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Garmin Software Version 0435.24 Cockpit Reference Guide

1. 59 ABNORMAL OPERATION Reversionary Abnormal COM Operation Audio Panel Fail safe Operation Hazard Displays with Loss of GPS Position Unusual Attitudes ceo mto oie BR RA RAR Bss Dead Reckoning ssssssseenene nennen ANNUNCIATIONS amp CAS Messages ode deed a Comparator 0 5 Reversionary Sensor Annunciations TAWS B Alerts see s s sini TCAS II Alerts and Annundiations Aural Ale eers Flight Plan Import Export Messages MFD amp PFD Message Advisories Database Message Advisories GMA 1347D 1347D 20 Message Advisories GIA 63W Message 150 5 GSD 41 Message Advisories Optional GEA 71 Message Advisories ssssssee nne GTX 33 33D Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GWX 68 Alert Messages nennen GDC 74B Message Advisories GCU 475 Message Advisories GMC 710 Message Advisories sss Miscellaneous Message Advisories ssssssss EA
2. 5 Crew Alerting System CAS 6 CAS Messages 3 eesti ote monens Gg de 000 6 NAV COM TRANSPONDER AUDIO PANEL 7 Enter or Change Flight ID 5 7 ADF Tuning s s s s s s ss s s s s s s is ss s s l 7 DME Tuning Optional s s s s s S s s s s s s s s s s s s s il 7 Enter a Transponder sss 8 Select Transponder Mode s s s s s sss s ssss s sss s ssssss n 8 Selecting a COM Radio 75 5 s s s s s s s ssss s sss s sss s ssssss n 8 Selecting a NAV Radio s s nnns 9 NAV COM Tuning 55 9 Intercom System ICS Isolation 9 Clearance Recorder and Player 0 AUTOMATIC FLIGHT CONTROL SYSTEM s 1 Flight Director Activation ssssssnnnnnnn 1 Vertical Modes nnne 2 Lateral Modes ouo ttti ctr rh tar do d 3 GPS NAVIGAHON 5 Direct to Navigation sssssssseseeeee nnne 5 Activate a Stored Flight Plan 6 Activate a Flight Plan Leg
3. 36 Copy a Flight Plan nnne Delete a Flight Plan etc Graphical Flight Plan Creation Export a Flight Plan to an SD Card 37 PROCEDURES URL Eel a a Load and Activate a Departure Procedure Activate A Departure Leg ssssssseeeeennnnnnnnnnns Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure 5 41 Activate An Approach in the Active Flight Plan 42 Activate a Vector to Final Approach Fix 42 Activate A Missed Approach in the Active Flight 77 42 HAZARD AVOIDANCE ois is os cena 43 Customizing the Hazard Displays on the Navigation 43 XM WX Satellite Weather Subscription 43 Traffic Systems 0207 00 0 00 46 Terrain Awareness amp Warning System TAVIS B 50 Airborne Color Weather Radar 52 ADDITIONAL FEATURES ssse nenne Synthetic Vision Optional Terminal Procedure Charts ii Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Ele of Contents AOPA Airport Directory ssssssseeeeenennenn nnne 59 SiriusXM Radio Entertainment Subscription
4. GARMIN Level 1 Level 2 Level 3 Level 4 Description ON Activates transponder transponder replies to identification interrogations VVhen the transponder is set to ON the TCAS II system is set to standby ALT Altitude Reporting Mode transponder replies to identification and altitude interrogations VVhen the transponder is set to ALT the TCAS TI system is set to standby TA ONLY Activates the TCAS TI system in TA Only Mode and sets the transponder to ALT TA RA Activates the TCAS TI system in TA RA Mode and sets the transponder to ALT BACK Returns to the previous softkey level TCAS Displays the TCAS control softkeys REL Displays intruder altitude as altitude relative to own aircraft altitude ABS Displays intruder MSL altitude ALT RNG Displays the altitude display range softkeys ABOVE Displays non threat traffic from 9900 feet above the aircraft to 2700 feet below the aircraft Typically used during climb phase of flight 104 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Appendix Level 1 Level 2 Level3 Level 4 Description CODE IDENT 190 00600 04 Rev A NORMAL Displays non threat traffic from 2700 feet above the aircraft to 2700 feet below the aircraft Typically used during enroute phase of flight BELOW Displays non threat traffic from 2700 feet above the aircraft to 9900 fe
5. Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system 74 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations 8 Alerts Flight Plan Import Export Results File contained user waypoints only Description The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun cated The flight plan on the SD card contains more waypoints than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Way points locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be
6. 84 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message COM1 RMT XFR 1 remote transfer key is stuck Comments The COM1 and or COM transfer switch is stuck in the enabled or pressed position COM2 RMT XFR 2 remote transfer key is stuck Press the transfer switch again to cycle its operation If the problem persists the 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 cycle its operation If the problem persists the system should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed GSD 41 MESSAGE ADVISORIES OP TIONAL Message Comments GSD1 CONFIG GSD1 config error Config service req d GSD1 and the CDU have different copies of the GSD1 configuration 6901 COOLING 5501 temperature too low GSD1 is reporting a low temperature condition GSD1 COOLING GSD1 over temperature GSD1 is reporting an over temperature condition GSD1 SERVICE GSD1 needs service Return unit for repair MANIFEST GSD1 software GSD1 is reporting an inte
7. TAWS Not No GPS position TAMS N A Available Excessively degraded GPS i signal Out of database TAWS N A None 7 Coverage area TCAS II ALERTS AND ANNUNCIATIONS Traffic Mode PFD Mode MFD Traffic Map Page Display Annunciation Mode Annunciation Status Icon Other Maps TCAS II Self test Initiated TEST Traffic Advisory and Resolution Advisory None TA RA 72 Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang TEST MODE also shown in white on top center of page 190 00600 04 Rev A A GARMIN Annunciations amp Alerts Traffic Mode PFD Mode MFD Traffic Map Page Display Annunciation Mode Annunciation Status Icon Other Maps Traffic Advisory Only TA ONLY TA ONLY TCAS II Standby STBY on ground 177 say TEC STBY also shown in white in D ITCAS STBY n center of page TCAS II Failed TCAS FAIL ext Annunciation appears yellow while in flight TCAS II Modes Traffic Map Page Annunciation Description Data is not being received from the TCAS II unit Data is being received from the TCAS II unit but the unit is self reporting a failure Incorrect data format received from the TCAS II unit TCAS II Failure Annunciations Traffic Status Banner Annunciation 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Description
8. 6 Stop Navigating a Flight Plan 7 Vertical Navigation 5 2 8 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Table of Contents GARMIN FLIGHT PLANNING ab aa Aaa 21 Weight Plannirig 3 dedo dde deed ede ente ded de 21 Trip Plannilig teet tede tate ids 21 Create a User Waypoint Defined by Latitude amp Longitude 23 Create a User Waypoint Defined by Radials from Other Waypoints 24 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 26 Create a User Waypoint using the Map 2 Delete a User Waypoint ssssssseee nnn Create a Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan 30 Enter an Airway in a Flight Plan 31 Invert An Active Flight Plan 33 Remove a Departure Arrival Approach or Airway from a Flight Plan 33 Store a Flight Plan coeant inen 34 Edit a Stored Flight Plan sssssssseeennnnn 34 Delete a Waypoint from the Flight Plan ss 35 Invert and Activate a Stored Flight 5 5 75
9. FlightPlamning 11 12 13 14 15 16 a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints 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 airports 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 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 USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint Press the ENT Key
10. MINIMUMS Turn the small FMS Knob clockwise to select BARO or RAD ALT Press the ENT Key Use the small FMS Knob to enter the desired altitude Press the ENT Key To remove the window press the CLR Key or the TMR REF Softkey DISPLAYING WIND DATA 1 2 3 4 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 3 Press the PFD Softkey Press the WIND Softkey to display wind data below the Selected Heading Press one of the OPTN softkeys to change how wind data is displayed To remove the Wind Data Window press the OFF Softkey zn g 2 o a sualy uonesado so1njeoJ 2 Buruuejg AEN Sd S24V oipny uadx svoli junuuy jeuuouqy paezey nubi xipueddy x pul GARMIN Flight Instruments I uS oipny uadx U105 AEN 52 AeN 5492 Buruuejd Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A GARMIN 4045 ENGINE INDICATION amp CREW ALERTING SYSTEM ian TT E 161 oipny uddx U10 AEN 72 8 n27 84 1 DC VOLTS AMPS T S24V gt ACN Sd5 1500 2727 90 10 BATTERY 1000 27 voLTS Wil so CABIN PRESS 700 700 ALT FT RAT
11. A Resolution Advisory is outside the selected display range Annunciation is removed when traffic comes within the selected display range a a a A Taffic Advisory is outside the selected display range Annunciation is removed when traffic comes within the selected display range i a a System cannot determine bearing of Resolution Advisory Annunciation indicates distance in nm altitude separation in hundreds of feet and altitude trend arrow climbing descending 73 s mip q e2uepioAy SaJnpa20Jd Duruue d AEN Sd5 92 olpny uqax sv siu uin su p ezeH nubi u102 AEN Yid jeuonippyv uoneiedo jJeuuouqv iiA FW x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN Traffic Status Banner Annunciation Shown as symbol on di Shown in center of Tra Description System cannot determine bearing of Traffic Advisory Annunciation indicates distance in nm altitude separation in hundreds of feet and altitude trend arrow climbing descending TCAS II unit has failed unit is self reporting a failure or sending incorrectly formatted data Data is not being received from the TCAS II unit c Map Page c Map Page TCAS II Traffic Status Annunciations AURAL AL
12. OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 2 3 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 34 1 2 3 4 5 6 7 Press the FPL Key for 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 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Fight Planning DELETE A WAYPOINT FROM THE FLIGHT PLAN Delete using the Quick Select Box active flight plan only 1 Press the FPL Key on the MFD Control Unit to display the active flight plan 2 Use the Joystick to move the Quick Select Box around the desired waypoint to be deleted 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected waypoint Delete using the cursor 1 Press the FPL Key to display the active flight plan Pr
13. ears in the AFCS Status Box The acceptable bank angle range is indicated in Scale of the Attitude Indicator sv l3 sjueuinasu oipny uadx 0105 AEN ARN Sd5 52 spay uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d Tunuuy Jeuuouqy Jeuonippy xipueddy x pul iui Wfl 2 GARMIN AFCS Sjueuinijsu fila 5729 U105 AEN 52 AeN 5492 4 r Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 14 A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 Press the Direct to I Key on the MFD or MFD Controller 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted GPS Navigation 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an 5 Turn the large FMS Knob counterclockwise to place the cursor over the NV altitu altitude constraint proceed to step 5 de 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 Turn the sm all FMS Knob to select MSL or
14. 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Select the MODE Softkey If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed Turn the Joystick to select the desired range If desired select the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Moni tor the displayed tilt value in the TILT field When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt of the antenna 1f the Tilt Line is not displayed perform the following steps 1 2 3 52 Press the MENU Key Turn the large FMS Knob to select Show Tilt Line Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Hazara avoidance Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field Wh
15. 5 6 1 8 9 10 11 12 x uw Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 Acknovvledge the Povver up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for each display Loading the Jeppesen Navigation Database as the Active Navigation Database 1 2 3 4 NOTE Loading the Jeppesen navigation database as the active database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow NOTE After the navigation database is loaded o
16. A GARMIN Level 1 Level 2 Level 3 Description IDENT STBY ON ALT GND VFR CODE TMR REF NRST MSG 102 0 7 BKSP Selects Standby Mode transponder does not reply to any interrogations Selects Mode A transponder replies to identification interrogations 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 discretely addressed Mode S interrogations Not available with TCAS II option Automatically enters the VFR code 1200 in the U S A only Not available when TCAS II option is installed 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 Messages Window Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN o optional Sc SS 7o 25s cor Jporowe peser esr user ssr T 35 npnmnmnmnunntun nnunnnu Press the BACK Softkey to return to the top level softkeys os rose F on ross TT JL ee pues T sx ss nnn nn nmnmnn Sele
17. A NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use A NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site 46 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Displaying Traffic on the Traffic Map Page 1 2 3 4 5 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select th
18. Overspeed Protection 12 P Pathways 55 56 PIREP 45 PIT 69 Play 10 Profile View 106 Q Quick Select Box 18 28 33 35 39 40 Index 2 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A GARMIN R Resolution Advisory 46 56 Reversionary mode 63 Reversionary Mode EICAS 5 ROC 71 S SafeTaxi amp 55 57 SBAS 12 41 51 65 66 83 84 Sector scan 54 Sensor 70 SIGMET 44 45 STAB 54 Standby 52 Standby Navigation Database 110 Store Flight Plan 34 SVS 55 94 Synchronization 108 SYNC Status 111 Synthetic Vision System 55 T TAF 43 TAS 47 48 87 TAVVS 50 51 71 TAWS A 71 98 TAVVS B 50 TCAS Il 8 48 49 56 97 102 104 Terrain 50 80 98 107 TFR 44 45 Tilt line 52 Timer 2 91 Topographical data 98 107 Traffic 43 47 49 106 Traffic Advisory 46 Traffic map page 47 48 49 Transponder 7 8 95 101 105 190 00600 04 Rev A A GARMIN V Vertical speed guidance 19 Vertical track 74 VNV 15 64 93 94 Vspeed 2 W WATCH 54 Waypoint Selection Submenu 29 Weather Attenuated Color Highlight 54 Weather data link page 43 Weather radar 52 Wind data 100 X XM lightning 98 107 XM WX Satellite Weather 43 44 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Index Index 3 sainjea4 eouepioAy SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sY213 sjuaumasu jeuonippy 2 nubi Tuo2 Ne
19. ddy x pul GARMIN GPS Navigation Ssjueuinijsu fila 5721 oipny uadx U105 AEN s24v 549 Buruuejd Blank Page 6 2 4 aoueplony puezey saunjyea4 jeuonippy uoneiedo jewuouqy suay unuuy x pu ddy x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 20 A GARMIN FLIGHT PLANNING WEIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters Turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the Weight Planning Page 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field 2 Enter the desired aircraft empty weight 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enterthe desired weight of Pilot amp Stores 5 Press the ENT Key 6 Continue repeating these steps until all desired weights have been entered Entering Fuel Parameters 1 If necessary press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors Or Manually enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Enter the desired reserve fuel quantity 6
20. or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the top card slot of the specified PFD or MFD contains invalid data The SD card in the bottom card slot of the specified PFD or MFD contains invalid data TRN AUD FAIL Im Awareness audio source unavailable The audio source for terrain awareness is offline Check G A1 or GIA 2 TERRAIN AUD CFG Trn Awareness audio config error Service req d Terrain audio alerts are not configured properly The system should be serviced XPDR 1 CRTL FAIL XPDR1 not receiving control information XPDR 2 CRTL FAIL XPDR2 not receiving control information Transponder 1 or 2 cannot be controlled because the transponder is not receiving control information The system should be serviced NO NAV CAPTURE ntercept angle too large for LOC BC capture The Localizer or Localizer Back Course was not captured because the intercept angle was too large GSD FAIL GSD1 is inoperative GSD1 has failed or status is unknown 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 95 saunqea4 uepjoay 2 Buruuejd AEN Sd 24V olpny uqax svoli sjuawin su paezey nubi wi0 gt AeN nubi jeuonippy uoneiedo Jeuuouqy ic EE x pul Flight Instruments Nav Com XPDR Audio Additional Hazard Flight Planning Abnormal EICAS AFCS GPS Nav Features Avoidance Procedures O
21. AGU 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 using the PFD 1 Press the Direct to Key E on the PFD 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 counterclockwise to place the cursor over the ALT altitud 190 00600 04 Rev A e field Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang sjuauimasu sub 5721 oipny uddx UI0JNeN ACN 540 52 suey uoneiedo sainjea4 aoueplony saunpadolg buluueld unuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 1 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude constraint Press the ENT Key If the
22. Airport Directory Information While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display SIRIUSXM RADIO ENTERTAINMENT SUBSCRIPTION OPTIONAL The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled 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 channels for the selected category 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 59 2 Buruuejd AeN Sd5 S24V oipny uadx svola siu u nnsul Tu102 AEN 346 eouepioAy paezey xipueddy sue v uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features 0 GARMIN Selecting a Category
23. HPA Press to display the BARO setting as hectopacals STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa OBS Selects OBS mode on the CDI when navigating by GPS only available with active leg CDI Cycles through GPS VORI LOC1 and VOR2 LOC2 navigation sources on the CDI ADF DME Displays the ADF DME Tuning Window providing ADF tuning capability when installed and allowing selection of the NAV source for tuning each DME optional M ser Jeesson sro T 5s T POET passe wesr sc 1 nn r r r m r Press the BACK Softkey to return to the top level softkeys ss Jes peooe Tver L Ex JL ev o r ALT LT 2 T T3 Ts L s L 7 Je se T back L wee EF V3 SEN UB n n EHH Transponder Softkeys Selecting BACK returns to the previous softkey level Level 1 Level 2 Level 3 Description XPDR Displays transponder mode selection softkeys XPDRI Selects the 1 transponder as active XPDR2 Selects the 42 transponder as active 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 101 SoJnjeaJ e uepioAy SaJnpa20Jd Duruue d AEN Sd5 241V oipny uddx sv l3 siu uin sul jeuonippy piezeg nubi Tuo2 NeN BUT uoneiedo Jeuuouqy Sue v unuuy a bz Additional Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix
24. MESSAGE ADVISORIES Annunciations amp Alerts Message GMC CONFIG GMC Config error Config service req d Comments GMC 710 configuration settings do not match those of backup configuration memory The system should be serviced GMC FAIL GMC is inoperative MANIFEST GMC software mismatch Communication halted A failure has been detected in the GMC 710 The GMC 710 is unavailable The GMC 710 has incorrect software installed The system should be serviced GMC KEYSTK GMC key name Key is stuck A key is stuck on the GMC 710 bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the system detects that a stored flight plan waypoint is locked This occurs when a navigation 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 navigat
25. 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 Press the ADF DME Softkey 2 If two DMEs are installed tum the large FMS to select the DME source field 3 Tum the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection 190 00600 04 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang 7 sjuauimasu sub 52 oipny uadx 5721 U10 AEN sualy uonesado so1njeoJ a2ueplony seinpe2oJd Buruuejg AEN 5649 junuuy jeuuouqy feuonippv paezey nubi xipuaddy x pul Abnormal Additional Hazard Annun Flight Instruments Flight Planning Nav Com AFCS XPDR Audio EICAS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Nav Com XPDR Audio Panel A GARMIN ENTER A TRANSPONDER CODE 1 2 3 Press the XPDR Softkey XPDR TFC if the TCAS II option is available Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press 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 ent
26. Press the FMS Knob to remove the cursor TRIP PLANNING 1 Tum the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select the Trip Planning Page 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 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Flight Planning sjuauimasu Yid 5721 oipny uddx UI0JNeN 52 2 AEN 540 nubi eouepioAy 2 suelv uoneiedo SaJnjeoJ unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 22 4 For a b o d Or Fo a b d Or A GARMIN Direct to planning Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the way
27. Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix n Annunciations amp Alerts A GARMIN GDC 74B MESSAGE ADVISORIES CONT Message ADC1 AS EC ADC1 airspeed error correction is unavailable ADC2 AS EC 2 airspeed error correction is unavailable Comments GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted The GDC 74B has incorrect software installed The system should be serviced GCU 475 MESSAGE ADVISORIES Message Comments GCU CNFG GCU Config error Config service req d GCU 475 configuration settings do not match those of backup configuration memory The system should be serviced GCU FAIL GCU is inoperative A failure has been detected in the GCU 475 The GCU 475 is unavailable MANIFEST GCU software mismatch communication halted The GCU 475 has incorrect software installed The system should be serviced GCU KEYSTK GCU key name Key is stuck 90 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A key is stuck on the GCU 475 bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists 190 00600 04 Rev A A GARMIN GMC 710
28. Rev A A GARMIN GPS Navigation White Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance Light Blue Text Altitude has been entered by the pilot Altitude is designated for use in giving vertical flight path guidance Altitude does not match the published altitude in navigation database or no published altitude exists Light Blue Subdued Text The system cannot use this altitude in determining vertical flight path guidance Small Text Altitude is not designated to be used in determining vertical flight path guidance Altitude has been retrieved from the navigation database and is provided as a reference 190 00600 04 Rev A Altitude is designated for use in giving vertical flight path guidance Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database The system cannot use this altitude in determining vertical flight path guidance Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 19 sjueumajsul UATE olpnyyuqax uo2 AEN Suelv uoneiedo s m SoJnpa204d buluueld unuuy Jeuuouqy Jeuonippy paezey Wfl x pu
29. TEMP COM2 over temp The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM 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 COM1 and or COM2 may still be usable The system should be serviced when possible 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 83 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V olpny uqax 7213 sjueumasu puezey BITTE UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy m x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck Comments The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cyde its operation If the problem persists the system should be serviced with other NAVS LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase of flight
30. The Category Box of the XM Radio Page displays the currently selected category of audio 1 2 3 Select the CATGRY Softkey on the XM Radio Page 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 Press the ENT Key Select an Available Channel within the Selected Category 1 2 3 While on the XM Radio Page select the CHNL Softkey 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 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 2 3 4 60 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Select the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Additional Features Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select the PRESETS Soft
31. aa a bab bada PFD Softkey Map sss MED Softkey Loading Updated Databases 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang iii Table of Contents GARMIN Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 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 Press the BARO Knob CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION Window 4 Tum the small FMS Knob clockwise to ON or counterclockwise to OFF SYNCHRONIZE CDI 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCH
32. activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang saunyea4 aoueplony saunpa20Jd Fuluueld ARN Sd5 2 olpny uqax Svo Sjueunasu paezey jeuonippy uoneiedo Jeuuouqy gt 5 o 2 x x pul ii UI0JNeN Wfi l4 Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments 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 XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The system sho
33. displaying data from the 1 Air Data Computer PFD1 is displaying data PFD2 is displaying data from the 1 AHRS PFD1 is displaying data from the 2 AHRS PFD2 is displaying data from the 1 GPS from the 2 GPS rom the 2 Air Data Computer PFD1 is displaying data Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations amp Alerts TAWS B ALERTS PFD MFD MFD Alert Type 1 TAWS B Page Aural Message s Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance Pull Up Warning RTC Imminent Terrain PULL UP Terrain Terrain Pull Up Impact Warning ITI Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance Up Pull Up Warning ROC Imminent Obstacle PULL UP Obstacle Obstacle Pull Impact Warning Up Pull Up 101 Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance Terrain Caution RTC Imminent Terrain TERRAIN CAUTION TERRAIN Caution Terrain Caution Impact Caution ITI Terrain Reduced Required TERRAIN OBSTACLE Caution Obstacle Obstacle Clearance Caution Obstacle Caution ROC Imminent Obstacle TERRA
34. small FMS Knob clockwise to display the Flight Plan Catalog Page 3 Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints 5 Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key 6 Repeat step numbers 4 and 5 to enter each additional flight plan waypoint 7 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 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 29 oipny uddx Sy2l3 Yid UI0JNeN 52 aoueplony paezey spay uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN IMPORT A FLIGHT PLAN FROM AN SD CARD 1
35. the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode Weather Alert To activate or deactivate Weather Alert select the WX ALRT Soltkey Activating and deactivating will also enable or inhibit the alert on the PFD Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode 54 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION OPTIONAL V ARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the a
36. 00 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 93 s m p q eo ueproAy SoJnpa204d Duruue d AEN 540 S24V oipny uadx 5721 sjueumasu puezey ubi UI05 AeN ubiu euonippv uoneiedo Jeuuouqy i PE x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message VNV Unavailable Parallel course selected Comments A parallel course has been selected causing the vertical deviation to go invalid NON WGS84 WPT Do not use GPS for navigation to xxx TRAFFIC FAIL Traffic device has failed The position of the selected waypoint xxxx is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint The system 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 GSD 41 GSD 69A or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles 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
37. 05 AEN S2dV AeN Sd5 Buruuejd 3 Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 38 A GARMIN 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 DEPARTURE LEG Activate leg using the Quick Select Box 1 Press the FPL Key on the MFD Control Unit to display the active flight plan 2 Use the Joystick to move the Quick Select Box to the TO waypoint of the desired leg within the departure 3 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 4 With ACTIVATE highlighted press the E
38. 2 3 4 5 6 7 8 Insert the SD card containing the flight plan in the top card slot on the MFD Press the FPL Key on the MFD Control Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn either FMS Knob to highlight an empty or existing flight plan Select the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again select the IMPORT Softkey Turn the small FMS Knob to highlight the desired flight plan for importing Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN Insert waypoint using the Quick Select Box 30 1 2 3 4 Press the FPL Key on the MFD Control Unit to display the active flight plan Use the Joystick to move the Insertion Point Indicator to the location for the new waypoint in the flight plan list Begin entering the identifier of the new waypoint using the MFD Control Unit s alphanumeric k
39. E o MFD Softkeys Level 1 Level 2 Description CAS 1 Scroll up Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling CAS Scroll down Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling MAP Enables second level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map PROFILE Displays removes Profile View on Navigation Map Page 106 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Appendix Level 1 Level 2 Description DCLIR 3 SHW CHRT 190 00600 04 Rev A TOPO TERRAIN AIRWAYS NEXRAD XM LING METAR LEGEND BACK 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 feature Displays XM lightning information on Navigation Map optional feature Displays METAR flags on airport symbols shown on the Navigation Map optional Displays the legend f
40. E FPM 750 es 750 1s 1990 O 89 2 Nzz 892 1500 OIL 1000 eeu 1000 Q 101 Psr 101 E 137 135 a FUEL 7500 5870 best ELV Q 300 LBS 300 E 5 0 DIFF PSI 530 PPH 530 Biss HEP GN 12 C 28 DC VOLTS 28 ze 245 DC AMPS 245 d BATT VOLTS 28 CABIN PRESS oz ALT FT 100 5 8 DIFF PSI 3 t FLAPS LAND EICAS Display Normal Mode EIS Display Reversionary Mode Z O Engine Fan Rotation 5 Interstage Turbine Cabin Pressure Altitude Speed Temperature and Change Rate 8 Oil Pressure amp Speed 5 1 High Pressure 2 Trim Indicator Turbine Rotation Fuel Display Speed Flap Indicator Electrical Display x pul CAS Display 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 5 A EcAS 008080 GARMIN CREW ALERTING SYSTEM CAS Flight Instruments A NOTE Refer to the Annunciations and Alerts section for specific CAS messages EICAS A NOTE Refer to the Airplane Flight Manual AFM for emergency z procedures ox NOTE If there is a mismatch between databases or software on the PFDs 0 CAS is inoperative When CAS messages are present while in reversionary mode the CAS Window appears on the display along with the flight instruments and EIS o m 22 zs CAS Window s CAS Display 5 XTALK ERROR A flight display crosstalk error has occurred GHC710 using T 8 backup data path zo s R ILC 85 Normal Mo
41. ENTER AN AIRWAY IN A FLIGHT PLAN Enter airway using the Quick Select Box 1 Press the FPL Key on the MFD Control Unit to display the active flight plan 2 Use the Joystick to move the Insertion Point Indicator to the desired entry point in the flight plan list 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sjuauimasu sub 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi eouepioAy 2 suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 32 3 4 5 6 7 8 A GARMIN Begin entering the identifier of the airway entry waypoint using the MFD Control Unit s alphanumeric keys The Waypoint Information Window is displayed as the identifier is entered Press the ENT Key The Quick Select Box and Insertion Point Indicator are now located following the newly entered waypoint Press the MENU Key and select Load Airway required on the PFD The Select Airway Page is displayed The Load Airway menu item is available only when an acceptable airway entry waypoint has been entered in step 3 the waypoint ahead of the Insertion Point Indicator Turn the FMS Knob to select t
42. ERTS Aural Alert Description Minimums minimums The aircraft has descended below the preset minimum descent altitude or decision altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Th e Traffic Information Service TIS has issued a Traffic Advisory alert TIS not available Th e aircraft is outside the Traffic nformation Service TIS coverage area not available when a TAS system is installed FLIGHT PLAN IMPO RT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Results Flight Plan Import Export Flight plan successfully imported Description A flight plan file stored on th mported as a stored flight p eS an D card was successfully User waypoints modified File contained user waypoints only imported success fully No stored flight plan data was system user waypoints No f have been modified The file stored on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the igh t plans stored in the system No flight plan files found to import The SD card contains no fligh tp an data Flight plan import failed 4 Flight plan data was not success ully imported from the SD card Flight plan partially imported
43. FMS Knob to select the System Status Page 12 The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed NOTE During the synchronization process version differences betvveen standby navigation databases will exist This will result in the system displaying a DB Mismatch alert for the standby navigation databases This alert will remain until the next power cycle 13 Turn system power OFF 14 Remove the SD card from the top card slot of the MFD 15 Turn system power ON 16 Press the ENT Key to acknowledge the startup screen 17 Turn the large FMS Knob to select the AUX Page group on the MFD 18 Turn the small FMS Knob to select the System Status Page 19 Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct standby navigation database cycle information is shown for each display 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 111 s n e 4 auepiony 2 Duruue d AEN Sd5 S24JV olpny uqax sv sjuauimasu jeuonippy 2 Wil Tuo2 NeN ibid uoneiedo Jeuuouqy Sue v unuuy kea Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Opera
44. G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Citation Mustang bre ki d A GARMIN Fax 4410870 8501251 Fax 886 02 2642 9099 orage m distribut n ground AOG technical support for Garmin panel mount n no part of this manual may be reproduced copied edium for any purpose ission of Garmin Garmin hereby grants permission to this manual onto a hard drive or ided that such evision must contain the complete text of this copyright electronic ion of this manual or any ubsidiaries WATCHS FliteCharts and Copyright O 2006 2011 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0435 23 or later for the Cessna Citation Mustang Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 040 9RB U K Tel 44 0870 8501241 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 For after hours emergency aircraft o and integrated avio
45. 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 SBAS 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 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair 6 51 FAIL G S1 is inoperative 6 52 FAIL G S2 is inoperative A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced
46. Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected displays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing Loading Garmin Database Updates 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the Garmin databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 108 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Appendix 4
47. IN CAUTION OBSTACLE Caution Obstacle Impact Caution 101 Caution Obstacle Premature Descent TERRAIN 100 0 TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Fve Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN mE Don t sink Rate Caution NCR 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 71 s m aoueplony SoJnpa204d Duruue d AEN 540 S24JV oipny uadx Svol3 sjueumasu puezey ubi U105 AEN BUTLER jeuonippy uoneiedo Jeuuouqy EY x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts GARMIN TAWS B System Status Annunciations Hu TAWS B Page Aural Alert Type Alert d ade Annunciation Message Annunciation ssentetinpoges Taus TEST EMEN ore TANS System System Test Pass None None Test OK TAWS Alerting is disabled TAWS INH None None MFD Terrain or Obstacle database unavailable or invalid None None TAWS operating with PFD Terrain or Obstacle databases TAWS B System Test Fail TAWS FAIL 77 Terrain or Obstacle database unavailable or invalid invalid TAWS System software configuration system TAMS FAIL Failure audio fault
48. Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 24 1 2 3 4 5 6 7 8 9 10 Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN
49. N 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 eg Large White 12400FT Text Insertion Large Light Point Blue Text Indicator Approach KDFW RNAY 17LGPsS LPY RIVET ief 7 Small Light Blue Text Quick Small Light Blue Subdued Text Small White Text with Altitude Restriction Bar SIUE Cross AT or ABOVE 5 000 fi Fac Cross AT 2 300 ft ICI Cross AT or BELOW 3 000 ft Altitudes associated with arrival and approach procedures are auto designated This means the system will automatically use the altitudes loaded with the arrival or approach for giving vertical flight path guidance outside the FAF Note that these altitudes will be displayed as small light blue text Altitudes that are designated for use in vertical navigation may 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 18 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04
50. N wb uoneiedo Jeuuouqy sue v unuuy ud ex GARMIN index Sjueuinijsu fila 5721 Tu102 AEN s24v AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey s s Jeuonippy uoneiedo jeuuouqy suay unuuy e E 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Index 4 GARMIN Garmin International nc 1200 Fast 151st Street Pe mo Olathe KS66062 USA p 913 397 8200 1 913 397 8282 Tt dn NET M 2345 Turner Road SE gt Salem OR 97302 USA E p 503 31 d 2006 2011 Garmin Ltd or its subsidiaries 190 00600 04 Rev A
51. NT Key Activate leg using the cursor 1 Press the FPL Key on the MFD Control Unit to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Procedures 39 sjueuimasu sub 5721 olpny uqax 0105 AEN 52 AEN 540 Duruue d nubi s mp old eouepioAy paezey spay uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 4 5 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 2 3 4 5 6 1 8 9 Press the PROC Key Turn the large FMS Knob to highlight SELECT ARRIVAL Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 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 displ
52. Pathways NOTE Pathways are not available when the cross pointer X Pointer flight director format is selected Press the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the PATHWAY Softkey Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 2 3 4 5 Press the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the HRZN HDG Softkey Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 2 3 4 5 56 Press the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the APTSIGNS Softkey Press the BACK Softkey to return to the previous page Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Md itinal Features TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary 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 T
53. Press the FMS Knob to remove the flashing cursor 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 25 sjuauimasu sub 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 26 1 2 3 4 5 6 7 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor i
54. RAPHICAL FLIGHT PLAN CREATION sjuauimasu Yid 1 Press the FPL Key to display the Active Flight Plan Page on the MFD 2 Use the Joystick to move the Insertion Point Indicator to the desired waypoint entry point in the flight plan list 5721 3 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 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 50 on oipny uddx UI0JNeN 52 5 To change the user waypoint name follow the procedure for modifying a user waypoint AEN Sd5 EXPORT A FLIGHT PLAN TO AN SD CARD 1 Insert the SD card into the top card slot on the MFD 2 Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to highlight the flight plan to be exported 6 Select the EXPORT Softkey 7 Press the ENT Key to confirm the export pu i8 SH ly uoneiado SoJnjeaJ eouepioAy saunpa20Jd unuuy jeuuouqy jeuonippy paezey xipuaddy x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 37 GARMIN Flight Planning Ssjueuinijsu fila 57213 oipny uadx U1
55. RONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 1 uonesado so1njeoJ uepjoay seinpa2oJd Buruuejg AEN 5649 24V oipny uadx svoli junuuy jeuuouqy paezey nubi xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES 1 Press 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 Press 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 Press the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Press the OBS Softkey to select OBS Mode 2 Turn the CRS Knob to select the desired course to from the waypoint Press the CRS Knob to slew the CDI Course Pointer to a course bearing directly to the waypoint 3 Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN fiel
56. Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct active navigation database cycle information is shown for each display Loading the Jeppesen Navigation Database as the Standby Navigation Database 1 2 3 4 5 7 8 9 10 NOTE After the navigation database is loaded or copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD Verify that an SD card is inserted in the bottom slot of each PFD and the MFD Turn the system ON A prompt is displayed Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD After the navigation database files are copied to the bottom SD card press any key to continue as instructed Again press any key to continue as instructed on the display Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting Press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Appendix 11 Turn the small
57. 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 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Hazard avoidance EnablelDisable Aviation Data 1 While the TAWS B 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 TAWS Inhibit A NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS 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 Pag
58. Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 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 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FliteCharts database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 79 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V olpny uqax 7213 sjueumasu piezeH 346 UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy FER x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Ad
59. Y or TA RA Softkey to begin displaying traffic TA RA or TA ONLY respectively is displayed in the TCAS Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode TFC STBY will be displayed in the TCAS Mode field 5 Select the ABS absolute or REL relative Softkey to display intruder altitude as an absolute altitude or an altitude relative to own aircraft altitude 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Changing the Altitude Range 1 On the Traffic Page select the ALT RNG Softkey 2 Select one of the following Softkeys ABOVE Displays non threat and proximity traffic from 9900 feet above the aircraft to 2700 feet below the aircraft Typically used during climb phase of flight NORMAL Displays non threat and proximity traffic from 2700 feet above the aircraft to 2700 feet below the aircraft Typically used during enroute phase of flight BELOW Displays non threat and proximity traffic from 2700 feet above the aircraft to 9900 feet below the aircraft Typically used during descent phase of flight UNREST unrestricted All traffic is displayed 3 To return to the Traffic Page select the BACK Softkey Displaying Traffic on the Navigation Map 1 Ensure TCAS II system is operating With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic will now be displayed o
60. abled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 66 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS CAS MESSAGES Messages Warning Caution 190 00600 04 Rev A Advisory Description Tailcone baggage door not fully secured Start control circuit breaker located in aft j box tripped C rent limiter blown located in aft j box Antiskid Control Uni cannot perform anti skid functions 0 erheated NiCad battery optional Battery temperature sensor failure Cabin altitude potentially unsa e Cabin door not fully secured A door monitor has not been pi operly tested or has failed Cockpit voice Recorder has failed Duc temperature too high or sensor disconnected Engi ne anti ice system ON and inlet temperature is cold FAD EC has a fault that requires maintenance An engine has failed DR FA Fue firewall shutoff valve fully closed Flight Data Recorder is not recording data A flap system failure has occurred Elec ric fuel boost pump ON Caution condition is displayed when the boost pump is operating in abnormal conditions in
61. ading sensors is 10 degrees s PITMISCOMP Difference in pitch sensors is gt 5 degrees X ROL MISCOMP Difference in roll sensors is gt 6 degrees 28 o data from one or both altitude sensors o data from one or both airspeed sensors i o data from one or both heading sensors o data from one or both pitch sensors F o data from one or both roll sensors de zz uoneiedo jJeuuouqv gt o 2 x x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 69 Fight EICAS Instruments Nav Com XPDR Audio Hazard Flight Features Avoidance Procedures Planning GPS Nav AFCS Additional Abnormal Operation Index Appendix Ea A Annunciations amp Alerts GARMIN REVERSIONARY SENSOR ANNUNCIATIONS 0 Reversionary Condition Sensor Window Text f Both PFDs are displaying data from the n mber one Air Data Computer f Both PFDs are displaying data from the n mber two Air Data Computer f Both PFDs are displaying data from the n Reference System mber one Attitude 8 Heading f Both PFDs are displaying data from the n Reference System mber two Attitude amp Heading Both PFDs are displaying data from the number one GPS receiver Both PFDs are displaying data from the number two GPS receiver PFD2 is
62. age MFD1 COOLING MFD1 has poor cooling Reducing power usage Comments The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 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 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the system shou
63. age 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 will be 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 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Additional Features 6 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 7 Press the FMS Knob when finished to remove the Chart Setup Menu AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check flygarmin com for the current database View
64. and 2 AHRS and Air Data Computers ADCI Selects the 41 Air Data Computer ADC2 Selects the 2 Air Data Computer AHRSI Selects the 1 AHRS AHRS2 Selects the 22 AHRS optional KE DNser SsENsoR ero OBS CDI LADF DME XPDR IDENT L TT IL IL L ws L Jw Lsa 1 optional optional ss Jw owe Tase ee se s 1 Select the BACK Softkey to return to the top level softkeys Lom OPTN2_ _OPTN3 Lor 1 1 1 Lvss 1 F3 V3 EN EN 75 EN EN ES n n onm PATHWAY SYN TERR HRZN HDG APTSIGNS BACK MSG F amp V3 V3 V3 V3 VN PN C3 P3 93 09 wn PFD Configuration Softkeys Level 1 Level 2 Level 3 Description PFD SYN VIS 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang PATHWAY 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 99 SoJnjeaJ e uepioAy 2 Duruue d AEN Sd5 241V oipny uddx sv l3 siu uinnsu jeuonippy 2 Wil Tuo2 NeN nubi uoneiedo Jeuuouqy Sue v unuuy z bud Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Inde
65. ant or make any representations regarding its accuracy reliability or otherwise Under no circumstances including negligence shall AOPA be liable for any incidental special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages User agrees not to sue AOPA and to the maximum extent allowed by law to release and hold harmless AOPA from any causes of action claims or losses related to any actual or alleged inaccuracies in the information Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you November 2011 190 00600 04 Rev A Printed in the U S A da GARMIN Frings Cautions amp Notes 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 di
66. ayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan ACTIVATE AN ARRIVAL LEG Activate Arrival using the Quick Select Box 40 1 2 3 4 Press the FPL Key on the MFD Control Unit to display the active flight plan Use the Joystick to move the Quick Select Box to the TO waypoint of the desired leg within the arrival Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key Activate Arrival using the cursor 1 2 Press the FPL Key on the MFD Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE Procedures NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches 1 Press the PROC Key 2 Tum the large FMS Knob
67. ce plays the latest recorded memory block and then returns to normal operation Pressing the PLAY Key again during play of a memory block stops play If a COM input signal is detected during play of a recorded memory block play is halted Pressing the PLAY Key twice within one half second while audio is playing plays the previous block of recorded audio Each subsequent two presses of the PLAY Key within one half second backtracks through the recorded memory blocks to reach and play any recorded block 10 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM 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 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 NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages 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 Button Roll Hold default ROL Pitch Hold default PIT Ta
68. contaminated schedule o power delivered to stal warning vane heater De ice boots inflating deflating as designed 2 probe heater failure ailcone temp high possible bleed air leak WIS FAIL L R W S O HEAT L R De ice system not operating normally Loss of power to windshield heater Windshield anti ice power ON temperature too high De ice system operating abnormally Gear on ground inputs do not agree display L R for example 68 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Only affected side displayed L R or L R in a CAS message applicable CAS messages listed here 190 00600 04 Rev A A GARMIN COMPARATOR ANNUNCIATIONS SjueuinJjsu Yid Note that operating the system in the vicinity of metal buildings or other metal structures can cause sensor differences that may result in nuisance miscompare annunciations during start up shut down or while taxiing m Comparator Condition Window Text 3 z Difference in altitude sensors is gt 200 ft 2 A f both airspeed sensors detect lt 35 knots this is inhibited f either airspeed sensor detects gt 35 knots and the difference insensorsis 2 15 kts f either airspeed sensor detects gt 80 knots and the difference in sensors is 10 kts 3 HDG MISCOMP Difference in he
69. cting BACK returns to the previous softkey level EF zer rss yarasa Ter TT Les osse nnnn nnnnnnn sjuauimasu sub 5721 olpny uqax uo2 AEN Selecting BACK returns to the z previous softkey level b osx BELO uses TT TE TT TsseTrsel FYENHENHN HUN Uu HMU UB 6 Selecting BACK returns to the previous softkey level 2 SS nnnnnnnunnnnun Selecting BACK returns to the previous softkey level Co L 2 125 L s L 7 Jes sss T Back T vse PS s n A nnn n5 o n5 n5 on Transponder Traffic Softkeys with TCAS II Option Duruue d Wil SeJnpa20Jd Ec Level 1 Level 2 1 Level 3 Level 4 Description 3 2 XPDR TFC Displays the transponder and TCAS II selection softkeys H 5 XPDRI Selects the 42 transponder as EH active me XPDR2 Selects the 2 transponder as ag active em MODE Displays transponder mode Sue v unuuy selection softkeys STBY Selects transponder Standby Mode transponder does not reply to any interrogations When the transponder is set to standby the TCAS TI system is also set to standby gt 5 x x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 103 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix _
70. curred in transferring data between the two GMAs The system should be serviced GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Config service req d The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMAT software mismatch communication halted MANIFEST GMA2 software mismatch communication halted The audio panel has incorrect software installed The System should be serviced 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 81 s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V olpny uqax 7213 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy Fw x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts A GARMIN GMA 1347D 1347D 20 MESSAGE ADVISORIES CONT Message GMAT SERVICE GMAT needs Service Return unit for repair GMA2 SERVICE GMA2 needs Service Return unit for repair Comments The audio panel self test has detected a problem in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Com
71. d is now highlighted 2 Turn the small FMS Knob to display the UP DOVVN 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 will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN light instruments 4 5 6 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey TURN VSPEED BUGS ON OR OFF BY CATEGORY 1 2 3 4 Press the TMR REF Softkey Press the MENU Key Turn the FMS Knob to highlight the desired option Press the ENT Key Press the TMR REF Softkey to remove the window SET BAROMETRIC RADAR ALTIMETER RA OPTIONAL MINIMUM DESCENT 1 2 3 4 5 6 1 ALTITUDE Press the TMR REF Softkey Turn the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of
72. de Reversionary Mode 25 Eu CAS Messages CAS MESSAGES Abnormal Operation NOTE Information on CAS messages in this pilot s guide is always superseded by the AFM Annun Alerts Warning red Immediate crew awareness and action required Master Warning triggered Caution yellow Immediate crew awareness and possible future corrective action required Master Caution triggered Advisory white Crew awareness required and subsequent action may be required Appendix Index 6 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPONDER AUDIO PANEL ENTER OR CHANGE FLIGHT ID 1 Press the TMR REF Softkey then turn the large FMS Knob to highlight the Flight ID field 2 Turn the small FMS Knob to enter the first character 3 Turn the large FMS Knob to select the next field 4 Tum the small FMS Knob to enter the next desired character 5 Repeat steps 3 and 4 until the desired Flight ID is entered 6 Press the ENT Key to update the Flight ID ADF TUNING OPTIONAL 1 Press the ADF DME Softkey 2 Turn the small FMS Knob to enter the first digit of the desired ADF frequency 3 Turn the large 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
73. dex Appendix A Appendix GARMIN Level 1 Level 2 Description 98 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 WXLGND Displays icon and age on the Inset Map for the selected weather products optional 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 coastlines ter rain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map not available with TAWS A NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XMLING Displays XM lightning information on Inset Map optional feature METAR Displays METAR flags on airport symbols shown on the Inset Map optional optional Treer SENSOR os5 T cor aoe xe08 T ven russe wesr T vss EY EY EY EY EN EN S EY n Press the BACK Softkey to return to the top level softkeys n rv m uu m SENSOR Softkeys Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Level 1 Level 2 Description SENSOR Displays softkeys for selecting the 1
74. ditional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Navigation database mismatch Xtalk is off Comments The PFDs and MFD have different navigation database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Standby Navigation database mismatch The PFDs and MFD have different standby navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch The PFDs and MFD have different terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Obstacle database mismatch The PFDs and MFD have different obstacle database versions or regions installed Check the AUX SYSTEM STATUS Page to de
75. e ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Hazard Avoidance 4 AEN 640 S24V oipny uddx svn siu umnnsul Tuo2 AEN iui Duruue d nubi e uepioAy s mp oold paezey SH V uoneiedo SaJnjeoJ Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 48 System Self Test 1 With the Traffic Map Page displayed set the range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert TAS System Test OK is heard If the self test fails the system reverts to Standby Mode and a voice alert TAS System Test Fail is heard Displaying Traffic on the Navigation Map 1 Ensure TAS i
76. e Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message Comments HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is SBAS capable MANIFEST G A1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect MANIFEST COM1 software mismatch communication halted MANIFEST 2 software mismatch communication halted COM1 and or COM2 software mismatch The G1000 system should be serviced MANIFEST NAV1 software mismatch communication halted MANIFEST NAV2 software mismatch communication halted NAV1 and or NAV2 software mismatch The G1000 system should be serviced COM1 CONFIG COM1 config error Config service req d COM2 CONFIG COM config error Config service req d COM1 and or COM2 configuration settings do not match backup configuration memory The G1000 system should be serviced COM1 TEMP COM over temp Reducing transmitter power Reducing transmitter power COM2
77. e error exists PFD1 DB ERR PFD1 obstacle database error exists PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU 78 Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists Comments 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 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe
78. e fuel filter impending bypass switch closed low level function failure level in tank is too low pressure too low Fuel transfer valve open One or both electrical generators offline Hydraulic system pressure too low Hydraulic pump running too long FD temperature is below 20 C One or both nose baggage doors not fully secured Antiskid control spindown function not working Oil pressure less than redline low limit Oxygen supply off Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 5721 UI0 eN 52 So1nje2J eouepioAy s mp oold Buruue d AEN Sd5 jeuonippyv uoneiedo jJeuuouqv gt o 2 x x pul iui nu paezey Flight Instruments Nav Com XPDR Audio Flight Planning Additional Hazard Avoidance Abnormal EICAS AFCS GPS Nav Procedures Features Operation Appendix Index Annunciations amp Alerts A GARMIN Messages Warning Caution Advisory P S HTR L R PRESS CTRL PRESS OFF SPD BRK EXTEND STALL WARN HI SURFACE DE ICE Description o current detected to pitot static heater Pressure controller loss of integrity Air Source Selector switch in OFF or fresh air position Speed brakes extended Failure detected in stall warning system Stall warning sys em on ice
79. e is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacles will now be displayed on the map 3 Terrain and obstacles may be displayed in the Profile View by selecting the PROFILE Softkey 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 5 AEN Sd5 S24V oipny uadx svn siu umnnsul Tuo2 AEN iui Duruue d nubi e uepioAy s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN AIRBORNE COLOR WEATHER RADAR WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar Page
80. e other sides COM or NAV For example if the pilot side Audio Panel 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 63 eouepioAy Senpa204d Buruue d ARN Sd5 S23V olpny gqax swola 5349 411115 puezey ubi U105 AEN ubiu soJnjeoJ jeuonippy xipuaddy suelv junuuy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EICAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation GARMIN fails the copilot side Audio Panel has access to all the radios except for COMI and NAVI In this case the copilot can receive the audio from NAV2 and operate COM2 for transmission reception In addition if there is a failure of one Audio Panel the following functions are no longer available on the failed side NAV ILS audio speaker cockpit cockpit passengers intercom aural warning alerts on headset entertainment inputs and digital recording radio Also if a stereo headset is in use and an Audio Panel fails only the left channel will be heard in the headphones 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 Loss of Hazard Functions with Loss of GPS Position UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual a
81. en scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Bearing Line 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain o WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN field 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position 3 Press the FMS Knob to remove the c
82. ered the transponder code becomes active SELECT TRANSPONDER MODE With TCAS II Option 1 2 3 Press the XPDR TFC Softkey Press the MODE Softkey to display the transponder mode selection softkeys Press the desired transponder mode softkey STBY ON or ALT Without TCAS Il Option 1 2 3 Press the XPDR Softkey If the aircraft is equipped with two transponders press the XPDR1 or XPDR2 Softkey to select the active transponder Press the desired transponder mode softkey STBY ON ALT or GND SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key if installed on the audio panel Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A E GARMIN Nav Com XPDR 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 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 2 Press the appropriate Frequency Transfer Key to place the frequency into
83. ess the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD Control Unit and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor c Turn the large FMS Knob to highlight the desired flight plan d Press the EDIT Softkey 2 Tum the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window 4 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 5 When all changes have been made press the FMS Knob to remove the cursor 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 35 olpny uqax Sy2l3 sjueuinasu U10 AEN ubiu 52 2 AEN 540 nubi eouepioAy paezey suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD Control Unit 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Tur
84. et below the aircraft Typically used during descent phase of flight UNREST All traffic is displayed TEST Activates Test Mode and displays test intruder symbols BACK Returns to the previous softkey level Displays transponder code selection softkeys 0 7 0 7 Use numbers to enter code IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen BKSP 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 105 sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV oipny uddx sv l sjuauimasu jeuonippy 2 nf Tuo2 NeN Yid uoneiedo Jeuuouqy Sue v unuuy z b Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN Level 1 Level 2 Level 3 Level 4 Description TMR REF Displays Timer References VVindovv NRST Displays Nearest Airports VVindovv MSG Displays Messages VVindovv MFD SOFTKEY MAP Fs 3 T 7 D Select the BACK Softkey on this level to return to the top softkey level optional optional C Lexan xure vero ecen 1 EY ES V3 V3 V3 D
85. eys The Waypoint Information Window is displayed as the identifier is entered Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Insert waypoint using the cursor 1 Press the FPL Key on the MFD Control Unit to display the active flight plan 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to move cursor and Insertion Point Indicator small light blue triangle to the desired insertion point in the flight plan The new waypoint is inserted before the highlighted waypoint 4 Turn the small FMS Knob The Waypoint Information Window is now displayed 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or Flight Planning 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 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 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
86. f VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude Pitch Hold may be used to climb descend to the default PIT Selected Altitude AFCS armed to capture the altitude 701 displayed in the Selected Altitude ALTS Armed window Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn Fr Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key VS nnnn Fem to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed BE s de IAS Hold in IAS or Mach while the aircraft is A FLC Key Flight Level Change dimbing descending to the Selected Mach Hold Altitude te Man VNAV Captures and tracks the VNAV flight VNV VPTH path Key AFCS armed to capture the altitude VNAV Target i Amas Arad disp ayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath GP on approach Captures and tracks the ILS glideslope P e Glideslope aptures and tracks the ILS glideslope GS on approach Commands a constant pitch angle Takeoff and wings level on the ground in TO preparation for takeoff GA Disengages the autopilot and Switch Go Around commands a constant p
87. field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system 8 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 9 Theflashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page 10 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 11 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 12 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 13 The flashing cursor moves to the air temperature TOTAL AIRTEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the
88. he FPL Key Begin entering the identifier of the departure waypoint using the MFD Control Unit s alphanumeric keys The Waypoint Information Window is displayed as the identifier is entered Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN ri htrinning 3 Press the ENT Key The Quick Select Box moves to the next empty field 4 Repeat steps 2 and 3 to enter each additional flight plan waypoint The active flight plan is modified as each waypoint is entered Creating an active flight plan using the cursor 1 Press the FPL Key 2 Press the FMS Knob to activate the cursor only on MFD 3 Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints 4 Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered 5 Repeat step numbers 3 and 4 to enter each additional flight plan waypoint 6 When all waypoints have been entered press the FMS Knob to remove the cursor SoJnpa20Jd buluueld AEN Sd5 nubi Creating a stored flight plan 1 Press the FPL Key 2 Tum the
89. he Joystick to move the Quick Select Box around the desired procedure name or airway in the flight plan 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 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 33 s tin sul Yid 5721 olpny uqax 0105 AEN 52 2 AEN 540 nubi eouepioAy paezey Suelv uoneiedo s n e 4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN Remove using the cursor 1 2 3 4 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 Control Unit and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor c Turn the large FMS Knob to highlight the desired flight plan d Press the EDIT Softkey 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 Press the CLR Key to display a confirmation window With
90. he 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 ID the VOR symbol 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 provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView Optional 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 Subscription Optional FliteCharts resemble the paper version of AeroNav Services te
91. he 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 inserted Enter airway using the cursor 1 2 3 4 5 6 Press the FPL Key on the MFD Control Unit Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to move the cursor and Insertion Point Indicator small light blue triangle to the desired waypoint insertion point in the flight plan 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 press the LD AIRWY Softkey or press the MENU Key and select Load Airway required on the PFD 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 p
92. he system should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX 68 configuration settings do not match those of the GDU configuration The system should be serviced GWX FAIL GWX is inoperative The GDU is not receiving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair MANIFEST GWX software mismatch communication halted A failure has been detected in the GWX 68 The GWX 68 may still be usable The GWX 68 has incorrect software installed The system should be serviced WX ALERT Possible severe weather ahead GDC 74B MESSAGE ADVISORIES Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm Message Comments ADC1 ALT EC ADCI altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude error correction is unavailable 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 89 Sonje24 aoueplony s mp oold Buruue d AEN Sd5 2 oipny uddx sv l3 sjueumasu paezey nubi jeuonippy uoneiedo Jeuuouqy EY x pul Hazard Flight Nav Com Flight Features Avoidance
93. ion database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired 190 00600 04 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang saunqea4 sanpa20Jq Buruuejd AEN 5640 24V olpny uqax svoli sjuaum sul paezey nubi u102 AEN nubi jeuonippy uoneiedo Jeuuouqy iue EY x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Verify user modified procedures DB CHANGE Database changed Comments This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after a navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date Verify stored airways DB CHANGE Database changed This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after a navigation database update Verify use of airways in stored flight plans and reload airways as needed FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database eliminates an obsolete appr
94. ircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVS enhancement to the PFD the following feature enhancements 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 Synthetic Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 55 s mp o4d Buruuejd AeN Sd5 S24V oipny uadx sola s u u nnsul Tu102 AEN 346 eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features Displaying Pathways 1 2 3 4 5 A GARMIN NOTE When the optional TCAS Il system issues a Resolution Advisory RA Pathways are automatically removed from the display Pathways may again be displayed by the pilot manually selecting
95. is operating exclusively in no GPS mode The system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 87 s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V oipny uadx 7213 sjueumasu piezeH ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy iuc 1 x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 122 Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message AHRS1 SRVC AHRS1 Magnetic field model needs update Comments The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 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 GEO LIMITS AHRS2 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 system should be
96. is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the system utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the system 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 Citation Mustang Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the system 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A da GARMIN Warnings Cautions 5 Notes V ARNING The illustrations in this guide are only examples Never use the system to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws F
97. itch angle and GA wings level in the air ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude 190 00600 04 Rev A A GARMIN wings level in the air AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle Low Bank Limits maximum commanded roll angle je HDG Heading Select Captures and tracks Selected Heading Key HDG Navigation GPS GPS Arm Capture Track Navigation VOR Enroute Arm Captures and tracks selected navigation NAV VOR Capture Track source GPS VOR LOC Key Navigation LOC Arm Capture Track LOC No Glideslope Am Captures and tracks a localizer signal BC Key BC Capture Track for backcourse approaches Approach GPS Arm GPS Capture Track Approach VOR Arm VAPP Capture Track Captures and tracks selected navigation APR Ke Approach 15 Arm source GPS VOR LOC Capture Track Glideslope Mode LOC automatically armed Commands a constant pitch angle Takeoff and wings level on the ground in TO preparation for takeoff GA Disengages the autopilot and Switch Go Around commands a constant pitch angle and GA No annunciation a 7 green along the Ro 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
98. ity Added database synchronization 190 00600 04 Added GDU 12 02 parameters Added Profile View Added MV DB update procedure Updated Database update procedures Updated XM WX weather product symbols Flight Plan Enhancements November 2011 Production Release 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang RR 1 Record of Revisions GARMI Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Tableof Contents cette 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure s s s si s sil 1 Change Altimeter Barometric Pressure Setting Units 1 Synchronizing the Altimeter Barometric Pressure Settings 1 Synchronize CDI ue eee ener ee ao e HER 1 Change Navigation Sources sssssssssseennnnennnnns 2 Enable Disable OBS Mode While Navigating with 6 5 2 GenericTimer aeos ono nn De RO HU Rm ne Ga 2 Configure Vspeed Bugs Individually sss 2 Turn Vspeed Bugs On or Off by Category 3 Set Barometric Radar Altimeter RA Optional Minimum Descent Altitude 3 Displaying Wind Data 3 ENGINE INDICATION amp CREW ALERTING SYSTEM
99. ivation of reversionary display mode is accomplished by pressing the DISPLAY BACKUP Button on the appropriate audio panel e PFDI By pressing the DISPLAY BACKUP Button on the left audio panel e MED By pressing the DISPLAY BACKUP Button on the left or the right audio panel PFD2 By pressing the DISPLAY BACKUP Button on the right audio panel NOTE The Cessna Citation Mustang 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 In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios AUDIO PANEL FAIL SAFE OPERATION If there is a failure of both Audio Panels a fail safe circuit connects the pilots headset and microphone directly to the COMI transceiver and the copilot headset directly to the COM2 transceiver Audio is not available on the speakers If there is a failure of one Audio Panel that side only has access to their respective on side fail safe COM NOTE Audio is not available on the speakers in case of an Audio Panel and its cross side GIA unit simultaneous failure If there is a failure of one Audio Panel the remaining Audio Panel does not have access to th
100. jeuuouqy Jeuonippy paezey nubi xipuaddy x pul Abnormal Additional Hazard Annun Flight Instruments Flight Planning Nav Com AFCS XPDR Audio EICAS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN CLEARANCE RECORDER AND PLAYER GMA 1347D NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC Record 1 Press the REC Key to begin recording 2 Press the REC Key again to stop recording Play 1 Press the PLAY Key once to play the latest recorded memory block 2 Press the PLAY Key once while playing to stop 3 Press the PLAY Key twice quickly while playing to begin playing the previously recorded block Each subsequent two presses will skip back to the previously recorded block GMA 1347D 20 NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot COM audio is recorded automatically Recorded audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the stored memory blocks starting from the oldest block The PLAY Key controls the play function The PLAY annunciator is illuminated to indicate when play is in progress The PLAY annunciator extinguishes after playback is finished Pressing the PLAY Key on
101. keoff on ground TO Takeoff on ground TO Go Around GA Go Around GA 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 VOR 1 Pitch Hold default PIT LOC BC Key Backcourse BC Pitch Hold default PIT GPS Pitch Hold default PIT APR Key Approach VOR 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 ux ps selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 11 svol4 siu umnsul nubi olpny uqax uo2 AEN ARN Sd5 52 suelv uoneiedo s n e 4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey n xipuaddy x pul Flight nstruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A GARMIN 12 is to be captured instead o
102. key to access the first five preset channels PS1 PS5 2 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 3 Select any one of the PS1 PS15 softkeys to assign a number to the active channel 4 Select the SET Softkey on the desired channel number to save the channel as a preset 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 61 xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV oipny uddx SV2l3 sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi u05 AeN ubiu x pul GARMIN itional Features Add Sjueuinijsu fila sv l4 olpny uddX U105 AEN 52 AeN 5492 4 r Blank Page 6 2 4 aoueplony puezey s l Jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 62 GARMIN Abnormal operation ABNORMAL OPERATION REVERSIONARY MODE If the system detects a failure in the MFD PFD1 will enter reversionary mode automatically Reversionary mode must be entered manually in the case of PFD1 or PFD2 failure In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Manual act
103. ld be serviced 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 7 soJnjeoJ 2 4 AEN Sd 24V oipny uadx svoli s u un su paezey nubi Juo ney Wil euonippv uoneiedo Jeuuouqy PE x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix ud Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap database error exists Comments The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists 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 system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle databas
104. ll other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the ovm 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 The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored t is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of 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 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 65 aoueplony seunpe
105. 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 message Message criteria entered by the user CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees 94 PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang The SD card was removed from the top card slot of the specified PFD or MFD The SD card needs to be reinserted 190 00600 04 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message PFD1 PFD2 or MFD1 CARD 2 REM Card 2 was removed Reinsert card Comments The SD card was removed from the bottom card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid PFD1 PFD2
106. mation 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 system are found in the G1000 Integrated Flight Deck Pilot s Guide Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Fesord f Hevislans Change Summary 190 00600 00 RevA Initial release Rev B Added Additional Features section 190 00600 01 Rev A Production release Rev B Added CAS INOP system messages Rev C Added COM 3 function for HF Added TAS Removed automatic Reversionary Mode operation 190 00600 02 RevA Added Synthetic Vision Added other GDU 9 01 parameters 190 00600 03 Added GDU 10 01 parameters Added GSD 41 Added GMA 20 Added new page navigation TCAS Il Radar Altimeter Added AOPA Airport Directory Added dual navigation database capabil
107. ments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The G A1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced GIA1 CONFIG GIA1 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 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 correctly 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 system should be serviced GIA1 SERVICE G A1 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 system should be serviced G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible 82 Garmin G1000 Cockpit Referenc
108. ments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 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 ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 2 3 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE APPROACH Press the ENT Key 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 1 2 3 4 42 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 button Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN 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 Me
109. n the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Tum the small FMS Knob to the right to display the NRST airports to the aircraft s current position Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN ight Planning 11 1 2 o d Or a b o d Or a b 4 Tum the large FMS Knob to select the desired vvaypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoi
110. n the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan is displayed 6 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 COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD Control Unit 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 select the COPY Softkey A Copy to flight plan 4 confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the MFD Control Unit 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Select the DELETE Softkey A Delete flight plan 19 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 36 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Flight Planning G
111. n the map 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Hazard Avoidance 49 AEN Sd5 S24V oipny uddx 5219 sjuauimasu Tuo2 AEN sub Duruue d nubi s mp oold paezey SH V uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN TERRAIN AWARENESS amp WARNING SYSTEM TAWS B 50 WARNING The TAWS display shows supplemental information only It should not be used for navigation NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area NOTE TAWS operation is only available when the system is configured for a TAWS B installation Manual System Test 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS System 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 and Obstacles on the TAWS B Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS B Page If desired select the VIEW
112. nfig service req d The transponder configuration settings do not match those of backup configuration memory The system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The system should be serviced MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair XPDR2 SRVC XPDR2 needs service Return unit for repair The 1 transponder should be serviced when possible The 2 transponder should be serviced when possible XPDR1 FAIL 1 is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder 86 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN GRS 77 MESSAGE ADVISORIES Annunciations amp Alerts Message AHRS1 TAS AHRS1 not receiving valid airspeed Comments 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 system should be
113. nics systems please contact Garmin s AOG Hotline at 913 397 0836 Web Site Address www garmin com Except as expressly provided herei transmitted disseminated downloaded or stored in any st without the express written perm download a single copy of this manual and of any revision to other electronic storage medium to be viewed for personal use prov or printed copy of this manual or notice and provided further that any unauthorized commercia revision hereto is strictly prohibited Garmin is a registered trademark of Garmin Ltd or its s SafeTaxi are t NavData is a of L 3 Co Inc Honeywel AOPA Membe permission of Garmin egist mmunications and Si and Bendix Ki CO Guardian is a trademark of ship Publications Inc and AOPA expressly disclaim all warranties wi ered trademark of Jeppesen Inc St riusXM is a ng are regist CO Guardian Inc egistered t ademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express ormscope is a registered trademark ademark of SiriusXM Sat ered trademarks of Honeywell International Inc ellite Radio its related organizations hereinafter collectively th respect to the AOPA information included in this data express or implied including but not limited to the implied warranties of merchantability and fitness for a particular purpose The information is provided as is and AOPA does not warr
114. nts Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor CREATE A USER WAYPOINT USING THE MAP POINTER Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint Press the ENT Key The User Waypoint Information Page is displayed with the captured position NOTE If the pointer has highlighted a map database feature one of three things happens upon pressing the ENT Key 1 information about the selected feature is displayed instead of initiating a new waypoint 2 a menu pops up allowing a choice between Review Airspaces or Create User Waypoint or 3 a new waypoint is initiated with the default name being the selected map item 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 2 sjuauimasu nubi 5721 olpny uqax 0105 AEN 52 2 AEN 540 nubi eouepioAy paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal An
115. nu 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 display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page XM WX SATELLITE WEATHER SUBSCRIPTION OPTIONAL WARNING Do not use datalink weather products e g XM WX Satellite Weather GFDS World Wide Weather or FIS B for hazardous weather penetration Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear Displaying XM WX 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 produc
116. nun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN 3 Enter a user waypoint name up to six characters 4 Press the ENT Key to accept the selected name 5 If desired define the type and location i e LAT LON RAD RAD or RAD DIS of the waypoint 6 Press the ENT Key to accept the new waypoint 7 If desired change the storage method of the waypoint to TEMPORARY or NORMAL by moving the cursor to TEMPORARY and selecting the ENT Key to check or uncheck the box 8 Press the FMS Knob to remove the flashing cursor 9 Press the GO BACK Softkey to return to the map page DELETE A 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 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 FLIGHT PLAN 28 NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan using the Quick Select Box MFD only 1 2 Press t
117. oach 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 Arriving 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 92 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message ARSPC NEAR Airspace near less than 2 nm Comments Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active SLCT FREQ Select appropriate frequency for approach The system notifies the pilot that the loaded approach is not active Acti
118. oint from the list and press the ENT Key LOAD is highlighted Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN 7 Press the ENT Key The system returns to editing the flight plan with the new airway inserted only when an acceptable airway entry waypoint has been entered in step 3 the waypoint ahead of the Insertion Point Indicator Flight Planning 6 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 7 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted 8 Press the ENT Key The system returns to editing the flight plan with the new airway inserted INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 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 Remove using the Quick Select Box active flight plan only 1 Press the FPL Key on the MFD Control Unit to display the active flight plan 2 Use t
119. ojd AEN 540 5247 oipny uddx sv l3 siu u nsul n Tuo2 NeN paezey saunqee4 jeuonippy Sue v unuuy xipuaddy x pul sub Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EICAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation GARMI N DR Mode is inherently less accurate than the standard GPS SBAS 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 position awareness using other navigation equipment until GPS derived position data is restored CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following 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 Current 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 couple to GPS for up to 20 minutes TAWS is also dis
120. or more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed 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 sys
121. or the selected weather products Available only when NEXRAD XM LTNG PROFILE and or METAR softkeys are selected Returns 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 active flight plan When available displays optional airport and terminal procedure charts Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 107 saunqea4 aDueplony seinpo2o0Jd Buruuejg AEN 5649 S24V oipny uadx svoli sjuaum su jeuonippy paezey 14614 Wil uoneiedo Jeuuouqy Sue v unuuy m bud Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix LOADING UPDATED DATABASES A GARMIN A CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in main tenance being required to reboot the system A NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page In some cases it may be necessary to obtain an unlock code from
122. oystick to place the Quick Select Box on the destination waypoint for the desired leg Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN GPS Navigation 3 Press the ACT LEG Softkey MFD only or press the MENU Key highlight Activate Leg and press the ENT Key A confirmation window is displayed with ACTIVATE highlighted 4 Press the ENT Key to activate the flight plan leg To cancel press the CLR Key or highlight CANCEL and press the ENT Key 5 Press the FMS Knob to remove the flashing cursor if required STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 17 sjuauimasu nubi 5721 oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey n xipuaddy x pul Flight Instruments Nav Com XPDR Audio EICAS Abnormal Additional Hazard Annun Flight Planning Appendix Alerts Operation Features Avoidance Procedures Index A GPS Navigation GARMI
123. peration Appendix Index Annunciations amp Alerts 96 Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A GARMIN 190 00600 04 Rev A GARMIN 88 Appendix APPENDIX sjuauimasu wp PFD SOFTKEY MAP optional Jer Jeenson ro T oss ore 908 oer REA wes IS r r r S rv um uu HN 5721 CDI NAV1 olpny uqax U105 AeN x Top Level PFD Softkeys e optional TCAS II optional TCAS II z TRFC MAP optional ET ser EE vro T 955 T cor urine arr oe russe wes SS n EY EY x mun s buluueld wold optional optional optional optional mm EV FX EX 3 o m 8 LA F N V3 V3 V3 v v m amp DCLTR 1 LE Select the BACK Softkey to return s Y to the top level softkeys E 8 INSET Map Softkeys ze 8 Level 1 Level 2 Description INSET or Pressing the INSET Softkey Displays Inset Map ae TRFC MAP in the PFD lower left corner The TRFC MAP 2 Softkey is displayed when the TCAS II option is installed Pressing the TRFC MAP Softkey displays the Inset Map showing Traffic Map Page Sue v unuuy OFF Removes Inset Map gt s o m x x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 97 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts In
124. point 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 Press the ENT Key to accept the waypoint For flight plan leg planning a b o d Select the FPL Softkey at the bottom of the display Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps 5 Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Flight Planning 6 Enter the departure time Press the ENT Key vvhen finished Departure time may be entered in local or UTC time depending upon system settings 7 The flashing cursor moves to the ground speed GS
125. press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure When the upload is complete the system is ready for use Uploading GRS2 Mag Var Database STARTING UPLOAD 0 0 Uploading Database to GRS2 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 113 saunqee4 2 Buruuejg AEN Sd5 S24V oipny uadx svoli siu un sul Jeuonippy paezey nubi UI05JNeN 146114 uoneiedo Jeuuouqy Sue v unuuy a k GARMIN Appendix Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 114 A GARMIN A Activate a flight plan 16 Active Channel 59 Active database 109 Active Navigation Database 109 ADF 7 9 AHRS 70 87 88 99 112 AIREP 45 AIRMET 44 45 Airport Signs 55 56 Airways 107 Air Data Computer 70 Alert messages 89 ALT 47 Altimeter setting 1 Altitude mode 47 Altitude volume 47 Antenna stabilization 54 Antenna tilt 52 AOPA s Airport Directory 59 Attitude amp Heading Reference System 70 Audio Panel 63 Audio panel controls NAV1 NAV2 9 Barometric Altitude Minimums 3 Barometric pressure 101 Bearing line 53 54 C Cabin pres
126. r copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 PFD2 or MFD to be updated label of SD card facing left Turn the system ON A prompt is displayed in the upper left corner of the display Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 109 sainjea4 aoueplony 2 Duruue d AEN Sd5 24JV oipny uddx sY213 sjuauimasu jeuonippy 2 Wil JUI0 NEN BUT uoneiedo Jeuuouqy Sue v unuuy m k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN 110 5 6 8 9 10 11 After the update completes the display starts in normal mode Tum the system OFF and remove the SD card from the top card slot Repeat steps 1 through 6 for the other displays PFD1 PFD2 or MFD Apply power to the system and press the ENT Key to acknowledge the startup Screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database
127. rminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 57 seapeooid Buluueld AEN 540 S24Y oipny uadx svolti syueumasul uo2 AEN eouepioAy paezey s n ze 4 jeuonippy uoneiedo Jeuuouqy Sue v unuuy xipuaddy x pul iui nu Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 58 A GARMIN 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 expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 2 3 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 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 Select the GO BACK Softkey to return to the previous page View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan P
128. rnal error condition The GSD may still be usable GSD1 has incorrect software installed The mismatch Communication halted system should be serviced 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 85 sainqea4 s mp oold Buruue d AEN Sd5 yi oipny uddx sv l3 sjueumasu paezey ETSI u102 NEN nubi jeuonippy uoneiedo Jeuuouqy ic PET x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix ond Annunciations amp Alerts GEA 71 MESSAGE ADVISORIES A GARMIN Message Comments GEA1 CONFIG GEA1 config error Config service req d GEA2 CONFIG GEA2 config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The system should be serviced The GEA2 configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GEA1 software mismatch communication halted MANIFEST GEA2 software mismatch communication halted The 1 GEA 71 has incorrect software installed The system should be serviced The 2 GEA 71 has incorrect software installed The system should be serviced GTX 33 33D MESSAGE ADVISORI ES Message Comments XPDR1 CONFIG XPDR1 config error Co
129. s operating 2 With the Navigation Map displayed select the MAP Softkey 3 Select the TRAFFIC Softkey Traffic is now displayed on the map Traffic Collision Avoidance System TCAS II Optional NOTE If the system is configured to use TIS the optional TCAS l is not available for use System Test 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the TEST Softkey The aural annunciation TCAS Test will be heard A test pattern of traffic symbols is displayed on the Traffic Page and inset map on the PFD The VSI will display a red no descent indication and a green climb indication of 2000 feet per min and red from 2000 to 4000 The pitch display will also display the appropriate indications appropriate with the VSI The self test takes approximately eight seconds to complete after which a voice alert TCAS Test Passed is heard In the event the system test fails a voice alert TCAS Test Failed is heard and a visual annunciation TCAS FA L appears on the PFD In addition a visual annunciation FAIL appears in the Operating Mode box on the Traffic Map Page Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN 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 TA ONL
130. serviced AHRS2 TAS AHRS2 not receiving valid airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS2 GPS AHRS2 using backup GPS source The 2 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS2 GPS AHRS2 not receiving any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS
131. serviced MANIFEST GRS2 software mismatch communication halted The 2 AHRS has incorrect software installed The system should be serviced GMU 44 MESSAGE ADVISORIES Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The system should be serviced 88 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 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 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed T
132. splayed 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 the GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B 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 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the 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 Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories if installed ATC guidance or positive visual acquisition of conflicting traffic 190 00600 04 Rev A Garmin G1000 Cockpit Reference G
133. sure altitude 5 CDI 1 2 9 93 Channel Presets 61 ChartView 57 Clearance player 10 Clearance Recorder 10 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Code selection softkeys 8 COM 8 9 10 63 Crew Alerting System CAS Messages 6 7 D DB Mismatch 108 111 DCLTR Softkey 57 Dead Reckoning 65 Declutter 64 98 107 Designated altitudes 18 19 Direct to 15 DME 7 9 DR mode 65 66 E Edit a flight plan 34 Engine display 5 F Flight Director 11 Flight ID 7 Flight path marker 55 FliteCharts 57 Frequency Transfer 9 G Gain 53 H Horizon heading 55 Horizontal scan 53 Inhibit 51 Inhibit TAWS 51 Inset Map 97 98 Intercom isolation 9 IOI 71 Index Index 1 sainjea4 eouepioAy SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sY213 sjuaumasu jeuonippy 2 nubi Tuo2 NeN wb uoneiedo Jeuuouqy sue v unuuy 1221 ow Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts El Appendix Index J Jeppesen 57 M Magnetic Field Variation Database 112 113 Map panning 44 Message advisories 76 95 METAR 43 44 45 98 107 Minimums 74 MISCOMP 69 Mode 5 102 Multi Function Display MFD Softkeys 106 N NAV 9 NAV1 2 9 NAV2 2 9 Navigation database 18 19 75 77 91 92 NEXRAD 43 98 107 0 OBS 2 Obstacles 80 81 83
134. system outside air temperature CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the MFD Control Unit 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 Enterthe desired waypoint name 5 Press the ENT Key 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 23 sjuauimasu sub 5721 oipny uddx UI0JNeN 52 SoJnpa20Jd AEN 540 nubi eouepioAy 2 suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS
135. t 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 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 43 AEN 540 S24V oipny uddx svo siu umnnsul Tuo2 AEN iui Duruue d wold s mp oold paezey SH V uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Map Panning Information Weather Data Link Page 1 2 3 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARs SIGMETs PIREPs or AIREPs 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 Enabling disabling winds alof
136. t data display in Profile View 1 2 3 4 5 6 7 Select the Navigation Map Page Press the MENU Key With Map Setup highlighted press the ENT Key Turn the small FMS Knob to select the Profile Group and press the ENT Key Turn the large FMS Knob to select Profile Winds Turn the small FMS Knob to select On or Off Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings NOTE NEXRAD data cannot be displayed at the same time as terrain echo tops turbulence or icing data is displayed XM WX Satellite Weather Products and Symbols Wx Product Status Icons Description US cin NEXRAD Available for the US and Canada The age of the displayed data CN 271 for each is shown at the right ECHO TOP The age of the displayed data is shown at the right Not adi om displayed when CLOUD TOP is displayed 12 CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed 44 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Hazard Avoidance Wx Product Status Icons Description XM LIGHTNING The age of the displayed data is shown at the right CELL MOVEMENT The age of the displayed data is shown at the right SIGMET amp AIRMET The age of the displayed data for each is shown at the right METAR Available for
137. tem 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 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A Wamings Santions Notes GARMIN NOTE All visual depictions contained within this document including screen images of the panel and displays are subject to change and may not reflect the most current system and databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The 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 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 infor
138. termine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 80 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Airport Terrain database mismatch Comments The PFDs and MFD have different airport terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on NAV DB UPDATED Active navigation database updated TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable System has updated the active navigation database from the standby navigation database One of the terrain airport terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 1347D 1347D 20 MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative GMA FAIL GMA2 is inoperative The audio panel self test has detected a failure The audio panel is unavailable The system should be serviced GMA XTALK GMA crosstalk error has occurred An error has oc
139. the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is Shown at the bottom FREEZING LEVEL The age of the displayed data is shown at the right WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right CYCLONE WARNING The age of the displayed data is shown at the right il VAY AIREP The age of the displayed data is shown at the right a Bn PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow 2171 TURBULENCE The age of the displayed data is shown at the right The FATUE IEEE altitude selection is shown at the bottom gi ICING POTENTIAL The age of the displayed data is shown at the right 6000FtT The altitude selection is shown at the bottom No Status Icon TFR Depicted as an area outlined in yellow 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 45 AEN 549 S24V oipny uadx 5729 sjueumasuj u102 AEN 1014 buluueld Wil e uepioAy s mp oold paezey sualy uonesado soJnjeoJ junu
140. the active frequency field INTERCOM SYSTEM ICS ISOLATION Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may select or deselect the intercom The MAN SQ Key allows either automatic or manual control of the intercom squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator When the MAN SQ Annunciator is extinguished Automatic Squelch is on the ICS Knob controls only the volume pressing the ICS Knob has no effect on the VOL SQ selection When the MAN SQ Annunciator is illuminated Manual Squelch the ICS Knob controls either volume or squelch selected by pressing the ICS Knob and indicated by the VOL or SQ annunciation Passenger Address PA System A passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the cockpit speaker Gf selected on or on the headset if the PA Key is selected on both audio panels PA messages are one way from the flight deck to the passengers 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 9 sjueuinasu nubi 52 oipny uadx 5721 U10 AEN uonesado soJnjeoJ 2 AEN Sd junuuy
141. tion Annun Alerts A Appendix 0808080 GARMIN Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by each AHRS GRSI and GRS2 If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure Note in the following example GRSI is the first AHRS to indicate an update is available In actuality this is dependent on which AHRS is the first to report status to the system GRS2 may be displayed before GRS1 The order is not important only that both AHRS be updated GRS1 MV DB Update Available Update from 2005 to 2010 OK or CANCEL GRS1 Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update 1 With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Uploading GRS1 Mag Var Database STARTING UPLOAD 0 0Z Uploading Database to GRS1 112 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN 00 Appendix 2 VVhen the upload is complete the prompt for the next GRS upload is displayed as seen in the follovving figure 6RS2 MV DB Update Available Update from 2005 to 2010 UK or CANCEL GRS2 Magnetic Field Variation Database Update Prompt 3 With OK highlighted
142. to highlight SELECT APPROACH 3 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 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 sjuaumasu yp 5721 oipny uddx UI0JNeN 52 AEN 540 buluueld nf s mp old eouepioAy paezey saunqea4 jeuonippy 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 or optional RAD ALT 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 procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD uoneiedo Jeuuouqy Sue v unuuy highlighted 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instru
143. ttitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glide AFCSAnnunciaions PFD Setup Menu path and Vertical Flight Director Windows displayed in Deviation Indicators Command Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports 2 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 64 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A GARMIN Abnormal operation 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 A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In a
144. uide for the Cessna Citation Mustang A Warnings Cantons amp Notes 51 j GARMIN WARNING Do not use datalink weather products e g XM WX Satellite Weather GFDS World Wide Weather or FIS B for hazardous weather penetration Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear 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 G1000 Integrated Flight Deck as installed in the Cessna Citation Mustang 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 system 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 system 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
145. uld be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 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 system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced 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 system should be serviced The MFD and PFDs have different software versions installed The system should be serviced 16 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power us
146. ursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field 190 00600 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 53 AEN Sd5 S24V oipny uddx 5219 sjuauimasu Tuo2 AEN 3 blu Duruue d nubi s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Ground Mapping 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Select the BACK Softkey Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turn the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor Antenna Stabilization 1 2 To activate or deactivate the antenna stabilization select the MODE Softkey Select
147. uy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Alerts Operation Features Avoidance Procedures Appendix Index A Hazard Avoidance 2 GARMIN TRAFFIC SYSTEMS WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic e Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Soltkey is displayed Ifa Traffic Advisory System TAS is configured a STANDBY NORMAL TEST and ALT MODE Softkey is displayed fa TCAS II system is configured a REL ABS TRC STBY TA ONLY TA RA TEST and ALT RNG Softkey is displayed Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA TAS and TCAS II only intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA Potential collision area is within 20 to 48 seconds Traffic Advisory Off Scale Resolution Advisory RA TCAS only Potential collision area is within 15 to 35 seconds Resolution Advisory Off Scale TCAS II only Traffic Symbol Description Traffic Information Service TIS
148. vate approach when required 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 PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF 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 190 006
149. 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 offset distance from the selected Direct to Press the ENT Key to highlight Activate or tum 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 Key again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the MFD Controller 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 1 2 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the destination waypoint for the desired leg Or Use the J
150. x Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description 100 DFLTS WIND DME BRGI BRG2 ALT UNIT SYN TERR HRZN HDG APTSIGNS OPIN 1 OPTN 2 OPTN 3 OFF METERS IN 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 direction and speed 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 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter and selected altitude in meters Press to display the BARO setting as inches of mercury Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 04 Rev A A GARMIN Appendix Level 1 Level2 Level 3 Description

Garmin Software Version 0435.24 Cockpit Reference Guide

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