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Garmin Software Version 0435.11 Cockpit Reference Guide

1. aying data from the number two GPS receiver PFD2 is displaying data from the 1 Air Data Computer PFD1 is displaying data from the 2 Air Data Computer PFD2 is displaying data from the 1 AHRS 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sainjea4 2 Duruue d AEN Sd5 S24JV olpny uqax 5921 s tin sul 2 Ubil uio AeN 1i jeuonippy uoneiedo jeuuouqv xipuaddy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Ed Annunciations amp Alerts A GARMIN Reversionary Sensor Window Text Condition PFD1 is displaying data from the 2 AHRS PFD2 is displaying data from the 1 GPS PFD1 is displaying data from the 2 GPS AFCS ALERTS Condition Annunciation Description Pitch Failure PTCH Pitch axis control failure AP is inoperative Roll Failure ROLL Roll axis control failure AP is inoperative MET Switch Stuck If annunciated when AP is engaged a failure has occurred in or Pitch Trim Axis PTRM the pitch trim system If annunciated when AP is not engaged Control Failure a failed or stuck switch is causing the annunciation System Failure AFCS AP and MET are unavailable FD may still be
2. MFD FAN FAIL The cooling fan for the MFD is inoperative AV FAN FAIL The cooling fan for remote avionics has failed AURAL ALERTS Alerts Window Message Audio Alert PFD1 FAN FAIL The cooling fan for PFD1 is inoperative PFD2 FAN FAIL The cooling fan for PFD2 is inoperative TN Aural Alert Description s Minimums minimums The aircra decision altitude t has descended below the preset minimum descent altitude or Vertical track The aircra navigation is enabled tis one minute from Top of Descent Issued only when vertical s TIS not available The aircra available when a TAS system is installed Traffic The Traffic Information Service TIS has issued a Traffic Advisory alert tis outside the Traffic Information Service TIS coverage area not MFD amp PFD MESSAGE ADVISORIES Message Comments was lost Recheck settings settings if desired DATA LOST Pilot stored data The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred serviced XTALK ERROR A flight display The MFD and PFDs are not communicating crosstalk error has occurred with each other The G1000 system should be PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair PFD2 SERVICE PFD2 ne
3. 2 Buruuejd AEN 5649 2 oipny uadx svoli siu umnsul paezey nubi u102 NEN Wil jeuonippy uoneiedo Jeuuouqy R x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix bres Annunciations amp Alerts GDC 74B MESSAGE ADVISORIES A GARMIN Message ADC1 ALT EC ADCI altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable Comments GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC ADC1 airspeed error correction is unavailable ADC2 AS EC 2 airspeed error correction is unavailable 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 G1000 system should be serviced GCU 475 MESSAGE ADVISORIES Message GCU CNFG GCU Config error Config service req d Comments GCU 475 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GCU FAIL GCU is inoperative MANIFEST GCU software mismatch communication halted A failure has been detected in the GCU 475 The GCU 475 is unavailable The G
4. CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must 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 da
5. sssssseeenennnnnen i Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Table of Contents ABNORMAL OPERATION Reversionary Mode ssssssssseeeneene nennen Abnormal COM Operation ssssssssseeenennnnnn Hazard Displays with Loss of GPS Position Unusual Attitudes sseennnnnnnnnne MEC O eerte te e Rete ee er ig ANNUNCIATIONS amp ALERTS CAS Messages Comparator Annunciations Reversionary Sensor Annunciations ssssssse AFCS Aleits ete d be odo TAWS Alerts Message Advisory Alerts Aural Alerts tor teat m dede teda ee MFD amp PFD Message Advisories Database Message Advisories GMA 1347D Message Advisories ss s s s s s ss s sss ssss 64 GIA 63W Message Advisories GEA 71 Message Advisories ssssssssseeee nne GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GWX 68 Alert Messages GDC 74B Message Advisories GCU 475 Message Advisories GMC 710 Message Advisories Miscellaneous Message Advisories APPENDIX GEN a 77 PED Softkey Map orc he eet eet te ctt etin eh n 77 MFD Softkey Map nennen 82 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guid
6. 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 Softkey 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 Pressing the MORE Softkey repeatedly cycles through the preset channels 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 4 2 Buruuejd AeN Sd5 S24V oipny uadx svola siu u nnsul Tu102 AEN 346 eouepioAy paezey xipueddy suelv uoneiedo sainjea4 unuuy Jeuuouqy jeuonippy x pul A Additional Features GARMIN 3 Select any one of the PS1 PS15 softkeys to assign a number to the active channel Fight Instruments 4 Select the SET Softkey on the desired channel number to save the channel R as a preset Adjusting Volume B E Radio volume is controlled at each passenger station BO Za x Flight Procedures Planning GPS Nav AFCS Hazard Avoidance Bu E ea ss se lt Annun Abnormal Appendix Alerts Operation Index 48 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A GARMIN Abnormal operation ABNORMAL OPERATION REVERSIONARY MODE If the system detects a failure in PFD1 reversionary mode is entered automatically Rev
7. 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sjuauimasu sub 5721 olpny uqax 0105 AEN ACN 540 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance 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 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or tum the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the
8. 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 second rectangular page icon Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 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 3 36 Ensure TAS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Hazard Avoidance TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY WARNING The TAWS display shows supplemental information only It should not be used for navigation A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual
9. Jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00600 02 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 fJ Key on the MFD Control Unit 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 to place the cursor over the VNV altitude field altitude constraint proceed to step 5 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 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field all FMS Knob to select MSL or AGU 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 Z on the PFD or controller 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
10. in the navigation database use this altitude in determining vertical flight path guidance The system cannot use this altitude in determining vertical flight path guidance Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN FLIGHT PLANNING WEIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters Flight Planning The Weight Planning Page is displayed after system power up If it is necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the first rectangular page icon 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 Enter the 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 Tum 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 d
11. jeuuouqy suay junuuy mun 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Index 4 A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT m e 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 21 Garmin Europe Ltd Liberty House Bulls Copse Roa Hounsdown Business Park Southampton SO40 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2006 2008 Garmin Ltd or its subsidiaries 190 00600 02 Rev A
12. optional feature Displays XM lightning information on Navigation Map optional feature 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 When available displays optional checklists 83 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang s m aoueplony sainpadold buluueld AEN Sd5 52 olpny uqax SV2l3 sjuauimasu jeuonippy 2 Wila JUI0 NEN wb uoneiedo Jeuuouqy Sue v unuuy k GARMIN Appendix Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy xe pul 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 84 A GARMIN A Activate a flight plan 16 Active Channel 46 ADF 7 8 Advisory alerts 59 AHRS 69 70 72 73 Airport Signs 43 44 Airways 83 Air Data Computer 55 Alert messages 71 ALT 36 Altimeter setting 1 50 Altitude mode 36 Altitude volume 36 Antenna stabilization 41 Antenna tilt 39 AP 56 Attitude amp Heading Reference System 55 Audio panel control
13. ssssseennnnnnes 7 ADF Tuning Optional sss 7 DIME Tuning me 7 Enter a Transponder Code sss 8 Selecting a COM Radio sssssssssseeennnennnennnnnes 8 Selecting a NAV Radio nennen 8 NAVICOM Tunirij neri rrt HR co etre re ro OR UR 8 Intercom System ICS Isolation 9 Digital Clearance Recorder and Player 0 AUTOMATIC FLIGHT CONTROL SYSTEM 5 1 Flight Director Activation sss 1 Vertical Modes are rrr ic Heo ER 2 Lateral Modes 3 5 Direct to Navigation sssssssseseeeee nennen 5 Activate a Stored Flight Plan 6 Activate a Flight Plan Leg 6 Stop Navigating a Flight Plan 7 Vertical Navigation 5 7 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A Table of Contents GARMIN FLIGHT PLANNING Uy cates vice bie ts d ets Weight Planning sssssessseeennnnnnnnnnnnnnnnnnnns canei tote 0000000000 Create a New User Waypoint Delete a User Waypoint sssssse nnn Create a New Flight Plan sss Insert a Waypoint in the Active Flight Plan 24 Enter an Airway in a Flight Plan Invert An Active Flight Plan Remove a Departure Arrival App
14. 6 Press the FMS Knob to remove the cursor Antenna Stabilization 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select 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 Softkey 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 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang AEN Sd5 S 24V oipny uddx Syl sjuaumasu Tuo2 AEN 364 Duruue d Wil aoueploay s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul GARMIN Hazard Avoidance Ssjueuinijsu fila svold oipny uadx U105 AEN s24v AeN Sd5 Duruue d Blank Page 6 2 4 2 saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00600 02 Rev A Garmin G1000 Cockpit Re
15. AHRS AHRS2 Selects the 22 AHRS 78 Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Appendix mn vmmummumm m sjuauimasu yp ESSN oes TE Esse Jur nn r m x 5721 Select the STD BARO or BACK Softkey to return to the top level softkeys olpny uqax uo2 AEN 52 L TT LL IL Yuersi L L EY V3 SUN P3 P8 98 n8 098 n5 nm l Lom m oes oFF l ll amp c L mse nmpnusnmunnnununnsntons9tom Tou PFD Configuration Softkeys AEN Sd5 Duruue d nf 2 Displays second level softkeys for additional PFD configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features eouepioAy paezey PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction soJnjeoJ jeuonippy uoneiedo Jeuuouqy HRZN HDG Displays compass heading along the Zero Pitch line APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm DFLTS Resets PFD to default settings including changing units to standard SH ly unuuy gt s 3 m x x pul 190 00600 02 Rev A Garmin G1000 Cockpit Reference
16. 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 dimb descend VS Key VS nnnn rpm to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed Hi nna IAS Hold in IAS or Mach while the aircraft is at FLC Key Flight Level Change dimbing descending to the Selected Mach Hold Altitude FLC M nnn VNAV Captures and tracks the VNAV flight VNV VPTH path Key AFCS armed to capture the altitude VNAV Target i R Altitude Armed disp ayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the WAAS GP glidepath on approach Captoresand tede thelb diae S Glideslope aptures and tracks the ILS glideslope GS on approach Disengages the autopilot and GA Go Around commands a constant pitch attitude GA Switch and wings level ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude is to be captured inste ad of 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 190 00600 02 Rev A A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude
17. Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums 66 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN GIA 63W MESSAGE ADVISORIES CONT Annunciations amp Alerts Message TRUE APR True north approach Change HDG reference to TRUE Comments Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE service Return GPS1 needs unit for repair GPS2 SERVICE service Return GPS2 needs unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE service Return NAV1 needs unit for repair NAV2 SERVICE service Return NAV2 needs unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operation If the problem persists the G1000 system should be serviced G S1 FAIL 6 51 is in
18. FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sjuaumasu Yid 5721 oipny uddx UI0JNeN 52 AEN 540 Duruue d nf s mp old uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 32 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the go around button Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Tra
19. Guide for the Cessna Citation Mustang 19 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix WIND DME BRGI BRG2 ALT UNIT STD BARO 80 OPTN 1 OPTN 2 OPTN3 OFF METERS IN HPA A GARMIN 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 Select to display 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 in meters Select to display the BARO setting as inches of mercury Select to display the BARO setting as hectopacals Sets altimeter setting to standard barometric pressure Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A mumu mumu uu sjuauimasu nubi XPDR1 XPDR2 STBY ON ALT GND VFR CODE IDENT BACK MSG Fu F3 5 09 9 n9 ru unu Select the BACK Softkey to return to the top
20. Index Hazard Avoidance A GARMIN Enable Disable Aviation Data 1 2 3 While the TAWS Page is displayed press the MENU Key Turn the small FMS Knob to select Show or Hide Aviation Data Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS Page is displayed select the INHIBIT Softkey 1 2 3 Or Press the MENU Key Turn the small FMS Knob to select Inhibit TAWS Press the ENT Key Enable TAWS While the TAWS Page is displayed select the INHIBIT Softkey 1 2 3 38 Or While the TAWS Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Hazard Avoidance 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 Ay 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 a
21. N 4 5 6 7 8 9 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired 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 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired waypoint within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 30 1 2 3 4 5 6 NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displa
22. S24V oipny uadx svola Tu102 AEN 346 eouepioAy paezey s m e q jeuonippy xipueddy suelv uoneiedo junuuy Jeuuouqy 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 GARMIN Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts in electronic form it is still advisable to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness w
23. SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key HF if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key HF if installed on the audio panel SELECTING A NAV RADIO 1 2 Press the CDI Softkey to select NAV1 VOR1 LOC1 or NAV2 VOR2 LOC2 Pressing the NAV1 NAV2 DME or ADF Key on the audio panel selects and deselects the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 2 3 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 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 Press the Frequency Transfer Key to place the frequency into the active frequency field Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A 1 Nav Com XPDR Audio Panel INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPIT Key on either audio panel to select those isolated from hearing the Nav Com radios and music Copilot Side Passenger Hears Selected Selected Selected Radios Radios Radios Aural Aural Aural Alerts Pilot Alerts Pilot Alerts Pilot Copilot Copilot Copilot Passengers Passengers Passengers Music Music Music Selected Selected
24. System Test 1 While the TAWS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS Page 3 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 37 x pu ddy su jy uoneiedo sainjea4 aueploAy 2 Duruue d AEN Sd5 S24JV olpny uqax 5213 sjuauimasu Tunuuy Jeuuouqy jeuonippy paezeH nu U10 AEN fid x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features
25. VPTH GPS NAV Key Navigation VOR 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 NAVor APR Key press activates flight director TE 7 selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 11 sjuauimasu nubi 5721 oipny uadx u102 AEN ARN Sd5 52 suey uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d Tunuuy Jeuuouqy Jeuonippy 2 xipueddy 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 A GARMIN 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 Selected Altitude displayed in the Selected Altitude
26. data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU 62 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists Comments The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persist
27. level softkeys 5721 LT TT T Ts L s L s jp 7 ekse T back L veo A V3 F3 A 9n n o n EH Select the BACK Softkey to return to the top level softkeys olpny uqax 0105 AEN 52 Transponder Softkeys AEN Sd5 ADF DME Displays the ADF DME Tuning Window XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does not reply to any interrogations Duruue d nubi SoJnpa20Jd ON Selects Mode A transponder replies to interrogations AIT Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations GND 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 aoueplony paezey saunyea4 jeuonippy uoneiedo Jeuuouqy VFR Automatically enters the VFR code 1200in 3 the U S A only iis CODE Displays transponder code selection softkeys 0 7 0 7 Use numbers to enter code gt 5 3 m x BKSP Removes numbers entered one at a time x pul 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Index A Appendix GARMIN IDENT Activat
28. monitor has not been xxix X properly tested or has failed 3 Duct temperature too high or sensor 8 2 disconnected s ENG A I COLD L R Engine anti ice system ON and inlet x lx emperature is cold A FADEC has a fault that requires EB maintenance ge KES An engine has failed Fuel firewall shutoff valve fully closed X A flap system failure has occurred X 8 Electric fuel boost pump ON Caution FUEL BOOST L R condition is d splayed when the X E E boost pump is operating in abnormal 38 conditions SE Engine fuel filter impending bypass X Switch closed EINEN UMEN sek Fuel low level function failure X X Fuel level in tank is too low X Fuel pressure too low XIX REN RUB a Fuel transfer valve open X b One or both electrical generators zi offline Hydraulic system pressure too low X X 5 Hydraulic pump running too long X X 8 53 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Flight Instruments Nav Com XPDR Audio Additional Hazard Flight Planning Abnormal EICAS AFCS GPS Nav Features Avoidance Procedures Operation Appendix Index Annunciations amp Alerts A GARMIN Messages Inhibits Description _ _lee Warning Caution Advisory 2 5 S 2 D MFD temperature is below 20 C One or both nose baggage doors not X fully secured 0 DO Antisk
29. 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 magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER f message Message criteria entered by the user 76 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN o 0000000 Appendix APPENDIX sjuaumasu nubi PFD SOFTKEY MAP 5721 r mu m r r mu s r CDI NAV1 olpny uqax uo2 AEN CDI GPS a Top Level PFD Softkeys E SENSOR PFD OBS ADF DME ITMR REF NS v vi 9 n Duruue d Wil optional optional n LA FF A n mn Select the BACK or OFF Softkey to return to the top level softkeys gt ES a m TE Inset Map Softkeys ae 52 os dai INSET Displays Inset Map in PFD lower left corner 2 2 OFF Removes Inset Map EH DCLTR 3 Selects desired amount of map detail cycles
30. 600 02 Added Synthetic Vision Added other GDU 9 01 parameters Revision Date of Revision Affected Pages Apri 2008 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang RR 1 A Record of Revisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Tibleof Contents tla te atit 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure ssssssssee 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 GPS 2 GenericTimer apayd n 2 Configure Vspeed Bugs Individually ss 2 Turn Vspeed Bugs On or Off by Category 3 Set Barometric Minimum Descent Altitude sss 3 Displaying Wind Data 3 ENGINE INDICATION amp CREW ALERTING SYSTEM 5 Crew Alerting System CAS 6 CAS Messages and Prioritization sss 6 NAV COM TRANSPONDER AUDIO PANEL 7 Enter or Change Flight ID
31. Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A Warnings Cautions amp Notes GARMIN WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East
32. Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 4 A GARMIN Select the GO BACK Softkey to return to the previous page Change Day Night View 2 3 4 5 6 1 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu XM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 2 3 Turn the large FMS Knob to select the Auxiliary Page Group Turn the small FMS Knob to select the displayed AUX XM Information Page Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active C
33. CU 475 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 475 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 72 Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN GMC 710 MESSAGE ADVISORIES Annunciations amp Alerts Message GMC CONFIG GMC Config error Config service req d Comments Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative A failure has been detected in the GMC 710 The GMC 710 is unavailable MANIFEST GMC software mismatch Communication halted The GMC 710 has incorrect software installed The G1000 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 G1000 system should be serviced if the problem persists MISCELLANEOUS MESSAGE ADVI SORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user w
34. DL69 CONFIG GDL 69 config error Config service req d Comments GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The G1000 system should be serviced 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 G1000 system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving 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 A failure has been detected in the GWX 68 The GWX 68 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The G1000 system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang so1njeoJ
35. Duruue d AEN Sd5 S24JV olpny uqax SV2l3 sjuauimasu Tunuuy qeuuouqy leuonippyv paezey Wfl U10 AEN ii 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 GARMI N 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 When 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 2 3 Press the MENU Key Turn the large FMS Knob to select Show Bearing Line Press the ENT Key Vertically Scan a Storm Cell 1 2 3 4 5 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 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed Move the Joystick right or left to move the scanned slice a few degrees right or left Turn the Joystick to adjust the range 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 1 2 3 4 40 WARNING Changing the ga
36. FDs and MFD have different obstacle database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays CAS INOP No Dispatch Database correction required The MFD and or PFDs have an aviation database mismatch A red will appear in the CAS display Load the same aviation database version in the MFD and both PFDs GMA 1347D 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 G1000 system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The G1000 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 G1000 system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The MANIFEST GMA2 software G1000 system should be serviced mismatch communication halted GMA1 SERVICE GMA
37. G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Citation Mustang A GARMIN Copyright 2006 2008 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0435 11 or later for the Cessna Citation Mustang Some differences in operati on may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Tel 913 397 8200 Garmin Tel 503 391 3411 Southampton 040 9RB U K Garmin Tel 44 Garmin Web Site Address www garmin com 0870 8501241 Except as expressly provided herein no part of disseminated downloaded or stored written manual Garmin and G10009 are registered tradem FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express Street Olathe Kansas 66062 U S A Fax 913 397 8282 AT Inc 2345 Turner Road SE Salem OR 97302 U S A Fax 503 364 2138 Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Fax 44 0870 8501251 Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 this manual may be reproduced copied transmitted in any storage medium for any purpose without the express permission of Garmin Garmin hereby gr
38. Loss of Hazard Functions with Loss of GPS Position x pul 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 4 Nav Com XPDR Audio Hazard Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation UNUSUAL ATTITUDES functions are displayed in these situations are disabled when the aircraft experiences unusual attitudes 50 Traffic Annunciations AFCS Annunciations Flight director Com mand Bars Inset Map Temperatures DME Information Window Wind Data Selected Heading Box Selected Course Box Transponder Status Box Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Extreme Pitch Indication System Time PFD Setup Menu Windows displayed in the lower right corner of the PFD Timer References Nearest Airports Flight Plan Messages Procedures Barometric Minimum Descent Altitude Box A GARMIN The PFD declutters when the aircraft enters an unusual attitude Only the primary The following information is removed from the PFD and corresponding softkeys Glideslope Glidepath and Vertical Deviation Indicators Altimeter Barometric Setting Selected Altitude VNV Target Altitude 190 00600 02 Rev A GARMIN Abnormal operation DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detect
39. 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 aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Warnings Cautions amp Notes V ARNING NEXRAD vveather data is to be used for long range planning purp
40. NAV1 2 8 NAV2 2 8 Navigation database 17 18 NEXRAD 33 34 78 83 0 OBS 2 Obstacles 64 65 Overspeed Protection 12 P Pathvvays 43 PIT 55 Play 10 Index 2 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A GARMIN R Reversionary Mode EICAS 5 Reversionary mode 49 ROC 57 58 S SafeTaxi 44 Sector scan 41 Sensor 55 STAB 41 Standby 39 Store Flight Plan 26 SVS 43 76 Synthetic Vision System 43 T TAF 33 TAS 36 69 TAWS 37 38 57 58 TAWS B 37 Terrain 37 63 78 83 Tilt line 39 Timer 2 73 Topographical data 78 83 Traffic 33 35 82 Traffic advisory 35 Traffic map page 35 36 Transponder 7 8 81 82 V Vertical speed guidance 18 Vertical track 59 VNV 15 50 75 76 Vspeed 2 190 00600 02 Rev A A GARMIN W WAAS 65 WATCH 41 Weather Attenuated Color Highlight 41 Weather data link page 33 Weather radar 39 Wind data 80 X XM lightning 78 83 XM weather 33 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Index Index 3 SaJnjeoJ aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 5921 sjuaumnasu jeuonippy 2 ni Tuo2 NeN sub uoneiedo Jeuuouqy SHE yunuuy m d GARMIN Index Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo
41. Radios Radios Aural Alerts Aural Alerts Copilot gets Copilot Music Passengers Passengers Music Music Selected Selected Radios radios Aural Passengers Aural Alerts Alerts Pilot Pilot Music Copilot Passengers Music Pilot Side Passenger Hears PILOT Key COPLT Key Pilot Hears Copilot Annunciator Annunciator Hears Selected Radios Aural Alerts Pilot Copilot Passengers Music Selected Radios Aural Alerts Pilot Copilot Selected Radios Aural Alerts Pilot Passengers Music Selected Radios Aural Selected Radios Aural Passengers Passengers Alerts Pilot Music Music Alerts Pilot Gol Copilot 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Sjueuinajsu iui S24V olpnyyuqax svn JUI05 AEN suey uoneiedo s m 2 Duruue d AEN Sd5 junuuy jeuuouqy feuonippv 2 Juil xipueddy x pul Flight Instruments Flight Planning Abnormal Additional Hazard Avoidance Annun Nav Com AFCS XPDR Audi EICAS Procedures GPS Nav Appendix Alerts Operation Features Index A Nav Com XPDR Audio Panel GARMIN DIGITAL CLEARANCE RECORDER AND PLAYER 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 Pr
42. Roll Hold or rolls wings level depending on default ROL commanded bank angle Low Bank Limits maximum commanded roll angle 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 Backcourse Arm Captures and tracks a localizer signal BC Ke BC Capture Track for backcourse approaches y Approach GPS GPS Arm Capture Track Approach VOR VAPP Arm Capture Track 1 Captures and tracks selected navigation APR Key Approach ILS Arm 1 source GPS VOR LOC Capture Track Glideslope Mode automatically armed sauna Disengages autopilot and commands GA GA constant pitch angle and wings level Switch No annunciation 5 7 in the AFCS Status Box The acceptable bank angle range is indicated in le of the Attitude Indicator green along the Ro 190 00600 02 Rev A Sca Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sv l3 sjuounasu oipny uddx U105 AeN ARN Sd5 52 Suelv uoneiedo sainjea4 aoueplony 2 Duruue d Tunuuy Jeuuouqy Jeuonippy xipueddy x pul iui TL paezey GARMIN AFCS Ssjueuinijsu fila 5721 oipny uadx U105 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey s m d
43. T needs The audio panel self test has detected a problem in service Return unit for repair the unit Certain audio functions may still be avail GMA2 SERVICE GMA2 needs able and the audio panel may still be usable The service Retum unit for repair G1000 system should be serviced when possible 64 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN GIA 63W MESSAGE ADVISORIES Annunciations amp Alerts Message GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d Comments The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced GIA1 SERVICE G A1 needs service Return the u
44. TART 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 Select 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 02 Rev A GARMIN Flight instruments 4 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF Softkey zu e gt g 2 o 2 a 5721 TURN VSPEED BUGS ON OR OFF BY CATEGORY 1 Press the TMR REF Softkey 2 Press the MENU Key 3 Turn the FMS Knob to highlight the desired option 4 Press the ENT Key Press the TMR REF Softkey to remove the window oipny uadx 0105 AEN 52 SET BAROMETRIC MINIMUM DESCENT ALTITUDE AEN Sd5 1 Select the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remov
45. This occurs when a stored flight plan contains an airway that is no longer consistent with the aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed FPL TRUNC Flight plan has been truncated This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint xxxx 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 74 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN A
46. Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field Turn the small FMS Knob to highlight the desired waypoint Select the DELETE Softkey The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A NEW FLIGHT PLAN 22 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A GARMIN ligt Planning Using the MFD 1 Press the FPL Key 2 Turn the small FMS Knob to display the Flight Plan Catalog Page 3 Select the NEW Softkey to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window 5 Enter the identifier of the departure waypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter the identifier for each additional flight plan waypoint 8 When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Using the PFD 1 2 3 4 5 6 1 8 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD Press the FPL Key Turn the small FMS Knob to display the Waypoint Information Page Turn the small FMS Knob to enter the first let
47. ants permission to download a single copy of this and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyrig commercial distribution of this manual or any ht notice and provided further that any unauthorized revision hereto is strictly prohibited arks of Garmin Ltd or its subsidiaries WATCHS Satellite Radio Inc April 2008 190 00600 permission of Garmin NavData is a registered trademark of Jeppesen Inc XM is a registered trademark of XM 02 Rev A Printed in the U S A A Warnings Cautions amp Notes GARMIN e o 6 WARNING The G1000 TAWS feature does not relieve the pilot from the responsibility of being aware of surroundings during flight The TAWS feature isonly to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above
48. available engaged when aircraft altitude above 30 000 ft and pus A de EDM cabin pressurization is lost Selected Heading set 90 left of current heading Selected Altitude set to 15000 ft Elevator Mistrim A condition has developed causing the pitch servo to Up provide a sustained force in the nose up direction Elevator Mistrim A condition has developed causing the pitch servo to Down provide a sustained force in the nose down direction Aileron Mistrim A condition has developed causing the roll servo to provide Left a sustained left force Aileron Mistrim A condition has developed causing the roll servo to provide Right meg a sustained right force Rudder Mistrim Left A condition has developed causi provide a sustained force ng the yaw servo to Rudder Mistrim Right A condition has developed causing the yaw servo to provide a sustained force Preflight Test CIEE RUD RUD ESPERE PFT Performing preflight system test Upon completion of the test the aural alert will be heard PFT Preflight system test has failed 56 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Annunciations amp Alerts TAWS ALERTS PFD MFD MFD Alert Type TAWS Page Aural Message NS Pop Up Alert Annunciation Excessive Des
49. aypoint 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 00600 02 Rev A 15 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang s m p q e ueproAy SoJnpa204d Duruue d AEN 540 24V oipny uadx sv2l3 sjueumasu puezey BITTE UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy 5 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations 8 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 NO WGS84 WPT Non WGS 84 waypoint for navigation Doox TRAFFIC FAIL Traffic device has failed The selected waypoint box does not use the WGS 84 datum Cross check position with alternate navigation sources The G1000 is no longer receiving data from the traffic system The traffic device should be serviced FAILED PATH A data path has failed A data path connected to the GDU or
50. aypoints 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 The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang n soJnjeoJ 2 Buruuejg AEN Sd S24V olpny uqax svoli sjuauinsu paezey nubi u102 NEN nubi jeuonippy uoneiedo Jeuuouqy n EE x pul Hazard Flight Nav Com Flight 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 an aviation 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
51. cent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP ee Terrain Terrain Pull Up Terrain Clearance or Pull Up Warning RTC TERRAIN AHEAD PULL UP or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up 7 Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up tena Oe T Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstade PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up o STALE PULP Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain 0 TERNAERD T Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AFAD Terrain Ahead Terrain Impact Caution ITI or Ahead Olin TEIN d Caution Terrain Caution Terrain 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 57 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V oipny uadx 5721 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy IM x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix poesi Annunc
52. d consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sepeooid uluueld AEN 540 52 oipny uadx Svo syuoumasul U105 AeN paezey saunyea4 Jeuolppy Sue v unuuy xipueddy x pul iui Wfil4 Nav Com XPDR Audio Hazard Avoidance Additional Annun Flight Instruments Flight Planning EICAS AFCS Alerts Features Procedures GPS Nav Appendix Index A Abnormal Operation GARMIN TEESDALESEY SE 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
53. data includes the following Navigation Status Box fields except Active Leg TAS and DIK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Track Bug All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and both TAWS and Terrain Proximity are disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 52 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A GARMI N Annunciations amp Alerts ANNUNCIATIONS amp ALERTS Sjueuingjsu sub CAS MESSAGES Messages Inhibits fea AN Description arn n aution visor cA geza 22 Tailcone baggage door not fully X E S secured s s Start control circuit breaker located i in aft j box tripped gt Current limiter blown located in a aft j box Antiskid Control Unit cannot perform s ips X a anti skid functions 3 Overheated NiCad battery optional 8 Battery temperature sensor failure Cabin altitude potentially unsafe X X X s z Q Cabin door not fully secured X 2 A door
54. e for the Cessna Citation Mustang 4 A Table of Contents GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 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 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Select the HPA Softkey to display the barometric pressure setting in hectopascals 4 Select the BACK Softkey to return to the top level softkeys 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 SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang xipueddy Suelv uoneied
55. e the window press the CLR Key or the TMR REF Softkey aoueplony SoJnpa204d Duruue d puezey ubi so1njeoJ jeuonippy DISPLAYING WIND DATA 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data below the Selected Heading 3 Select one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window select the OFF Softkey xipueddy Suelv uoneiedo junuuy Jeuuouqy x pul 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang GARMIN Flight Instruments i U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A GARMIN EA ENGINE INDICATION amp CREW ALERTING SYSTEM ign ITTC sg E oipny uddx U10 AEN S24V VOLTS AMPS G 4 1500 2727 30 BATTERY 1000 27 voLTs ACN Sd5 fila Buiuue d CABIN PRESS 700 700 ALT FT RATE 750 es RP 8 89 2 Nzz 89 2 1500 OIL 2 1000 1000 101 Psi 101 Q 137 t 135 x 7500 FUEL i 5870 DEST ELV 0 300 LBS 300 5 0 DIFF PSI 530 PPH 530 12 C 28 DC VOLTS 28 245 DC AMPS 245 BATT VOLTS 28 CABIN PRESS ALT FT 100 DIFF PSI 3 FLAPS LAND ze EICAS Dis
56. eds The PFD and or MFD self test has detected a service Return unit for repair problem The G1000 system should be serviced 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 59 Sonje2J aoueplony SoJnpa20Jd Buruue d AEN Sd5 2 oipny uddx sv l3 Sjueumansu paezey nubi nubi jeuonippy uoneiedo Jeuuouqy 5 EE 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 A GARMIN MFD amp PFD MESSAGE ADVISORIES CONT Message MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted Comments The PFD and or MFD has incorrect software installed The G1000 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 G1000 system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFDs have different sof
57. ersionary mode must be entered manually in the case of PFD2 or MFD failure In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display sjuaumasu iui 5721 olpny uqax 0105 AEN Manual activation 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 52 AEN 540 Duruue d Wil NOTE The Cessna Citation Mustang Airplane Flight Manual AFM always takes precedence over the information found in this section SeJnpa20Jd 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 eouepioAy paezey soinjeo4 Jeuonippy 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 sue v unuuy xipuaddy anuuuu
58. es the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen TMR REF Displays Timer References Window NRST Displays Nearest Airports Window MSG Displays Message Window MFD SOFTKEY MAP V3 T a ES Select the BACK Softkey on this level to return to the top softkey level optional optional nen A MFD Softkeys CAS 1 Scroll up Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling CAS Y Scroll down Displayed only when a sufficient number of items are displayed in the Crew Alert ing System Display to warrant scrolling MAP Enables second level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map 82 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN DCLTR 3 SHW CHRT CHKLIST 190 00600 02 Rev A TOPO TERRAIN AIRWAYS NEXRAD XM LING BACK Appendix 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 AIl 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
59. esired reserve fuel quantity 6 Press the FMS Knob to remove the cursor TRIP PLANNING 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select the second rectangular page icon 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode select the AUTO or MANUAL Softkey 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 19 sjuauimasu iui 5729 oipny uddx UI0JNeN 52 SoJnpa204d AEN 540 nubi uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey 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 20 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 startin
60. ess 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold default ROL Pitch Hold default PIT GA Switch 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
61. euonippy uoneiedo Jeuuouqy 3 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing Comments The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists 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 G1000 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 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 The MFD and or PFD detected a failure in the airport terrain database Ensure that the
62. ference Guide for the Cessna Citation Mustang 42 A GARMIN ADDITIONAL FEATURES SYNTHETIC VISION Additional Features Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS offers a three dimensional view of terrain and obstacles obstacles that pose a threat to the aircraft in flight are shaded yellow or red Terrain and In addition to SVS enhancement to the PFD the following feature enhancements have been added to e Pathways the PFD 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 Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 43 2 Buruuejd AeN Sd5
63. ffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page XM WEATHER OPTIONAL N V ARNING Use of XM vveather for hazardous vveather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 3 AEN 540 S24V oipny uadx svo syuauinyysuy Tuo2 AEN iui Duruue d wold aoueploay s mp oold paezey suelv uoneiedo SaJnjeoJ Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abno
64. g waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint 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 02 Rev A A GARMIN 6 Enterthe departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings Flight Planning 7 Enter the fuel flow Press t
65. hannel 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 46 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Silil nl festimi Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 While on the XM Radio Page select the CHNL Softkey 2 Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Select the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel
66. he ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system 8 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 9 The flashing cursor moves to the calibrated airspeed field Enter a calibrated airspeed Press the ENT Key when finished CREATE A NEW USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Select the NEW Softkey A waypoint is created at the current aircraft position 4 Enterthe desired waypoint name 5 Press the ENT Key 6 Thecursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Use one of the following methods to enter the reference waypoint a Turn the small FMS Knob to the left to display a list of flight plan waypoints This list is populated only when there is an active flight plan b Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Ke
67. hile taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying 4 Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Additional Festimet the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of National Aeronautical Charting Office NACO ter
68. ht Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 26 1 2 3 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 of the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Flight Planning 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 Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn 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 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
69. iations amp Alerts A GARMIN PFD MFD MFD Alert Type TAWS Page Aural Message ag Pop Up Alert Annunciation Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Cau Obstacle Clearance or tion Obstacle Caution ROC BHB a Obstacle Ahead Obstacle Ahead Imminent Obstade TERRAIN AHEAD Obstacle Ahead Obstacle Impact Caution 101 or Ahead OBSTALE x Caution Obstacle Cau tion Obstacle Premature Descent TERRAIN TOO LOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Climb TERRAIN Dots Don t Sink Rate Caution NCR or or TEE Tox Low Terrain Default configuration TAWS System Status Annunciations PFD MFD MED Alert Type TAWS Page Aural Message Pe Pop Up Alert Annunciation TAWS System Test Fail TAWS FAIL None TAWS System Failure TAWS Alerting is disabled TAWS INHB None None No GPS position or TAWS NA None TAWS Not Available excessively degraded GPS signal System Test in progress TAHS TEST None None System Test pass None None TAWS System Test OK 58 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN MESSAGE ADVISORY ALERTS Annunciations amp Alerts
70. id cont ol spindown function x x not working Oil pressure less than redline low limit X XIX Oxygen supply off xi X X o current detected to pitot static X heater R Pressure controller loss of integrity xi X X Air Source Selector switch in OFF or X X resh air position PD BR DE Speed brakes extended X Failure detected in stall warning system X X X X Stal warning system on ice X X contaminated schedule o power delivered to stall warning vane heater A De ice boots inflating deflating as designed 2 probe heater failure xi X X 7 temp high possible bleed xl x dx De ice system not operating normally X wim Loss of power to windshield heater X mee Windshield anti ice power ON emperature too high X De ice system operating abnormally X Gear on ground inputs do not agree xi X X Only affected side displayed L R or L R in a CAS message applicable CAS messages listed here e display L R for example Name EMER Emergency Bus Mode Inhibit Inhibit ESI Engine Start Inhibit TOPI Takeoff Operation Phase Inhibit AIR In Air Inhibit LOPI Landing Operation Phase Inhibit ESDI Engine Shutdown Inhibit 54 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Annunciations amp Alerts COMPARATOR ANNUNCIATIONS Comparator Window Text Condition Difference in altitude sen
71. in 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 Select the GAIN Softkey to activate the cursor in the GAIN field 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 Press the FMS Knob to remove the cursor Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A 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 Hazard Avoidance 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
72. in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn 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 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 for the MFD 2 Turn 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 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 2 sjuauimasu nubi 5721 oipny uddx UI0JNeN 52 2 AEN 540 nubi uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey 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 5 6 A GARMIN Select the DELETE Softkey A Delete flight plan 22 confirmation window is displayed With OK highlighted press the ENT Key to dele
73. in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic If 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 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Hazard Avoidance Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation o Proximity Advisory PA TAS only intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed i
74. ircraft 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 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Radar Page 3 Select the MODE Softkey 4 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 5 Turn the Joystick to select the desired range 6 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 If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Tilt Line 3 Press the ENT Key 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 3 xipueddy suelv uoneiedo sainjea4 aueploAy 2
75. is will not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually 2217 11 70 Large White 22U 90 220 8 0NM 9900 Large Light E k Blue Text Poprooch KDFH RNAV 17LePs LPY 18 8N Small Light 33 Blue Tex d Small Light MENOL faf 39 70 RH17 53 8 pus NOE Small White Text 990FT 0 8 with Altitude POLKE Restriction Bar SIUE Cross AT or ABOVE 5 000 fi Facts Cross AT 2 300 fi inn SE AT or BELOW 3 000 ft 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Sjueuinajsu nubi 5721 oipny uadx 010 AEN spay uoneiedo s m SoJnpa20Jd Duruue d Tunuuy Jeuuouqy Jeuonippy p EZEH nuru xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EICAS Procedures Appendix Alerts Operation Features Index GPS Navigation A GARMIN 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 al
76. ite directly above the procedure s waypoints 190 00600 02 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 uoneiedo saunyea4 Junuuy jeuuouqy jeuonippy paezey 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 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 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 Flig
77. minal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX or NOTAM Softkey to access charts for departures arrivals approaches weather or NOTAMs 3 Select the GO BACK Softkey to return to the previous page View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 4 s mp o4d Buruuejd AeN Sd5 S24V oipny uadx svola siu u nnsul 614 Tu102 AEN 346 eouepioAy paezey s n ze 4 jeuonippy xipueddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard
78. n the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic is now displayed on the map 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 35 AEN 540 52 oipny uddx svn siu umnnsul Tuo2 AEN ii Duruue d nf aoueploay s mp oold paezey suelv uoneiedo SaJnjeoJ Junuuy 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 A Hazard Avoidance GARMIN Traffic Advisory System TAS Optional System Self Test 1 2 3 4 Set the range to 2 6 nm Select the STANDBY Softkey Select the TEST Softkey 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 Traffic Map Page
79. ne of the following a b a b o d a b o d e Enter the user vvaypoint identifier facility or city Press the ENT Key Or 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 NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or 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 Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 24 1 2 3 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN 4 Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway Flight Planning menu item is available only when an acceptable airway entr
80. nit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced 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 WAAS capable MANIFEST GIA1 software MANIFEST GIA2 software mismatch communication halted mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced 190 00600 02 Rev A 65 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 olpny uqax Svo Sjueunasu paezey jeuonippy uoneiedo Jeuuouqy x pul iui U105 AeN TL 3 PE Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix bees Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM 2 over temp Reducing transmitter power Comments The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system
81. nnunciations 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 Activate 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 w
82. nob 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 1 Press the FPL Key for the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure Procedures 4 Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 29 sjuaumasu Yid 5721 olpny uqax 0105 AEN 52 AEN 540 Duruue d wold s mp old uoneiado saunyea4 Junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMI
83. o sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV olpny uqax Sy2l junuuy Jeuuouqy Jeuonippy paezey ubi u102 AEN 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 2 3 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency Select the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Select the OBS Softkey to select OBS Mode 2 Turn a CRS Knob to select the desired course to from the waypoint Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Select the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Select the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Turn the small FMS Knob to display the UP 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 S
84. odel 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 G1000 system should be serviced MANIFEST GRS2 software mismatch communication halted The 2 AHRS has incorrect software installed The G1000 system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced 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 G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The G1000 system should be serviced 70 Garmin 61000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN GDL 69A MESSAGE ADVISORIES Annunciations amp Alerts Message G
85. on Mustang 190 00600 02 Rev A A GARMIN GRS 77 MESSAGE ADVISORIES Annunciations amp Alerts Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced 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 G1000 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 G1000 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 G1000 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 G1000 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 G1000 system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The G1000 system should be
86. operative G S2 FAIL 6 52 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced service Return G S1 SERVICE G S1 needs unit for repair service Return G S2 SERVICE G S2 needs unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 67 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 7213 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy Ins PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts GEA 71 MESSAGE ADVISORIES A GARMIN Message GEA1 CONFIG GEAT config error Config service req d Comments The GEAT configuration settings do not match those of backup configuration memory The G1000 system should be serviced GEA2 CONFIG GEA2 config error Config service req d The GEA2 configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrec
87. oses only Due to inherent delays in data transmission and the relative age of the data NEXRAD vveather data should not be used for short range vveather avoidance V ARNING The Garmin G1000 as installed in the Cessna Citation Mustang aircraft has a very high degree of functional integrity Hovvever the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Cessna Citation Mustang
88. play Normal Mode EIS Display Reversionary Mode gt O Engine Fan Rotation 5 Interstage Turbine Cabin Pressure Altitude 3 Speed Temperature and Change Rate Oil Pressure amp Speed 5 Engine High Pressure 2 Trim Indicator Turbine Rotation 0 Fuel Display Speed Flap Indicator Electrical Di 4 CAS Display 0 ectrical Display x pul 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A EICAS 0000 GARMIN CREW ALERTING SYSTEM CAS Flight Instruments NOTE Refer to the Annunciations and Alerts section for specific CAS messages EICAS NOTE Refer to the Airplane Flight Manual AFM for emergency procedures Nav Com XPDR Audio NOTE If there is a mismatch between databases or software on the PFDs CAS is inoperative AFCS When CAS messages are present while in reversionary mode the CAS Window appears on the display along with the flight instruments and EIS GPS Nav Flight Planning CAS Window DEST ELU CAS Display DIFF PSI Procedures XTALK ERROR A flight display crosstalk error has occurred IBACKUP MATT backup data path Hazard Avoidance Features Normal Mode Reversionary Mode Additional CAS Messages Abnormal Operation CAS MESSAGES AND PRIORITIZATION NOTE Information on CAS messages in this pilot s guide is always superseded by the AFM Warning red Immediate crew awarenes
89. rge 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 1 Press the ADF DME or DME Softkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sjuauimasu iui 52 oipny uadx 5721 U10 AEN xipueddy suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 unuuy Jeuuouqy Jeuonippy paezey Wfl x pul Flight Instruments Flight Planning Abnormal Additional Hazard Avoidance Annun Nav Com AFCS XPDR Audi EICAS GPS Nav Procedures Appendix Alerts Operation Features Index Nav Com XPDR Audio Panel A GARMIN ENTER A TRANSPONDER CODE 1 2 3 4 Press the XPDR Softkey to display the transponder mode selection softkeys Press the XPDR1 or XPDR2 Softkey to select the active transponder 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 entered the transponder code becomes active
90. rmal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMI N 4 Select the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 2 3 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key vvhen panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport vvith METAR information does not display more information but allovvs the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cell Movement City Forecast Freezing Levels Cyclone Warnings sin 22 b SUR LIC r METARs Surface Analysis County Warnings Cloud Top SIGMETs AIRMETs Winds Aloft TRAFFIC SYSTEMS 34 WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid
91. roach or Airway from a Flight Plan 25 Store a Flight Plan Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan 26 Invert and Activate a Stored Flight Plan 2 Copy a Flight Plan imi me ceteieit e 2 Delete a Flight Plan ec etre eire 2 Graphical Flight Plan Creation 28 PROCEDURES ote 29 Load and Activate a Departure Procedure sse 29 Activate A Departure Leg ssssssseeeeenennennnnne Load An Arrival Procedure Activate An Arrival Leg sssssssssseeeeenennnnnnnnnnns Load and or Activate an Approach Procedure 30 Activate An Approach in the Active Flight Plan 31 Activate a Vector to Final Approach Fix ssssssee 31 Activate A Missed Approach in the Active Flight Plan 32 HAZARD AVOIDANCE s s nnns 33 Customizing the Hazard Displays on the Navigation 33 XM Weather Optionall s s s s s s s s s s s s s s s il s 33 Tralfic Systems een he en eb ttt teen net rh to traer ien 34 Terrain Awareness amp Warning System TAWS Display 37 Airborne Color Weather Radar 39 ADDITIONAL FEATURES atenta titration Synthetic Vision Terminal Procedure Charts XM Radio Entertainment
92. s NAV1 NAV2 8 Barometric Altitude Minimums 3 Bearing line 40 41 C Cabin pressure altitude 5 CDI 1 2 8 75 Channel Presets 47 ChartView 44 45 Clearance player 10 Clearance Recorder 10 Code selection softkeys 8 COM 8 10 49 Crew Alerting System CAS Messages 6 7 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang D DCLTR Softkey 44 Dead Reckoning 51 Declutter 50 77 83 Designated altitudes 18 Direct to 15 DME 7 8 DR mode 51 52 E Edit a flight plan 26 Engine display 5 F FD 56 Flight Director 11 Flight ID 7 Flight path marker 43 FliteCharts 44 45 Frequency Transfer 8 G Gain 40 H HF 8 Horizontal scan 40 Horizon heading 43 Inhibit 38 Inhibit TAWS 38 Inset Map 77 78 Intercom isolation 9 IOI 57 58 Index Index 1 SaJnjeoJ aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 5921 sjuaumnasu jeuonippy 2 ni Tuo2 NeN iui uoneiedo Jeuuouqy Sue v unuuy d Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts kel Appendix index leppesen 45 M Map panning 34 Message advisories 59 64 67 69 70 72 76 56 33 Minimums 59 MISCOMP 55 Mistrim 56 Mode 5 81 Mode selection softkeys 8 Multi Function Display MFD Softkeys 82 N NACO 45 NAV 8
93. s The G1000 system should be serviced DB MISMATCH Aviation database version mismatch Xtalk is off The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays DB MISMATCH Aviation database type mismatch Xtalk is off The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Install correct aviation database type in all displays DB MISMATCH Terrain database version mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays DB MISMATCH Terrain database type mismatch The PFDs and MFD have different terrain database types installed Install correct terrain database type in all displays 190 00600 02 Rev A 63 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang SoJnjeo aoueplony SoJnpa204d Duiuue d AEN 540 S24V oipny uadx 5721 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy 3 EE x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix bres Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Obstacle database version mismatch Comments The P
94. s an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function is not be capable of estimating your position an
95. s 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 Annun Alerts Appendix Index Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 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 In the FLT ID field updating is momentarily displayed Do not perform any other G1000 functions until updating is no longer displayed 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 Press the ENT Key again to transfer the frequency to the active field 8 Turn the la
96. serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The G1000 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 69 s m p q e uepioAy SoJnpa204d Duruue d AEN 540 S24V oipny uadx 5721 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy dd EE x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix ee 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 m
97. should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM needs service Return unit for repair The system has detected a failure in COM1 and or COM2 1 and or COM2 may still be usable The G1000 system should be serviced when possible COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR 2 remote transfer key is stuck The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach
98. sors is gt 200 ft 4 f both airspeed sensors detect 35 knots this is inhibited f eithe ts airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 ts f eithe airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 Differe nce in heading sensors is 6 degrees Difference in p ch sensors is 5 degrees Differe nce in roll sensors is 6 degrees YR eR e No data from one o both altitude sensors n one o TARLA No data from one or both airspeed sensors ICE Ee No data fron both heading sensors iB Ee No data fron n one o both pitch sensors OIM ORO No data from one o both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Sensor Window Text Condition Both DE Ds are di sp f aying data from the n c mber one Air Data Computer Both DE Ds are di sp f aying data from the n mber two Air Data Computer Both System DE Ds are di sp f aying data from the n mber one Attitude amp Heading Reference Both System DE Ds are di sp f aying data from the n c mber two Attitude amp Heading Reference Both DE Ds are di sp aying data from the number one GPS receiver Both DE Ds are di sp
99. t software installed The G1000 system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The G1000 system should be serviced GTX 33 MESSAGE ADVISORIES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d MANIFEST GTX1 software mismatch communication halted The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced The transponder has incorrect software installed The G1000 system should be serviced MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR2 SRVC XPDR2 needs service Return unit for repair 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 68 Garmin G1000 Cockpit Reference Guide for the Cessna Citati
100. ta Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A dh GARMIN Nanings Caulons amp Notes A NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars 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 A NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang A Warnings Cautions amp Notes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Fesuiisr Change Summary 190 00600 00 RevA Initial release Rev B Added Additional Features section 190 00600 01 RevA 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 00
101. te the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 28 1 2 3 4 5 Press the FPL Key to display the Active Flight Plan Page on the MFD 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 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so on To change the user waypoint name follow the procedure for modifying a user waypoint Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A 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 K
102. tem should be serviced The PFD2 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The G1000 system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists PFD2 DB ERR PFD2 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 basemap database error exists database error exists PFD1 DB ERR PFD1 basemap PFD2 DB ERR PFD2 basemap database error exists 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 G1000 system should be serviced 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang soJnjeoJ 2 AEN Sd 2 olpny uqax svoli siu umn sul paezey nubi Juo ney Wil j
103. ter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active 23 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sjuauimasu iui 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi sual uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com Fight EICAS Instruments XPDR Audio AFCS Flight Procedures Planning GPS Nav Hazard Features Avoidance Additional Abnormal Operation Appendix Index Flight Planning A GARMIN INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If necessary press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed Enter the new flight plan waypoint by o
104. 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 SHE unuuy gt 5 3 m x 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang u Additional Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A GARMIN Appendix TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coast lines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional feature INSET SENSOR rro o8s DI ADF DME XPDR IDENT TMRREF NRST MSG LA S D S HO DAD D E L IL IL 1 LA EY F3 V3 V3 V3 P3 73 Select the BACK Softkey to return to the top level softkeys Sensor Softkeys SENSOR Displays softkeys for selecting the 1 and 2 AHRS and Air Data Computers ADCI Selects the 41 Air Data Computer ADC2 Selects the 42 Air Data Computer AHRSI Selects the 1
105. titudes will be displayed as small light blue text Altitudes that have been 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 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 Small Text Altitude is not designated to be used in determining vertical light path guidance Altitude has been retrieved from the navigation database and is provided as a eference n White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot 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 Altitude is designated for use in giving vertical flight path guidance Altitude has been etrieved from the navigation database or has been entered by the pilot and matches a published altitude
106. tware versions installed The G1000 system should be serviced CAS INOP No Dispatch Software correction required The MFD and or PFDs have a software mismatch A red X will appear in the CAS display The G1000 system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G1000 system should be serviced A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 60 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message CNFG MODULE PFD1 configuration module is inoperative Comments The PFD1 configuration module backup memory has failed The G1000 system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD1 voltage is low The G1000 sys
107. 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 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 16 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A GARMIN 0 GPS Navigation 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 Th
108. y Or 190 00600 02 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang sjuauimasu yp 5721 oipny uddx UI0JNeN 52 s mp oold Duiuue d AEN Sd5 fila sual uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey 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 7 8 9 10 A GARMIN 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 After pressing the ENT Key the cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint Press the ENT Key The cursor is now placed for entering another reference waypoint if desired 11 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 2 3 4 5 6 7 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the FMS Knob to activate the cursor
109. y waypoint has been chosen the waypoint ahead of the cursor position 5 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 6 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted 7 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 1 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 MFD FPL Key and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in wh
110. yed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190 00600 02 Rev A GARMIN LLL Procedures the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 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 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key 10 ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Turn the large

Garmin Software Version 0435.11 Cockpit Reference Guide

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