry PTK FAIL Parallel track unavailable Comments Bad parallel track geometry invalid leg type PTK FAIL Parallel track unavailable Invalid leg type for parallel offset past IAF PTK FAIL Parallel track unavailable IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertic
84. m ENGINE INDICATION SYSTEM SEA RPH 2300 ARSE II 6 10 20 30 40 F FUEL QTY GAL v m I 6 16 20 30 40 F FFLOW GPH 17 2 FFLOW GPH 17 2 YET MET 8 OX X GO Seo AILERON TRIM AILERON TRIM v Cessna 350 Cessna 400 EIS Display O Engine Manifold Pressure Gauge Exhaust Gas Temperature Indicator ne Cessna 350 only achometer Turbine Inlet Temperature Indicator 0 Fuel Quantity Indicator Cessna 400 only Fuel Flow Indicator 9 Oylinder Head Temperature Indicator G Oil Pressure Indicator Trim Group Oil Temperature Indicator 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 5 sjueumasu xipuaddy uoneiedo s m e q e uepioAy 2 Duruue d AEN Sd5 24V olpny uqax Jeuuouqy jeuonippy x pul 3 U105 AeN nubi paezey unuuy GARMIN ENGINE PAGE Selecting the SYSTEM Softkey on the MFD accesses the Engine Page which displays all Engine Indication System instruments selecting the softkey again exits the Engine Page Oxygen quantity and outlet pressure are also shown on the Engine Page The OXYGEN Softkey can be used to turn the optional oxygen system on off If an oxygen system is not installed blank gauges are displayed 8 888 com 8 000 conz C r 2 i 5 ball vc 35 8 T SI Fa q Fa to ta L FUEL QTY GAL R FUEL QTY GAL f TE
85. ments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 4 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 Key to return to the map 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 3 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 shows 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 Echo Top Cloud Top and Echo Top Mutually Exclusive Cell Movement City Forecast Freezing Levels Cyclone Warnings M e E QU 1 XM Lightning METARs Surface Analysis County Warnings Cloud Top SIGMETs AIRMETs Winds Aloft TRAFFIC SYSTEMS e If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS i
86. n 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 the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function is not capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain positio
87. n awareness using other navigation equipment until GPS derived position data is restored 69 CDI Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 55 sjuauinajsu Wfl aoueplony 2 buluueld AEN Sd5 S24V oipny uadx puezey ubi UI05 AeN saunyea4 jeuonippy xipuaddy Suelv unuuy x pul Nav Com XPDR Audio Hazard Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation A GARMIN As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and Terrain Proximity and TAWS are disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 56 Garmin G10
88. na 350 400 69 saunqea4 2 Buruuejd AEN 5649 24V oipny uadx sia siu umn sul paezey nubi u102 AEN Wil jeuonippy uoneiedo Jeuuouqy nM Ea x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix m Annunciations amp Alerts A GARMIN GIA 63 MESSAGE ADVISORIES CONT Message Comments G S1 SERVICE G S1 needs service Return unit for repair Return unit for repair G S2 SERVICE G S2 needs service 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 GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature is too low to operate cor
89. nd Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message with other NAVS LOI GPS integrity lost Crosscheck Comments GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver m
90. nder to peak is denoted by the Last annunciation below its bar on the graph and the EGT readout is outlined in light blue paezey Temperature Deviation fm Peah Last Cylinder p ES TEMPERATURE Tir a CHT FF 1426 1438 1366 392 378 378 e 00 1402 137 7 80 as 4500 1400 1402 1374 Son 372 380 352 3 3 l H 11 1 er Indicates gt Last 3 y as 2 i 45 6 Cylinder to l n ur 2 Peah Assist Mode Last Peaked Cylinder Cessna 350 x pul 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 11 Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS GPS Nav Procedures Appendix Alerts Operation Features Index Engine Indication System Cessna 400 A GARMIN Once the ASSIST Softkey is selected the peak of each TIT is indicated by a light blue bar which moves and remains at the peak Turbine Inlet Temperature Peak TIT TEHPERATURE 1608 1450 1300 1158 1990 Lean or Rich TIT Deviation From Peak from Peak Engine Leaning Assist Mode Cessna 400 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN NAV COM TRANSPONDER AUDIO PANEL Nav Com XPDR Audio Panel ADF TUNING OPTIONAL 1 Select the ADF DME Softkey 2 Turn the small FMS Knob to enter the first digit of the desired ADF frequency 3 Turn the large
91. nnun EIS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 22 1 2 3 From the Active Fl
92. ns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the ac tive flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 87 sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV oipny uddx sia sjuaumnasu jeuonippy 2 nf JUI0 NEN ATE uoneiedo Jeuuouqy Sue v unuuy End GARMIN Appendix Sjueuinijsu fila 59 U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey saunjyea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00567 03 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna 350 400 88 A GARMIN A Activate a flight plan 22 Active channel 51 ADF 13 14 54 83 84 Advisory alerts 58 AHRS 74 75 Airport Signs 47 48 Airways 87 AP 59 Assist engine leaning 10 12 Audio panel controls NAV1 NAV2 14 Autopilot 59 Barometric Altitude Minimums 3 Barometric pressure 84 C Carbon monoxide detection 7 CDI 1 14 77 Channel Presets 52 ChartView 48 49 Clearance player 14 Clearance Recorder 14 Code selection soft
93. oll servo 7 to provide a sustained right force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Preflight Test PFT Performing preflight system test Upon completion the aural alert will be heard PFT Preflight system test has failed 5 p 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 59 uoneiedo Jeuuouqy x pul A Annunciations amp Alerts GARMIN TERRAIN SVS ALERTS Flight Instruments PFD MFD Alert Type TERRAIN SVS MFD Aural Page Pop Up Alert Message D Annunciation Reduced Required Terrain TERRAIN Warning Terrain 82 Clearance Warning RTC Terrain 2 5 Imminent Terrain Impact TERRAIN Warning Terrain Warning ITI Terrain Warning Obstac AFCS Reduced Required Obstacle TERRAIN Dd Clearance Warning ROC Obstacle Imminent Obstacle Impact TERRAIN Warning Obstacle Warning 101 Obstacle Reduced Required Terrain TERRAIN CAUTION TERRAIN Caution Terrain _ Clearance Caution RTC Terrain E Imminent Terrain Impact TERRAIN CAUTTON TERRAIN Caution Terrain Caution ITI Terrain E Reduced Required Obstacle TERRAIN cautton osstacteE Caution Obstacle 8 1 Clearance Caution ROC Obstacle Imminent Obstacle Impact TERRAIN cautton OBSTACLE Caution Obs
94. pproach path angle during landing Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 system SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD In addition to SVS enhancement to the PFD the following features have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying SVS Terrain 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 Select the SYN TERR Softkey 4 Select the BACK Softkey to return to the previous page 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 47 xipueddy suelv uoneiedo sainyea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimasu unuuy Jeuuouqy jeuonippy paezey nu U10 AEN iui x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A ARMINM Displaying Pathvvays 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 If not already enabled select the SYN TERR Softkey 4 Select the PA
95. re installed The G1000 system should be serviced 74 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN GDL 69A MESSAGE ADVISORIES Annunciations amp Alerts Message GDL69 CONFIG GDL 69 config error Config service req d Comments GDL 69 configuration settings do not match those of backup configuration 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 communication halted The GDL 69 has incorrect software installed The G1000 system should be serviced GDC 74A MESSAGE ADVISORIES Message Comments MANIFEST GDC1 software mismatch communication halted The GDC 74A has incorrect software installed The G1000 system should be serviced GCU 476 MESSAGE ADVISORIES Message Comments GCU CNFG GCU Config error Config service req d GCU FAIL GCU is inoperative GCU 476 configuration settings do not match those of backup configuration memory The G1000 system should be serviced A failure has been detected in the GCU 476 The GCU 476 is unavailable MANIFEST GCU software mismatch communication halted The GCU 476 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name K
96. rectly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature temperature GIA2 COOLING GIA2 over The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced 70 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted Comments A GIA mismatch has been detected where only one is WAAS capable MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM 2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM
97. runway Press the ENT Key With LOAD highlighted press the ENT Key The arrival becomes part of the active flight plan If an altitude associated with a waypoint in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired waypoint altitude Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired waypoint within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 1 2 36 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 Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A GARMIN LLL Procedures Press the ENT Key A list of available approaches for the destination airport is displayed 4 Turn either FMS Knob to highlight the desired approach 5 Press the ENT Key
98. s configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed 40 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Hazard Avoidance Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation S Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not 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 Tum 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 OPERATING is displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is 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 6 Selec
99. serviced GTX 33 MESSAGE ADVISORIES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR1 FAIL 1 is inoperative There is no communication with the 1 transponder 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 13 So1nje2J aoueplony s mp oold Buruue d AEN Sd5 S24JV oipny uddx Sia sjueumasu paezey ETSI nubi jeuonippy uoneiedo Jeuuouqy Ins PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Appendix Index Annunciations amp Alerts GRS 77 MESSAGE ADVISORIES A GARMIN Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using th
100. t d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 1 2 3 4 5 6 1 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserte
101. t Reference Guide for the Cessna 350 400 79 s m p q eo uepioAy SoJnpa204d Duruue d AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy Ins Dow x pul Flight Instruments Nav Com XPDR Audio Flight Planning Additional Hazard Avoidance Abnormal EIS AFCS Procedures GPS Nav Features Operation Appendix Index Annunciations amp Alerts Blank Page 80 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 A GARMIN 190 00567 03 Rev A amp GARMIN Appendix APPENDIX sjuauimasu sub PFD SOFTKEY MAP 59 optional mer 997 C590 foe xe ST pweme Wer wmm 77 um m 7 uu uu m olpny uqax uo2 AEN CDI NAV2 52 Top Level Softkeys AEN Sd5 optional mnnunnn buluueld nubi optional optional ess E parce oS n E 8 LA FHN EE S Press the BACK Softkey to return to the top level softkeys gt Chr 5 aa m 2E Inset Map Softkeys ge go os dasi INSET Displays Inset Map in PFD lower left corner 92 OFF Removes Inset Map eki DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan Sue v unuuy gt 5 3 a x x pul 190 005
102. t the TNA MUTE Softkey to mute the Traffic Not Available aural alert 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 AEN Sd5 S24V oipny uddx sia J05 AeN ii Duruue d nf aoueploay s mp oold paezey suelv uoneiedo SaJnjeoJ Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 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 is now displayed on the map Traffic Advisory System TAS Optional 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 displayed in the Traffic Mode field 3 Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by selecting the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 5 Select the MUTE Softkey to mute TAS voice alerts Displaying Traffic on the Navigation Map 1
103. tacle Caution 101 Obstacle Hazard Avoidance Terrain SVS System Status Annunciations PFD MFD Alert Type TERRAIN SVS Page Aural Message Annunciation System Test fail TER FAIL Terrain System Failure E Terrain Alerting is disabled TER INHB one Additional Features Abnormal Operation No GPS position or excessively TER N A Terrain System Not Available degraded GPS signal Terrain System Available will be heard when sufficient GPS signal is re established System Test in progress TER TEST None System Test pass Terrain System Test OK Ix Append Index 60 Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A A GARMIN Annunciations amp Alerts TAWS ALERTS PFD MFD MFD Alert Type TAWS B Page Aural Message 5 Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance or Pull Up Warning RTC or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up 2 Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up tena Oe 3 Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstade PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up 0
104. tely addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection soft keys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 85 sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimasu Jeuonippy nubi Tuo2 NeN ui uoneiedo Jeuuouqy Sue v unuuy End Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index Appendix MFD SOFTKEY MAP Press the SYSTEM Softkey to Fk FN A 7 F wo return to the default page level optional A GARMIN SHW CHRT A optional optional Default softkey is dependant on Press the BACK Softkey on this the selection made level to return to the top softkey level options optional optional TRAFFIC TOPO TERRAIN AIRWAYS lt NEXRAD XM LTNG BACK SYSTEM OXYGEN DCLTR ASSIST CO RST DEC FUEL INC FUEL RST FUEL mre on SYSTEM 86 SYSTEM OXYGEN DCLIR ASSIST CO RST DEC FUEL
105. ther information provided by the GDL 69A is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 190 00567 03 Rev A amp unu Cautions amp Notes 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 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 WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is 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 NA
106. tion date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 49 xipuaddy suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimasu junuuy Jeuuouqy Jeuonippy paezey 346 wo gt AeN ufi x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features A GARMIN View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5
107. to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Enter the fuel onboard Press the ENT Key when finished Note that in AUTOMATIC page mode fuel onboard is provided by the fuel totalizer The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature Garmin G1000 Cockpit Referen
108. 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 It is 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 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 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 ac
109. y of traffic 3 Press the small FMS Knob to return to the Navigation Map Page XM WEATHER OPTIONAL N V ARNING Use of XM vveather for hazardous vveather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 190 00567 03 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna 350 400 39 AEN 540 S24V orpnyyuqax sia Sjueumajsul Tuo2 AEN fid Duruue d nubi aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instru

Garmin Software Version 0534.11 Cockpit Reference Guide

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