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Garmin CitationJet Model 525 Cockpit Reference Guide

1. Advisory Annunciations Message Advisory Alerts Comparator Annunciations sssssseee nnn Reversionary Sensor Annunciations TAWS A Alerts sss tnter ttt TAWS B Alerts uu esp eid atia da Gr oe och ordeo Aural Alerts s AFCS ALERTS een he hf BAS Flight Plan Import Export Messages MFD amp PFD Message Advisories Database Message Advisories GMA 1347D 20 Message Advisories GIA 63W Message Advisories sss GEA 71 Message Advisories ssssssssseeee nnn GTX 33 33D Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories sssssssssseeee nne GDL 59 Message Advisories GSR 56 Message Advisories GDL 69A Message Advisories GWX 68 Alert Messages GDC 74B Message Advisories GCU 475 Message Advisories GMC 710 Message Advisories GTS 820 Message Advisories Miscellaneous Message Advisories sssssss 190 01130 00 Rev A Garmin G10009 Cockpit Reference Guide for the Cessna Citationlet Model 525 l Table of Contents GARMIN TELEHUU 5 07 PFD Softkey Map cccccccccccsssssssssssssssssssssssssssssscsssssssssssssssssssss
2. 77 555 40 HAZARD AVOIANEE oo acea ia aliia 4 Customizing the Hazard Displays on the Navigation Map 4 STORMSCOPE Optional XM Weather Subscription Optional Traffic Systems RN GER EAE Terrain Awareness amp Warning System ssssssssseeen 46 Airborne Color Weather Radar 50 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN table of Contents ADDITIONAL 5 ne Synthetic Vision Terminal Procedure Charts sse AOPA Airport Directory 5 5 Satellite Telephone Communication Optional XM Radio Entertainment Subscription Optional 61 ABNORMAL OPERATION Reversionary Abnormal COM Operation Audio Panel Fail safe Hazard Displays with Loss of GPS Position Unusual 5 Dead Reckoning ANNUNCIATIONS amp
3. oipny uadx 0105 AEN the selection made level to return to the top softkey level in the map setup options optional optional optional TRAFFIC ToPo T TERRAIN AIRWAYS STRMSCP L NEXRAD xMLmNs T BACK AIRWY ON AIRWY LO AIRWAY HI o wu z t lt to the previous softkey level Press the BACK Softkey to pil Duruue d Wil oar oat 1 AccePT Back Press the BACK Softkey to return 5 to the previous softkey level Y 1 0 1 4 0 1 BACK EY ES V3 V3 v3 V3 YF SoJnpa20Jd MFD Softkeys aoueplony paezey TARGTNI Accesses the softkeys for selecting the target N1 thrust mode and ground Outside Air Temperature OAT TO GA Selects the takeoff go around target N1 thrust mode soJnjeoJ jeuonippy uoneiedo Jeuuouqy CLB Selects maximum climb target Nl thrust x mode 25 CRU Selects maximum cruise target N1 thrust mode gt 5 o z m x x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 103 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix OFF GND OAT TRAFFIC TOPO TERRAIN AIRWAYS 1 0 1 1 0 1 OAT OAT ACCEPT A GARMIN Accesses the softkey
4. 3 m x x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 101 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix IDENT TMR REF NRST ALERTS VFR CODE IDENT ADS B TX 0 7 BKSP A GARMIN Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection softkeys 0 7 Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Activates deactivates transmission of the aircrafts three dimensional position and aircraft heading for reception by ADS B systems Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window 102 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Appendix MFD SOFTKEY MAP sjuauimnasu sub DCLTR zw CHRT Es A n optional 53 gt oca CRU MAN orc eoar n ovS a Default softkey is dependant on Press the BACK Softkey on this
5. Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 2 3 4 5 6 7 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan near
6. paezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 54 GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION OPTIONAL sjuauimasu nubi WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic oipny uddx UI0JNeN 52 Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the 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 Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVS enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display 2
7. Duruue d AEN Sd5 nf eouepioAy paezey s m e q jeuonippy 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 xipueddy suelv uoneiedo junuuy Jeuuouqy x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 55 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A 5 GARMIN Displaying Pathways NOTE Pathways are not available when the cross pointer X Pointer flight director format is selected 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 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 TERMINA
8. Fax 4410870 8501251 orage m u 2nd Road Shiir Taipei County Taiwan Fax 886 02 2642 9099 n ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 n no part of this manual may be reproduced copied edium for any purpose permission of Garmin Garmin hereby grants permission to at any unauthorized commercia ibited this manual onto a hard drive or ided that such electronic ion of this manual or any ed trademark of Garmin Ltd or its subsidiaries WATCHS FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express NavData is a regist permission of Garmin ered trademark of Jeppesen Inc and XM is a registered trademark of XM Satellite Radio Inc Honeywell and Bendix King are registered trademarks of Honeywell International Inc CO Guardian is a trademark of CO Guardian Inc May 2010 190 01130 00 Rev A Printed in the U S A amp Warnings Cantans amp Notes WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoid
9. CHECKLIST Con2 GDC1 UDLE3 1 DATABASE VERSION CYCLE 6142 L ki 3 20 EFFECTIVE GEA 6141 GMA1 2 EXPIRES t 2009 Aircraft Ovners an CHART BOTTOM CARD GP51 CHART REGION GRS1 202 CYCLE 551 175 293 201 EFFECT VE GPS2 EXPIRES DISABLES Co ht 200 652 GSA PTCH CTL LRU Display Database Selection Softkey AUX System Status Page The Display Database Selection Softkey is used to place the cursor in the Database Window Upon first press of the Display Database Selection Softkey the softkey will change to a selected state black text on gray background and the cursor will appear in the Database Window At this point the user can scroll through all databases in the Database Window to view status information If the Display Database Selection Softkey is pressed repeatedly the softkey will switch between PFD1 PFD2 and MFD1 Database status information in the Database Window will reflect the database of the selected PFD or MFD 106 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN 00 Appendix ez Ds FT Unselected MFDI DB Selected PFD DB Selected Display Database Selection Softkey Garmin Databases The following databases are stored on Supplemental Data Cards provided by Garmin Expanded basemap Obstacle Airport Directory Terrain SafeTaxi AOPA Airport terrain FliteCharts After subscribing to the desir
10. DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Tum the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Select the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key 190 01 130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 Press the ENT Key The cursor is displayed in the RAD radial field Enter 29 sjuauimasu sub oipny uadx si U105 AeN 52 2 4 AEN 540 nubi uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A NEW FLIGHT PLAN 30 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created
11. Sue v unuuy O Engine Fan Rotation Speed Engine Oil Pressure and Temperature Interturbine Temperature G Fuel Display Engine High Pressure Turbine Rotation Speed x pu ddy When an unsafe operating condition occurs the pointer and readout color change to indicate a caution yellow or warning red If the time limit for an unsafe condition is exceeded the color of the sliders pointers and digits may change to denote an increase x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 5 iui TL Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Appendix Index A Es GARMIN in priority level even if the parameter is still within the lower priority condition range If sensor data for a parameter becomes invalid or unavailable a red X is displayed across the indicator and or readout Exceedance Levels Slider Slider Norma Exceed k Normal Band Pointer Mid od Exceedance Indicators and Exceedance Levels INTER TURBINE TEMPERATURE When either engine is not running red triangles indicate the ITT limits which must not be exceeded while starting When the respective engine ignitors are on IGN appears in green text at the top of the ITT scales When both engines are running the ITT scale is reduced and the
12. 13 Remove and reapply power to the system Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Canceling an automatic database synchronization 1 While synchronization is in progress press the SYNC DBS Softkey to disable automatic database synchronization 2 Acknowledge the cancelation by pressing the ENT Key 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 Appendix Press the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for each display 109 sainjea4 aoueplony 2 Duruue d AEN Sd5 S241V olpny uqax sia sjuauimasu jeuonippy 2 Wil JUI0 NEN Yid uoneiedo Jeuuouqy Sue v unuuy k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN Loading the Jeppesen navigation database NOTE Loading the Jeppesen navigation database prior to its effective date Will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow 1 Copy the new navigation database to an SD card obtained from Gar
13. Mode selection softkeys 11 Multi Function Display MFD Softkeys 103 N N2 Display 8 NAV 12 NAV1 2 12 NAV2 2 12 82 93 Network 59 61 NEXRAD 43 44 98 105 Index 2 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 Navigation database 21 22 77 79 A GARMIN 0 OBS 2 Obstacles 82 84 Outside Air Temperature OAT 7 Overspeed Protection 16 P Pathvvays 55 56 PIT 70 R Reversionary mode 65 ROC 71 74 S SafeTaxi amp 55 56 Sector scan 52 Secure Digital SD cards 106 Sensor 70 STAB 53 Standby 50 Store Flight Plan 34 Stormscope lightning data 41 42 Strike 41 Strike mode 42 Supplemental Data Card 107 108 SVS 55 96 Synthetic Vision System 55 T TAF 43 TAS 45 46 87 TAWS 46 47 48 49 50 71 72 74 TAVVS A 46 47 48 71 72 73 74 98 TAVVS B 46 48 Telephone 59 Temperature Outside Air 0AT 7 190 01130 00 Rev A A GARMIN Terrain 46 48 71 72 82 98 104 Thrust rating 8 Tilt line 51 Timer 2 93 Topographical data 98 104 Traffic 41 45 104 Traffic advisory 45 Traffic Advisory 44 Traffic map page 45 46 Transponder 11 101 102 V Vertical speed guidance 22 Vertical track 75 VNV 19 66 95 Vspeed 2 W WAAS 84 WATCH 53 Waypoint Selection Submenu 30 Weather Attenuated Color Highlight 53 Weather data link page 43 Weather radar 50 Wind data 100 X XM lightning 98 105 XM weather 43 XPD
14. OK is heard Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A amp GARMIN Hazard Avoidance Display Terrain and Obstacles on the TAWS B Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS B Page If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude EnablelDisable Aviation Data 1 2 3 While the TAWS B 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 LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS B Page is displayed se
15. The UP DOWN field is now highlighted 2 Tum the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN 4 5 6 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey TURN VSPEED BUGS ON OR OFF BY CATEGORY 1 2 3 4 Press the TMR REF Softkey Press the MENU Key Turn the FMS Knob to highlight the desired option Press the ENT Key Press the TMR REF Softkey to remove the window SET BAROMETRIC RADAR ALTIMETER RA OPTIONAL MINIMUM DESCENT 1 2 3 4 5 6 7 ALTITUDE Press the TMR REF Softkey Turn the large FMS Knob to highlight the OFF BARO RAD ALT field t
16. 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 33 oipny uddx 59 sjuaumasu U105 AEN 346 3 52 2 AEN 540 nubi sual uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN STORE A FLIGHT PLAN 1 2 3 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 7 Press the FPL Key for the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FRO
17. 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan SHOW yunuuy gt 5 m x x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 97 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix CCUG ARMIN TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map not available with TAWS A STRMSCP Displays Stormscope data on the Inset Map optional feature NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LTNG Displays XM lightning information on Inset Map optional feature optional Trser SENSOR e qp oss co wwe Tyson prewrJrumme AST TEATS EY EY EY EY EN S ES EY ES Press the BACK Softkey to return to the top level softkeys Exc Tae E 1 peser Ges 1E 1E a 7 Kr uu ou m Es EUM SENSOR Softkeys SENSOR D
18. 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 525 BC Key BC Capture Track for backcourse approaches Approach GPS Arm Capture Track op Approach VOR Arm VAPP Capture Track Captures and tracks selected navigation APR Key Approach ILS Arm Source GPS VOR LOC Capture Track Glideslope Mode automatically armed sauna Disengages autopilot and commands GA GA constant pitch angle and wings level Switch ears in the AFCS Status Box The acceptable bank angle range is indicated in Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 17 sia sjuounasu oipny uadx 0105 AEN ARN Sd5 52 Suelv uoneiedo sainjea4 aoueplony 2 buluueld Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul iui TL paezey GARMIN AFCS Sjueuinijsu fila 59 Tu102 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 18 A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 Press the Direct to Z
19. Key on the MFD or MFD Controller 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob counterclockwise to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MSL or AGL 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation using the PFD 1 Press the Direct to Key E on the PFD 2 Tum the large FMS Knob to place the cursor in the desired selection field GPS Navigation 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob counterclockwise to place the cursor over the ALT altitud
20. Pilots must maneuver the aircraft based upon TCAS II Resolution Advisories if installed 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 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A amp GARMIN Warnings Cautions 5 Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD vveather data should not be used for short range weather avoidance WARNING The G1000 Integrated Flight Deck as installed in the Cessna CitationJet Model 525 aircraft has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the system It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons system operational procedures must be learned on the ground WARNING The United States government operates
21. Sector Scan 6 Press the FMS Knob to remove the cursor Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN 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 Hazard Avoidance When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 53 sjuauimasu nubi AEN Sd5 52 oipny uddx 010 AEN Duruue d nf aoueploay s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul GARMIN Hazard Avoidance Sjueuinijsu nubi 59 U105 AEN s24v AeN Sd5 Duruue d Blank Page 6 2 4 eouepioAy
22. amp Alerts A GARMIN AFCS ALERTS Condition Annunciation Description Pitch Failure PT CH Pitch axis control failure AP is inoperative Roll Failure ROLL Roll axis control failure AP is inoperative MET Switch Stuck PT RM If annunciated when AP is engaged take control of the or Pitch Trim Axis aircraft and disengage the autopilot If annunciated Control Failure when AP is not engaged move each half of the MET Switch separately to check if a stuck switch is causing the annunciation Yaw Damper Failure YD control failure AP also inoperative System Failure AP and MET are unavailable FD may still be available Elevator Mistrim Up A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose up control wheel force upon autopilot disconnect Elevator Mistrim Down A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose down control wheel force upon autopilot disconnect Aileron Mistrim Left A condition has developed causing the roll servo to provide a sustained left force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Aileron Mistrim A condition has developed causing the roll servo to provide Right a sustained right force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits
23. be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS 1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The system should be serviced MANIFEST GRS2 software mismatch communication halted The 2 AHRS has incorrect software installed The system should be serv
24. fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system 9 flashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page 10 The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system 11 The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system 12 The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD 13 The flashing cursor moves to the air temperature TOTAL AIRTEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tum the large FMS Knob on the Control Unit to select the WPT pag
25. 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 ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum 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 Tum the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 final approach course becomes the active leg 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 39 sjuauimasu sub oipny udax si U105 AeN 52 AEN 540 buluueld ni s mp old uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 40 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confi
26. information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information 190 01130 00 Rev A Garmin 610002 Cockpit Reference Guide for the Cessna CitationJet Model 525 43 ARN Sd5 S24V olpny uqax 59 UI0 AeN buluueld ni aoueploay s mp oold paezey Sue v uoneiedo SaJnjeoJ Junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance Ss GARMIN Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cyclone Warnings AIREPs City Forecast Icing Potential WWE Cell Movement Freezing Levels l Turbulence PIREP XM Lightning METARs Surface Analysis County Warnings Cloud Top SIGMETS AIRMET5 Winds Aloft TRAFFIC SYSTEMS A WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic e If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Softkey is displayed Ifa Traffic Advisory System TAS or TCAS I system is con
27. is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 5 Press the ENT Key 190 01130 00 Rev A Garmin 610002 Cockpit Reference Guide for the Cessna CitationJet Model 525 41 Duruue d ni aoueploay s mp oold paezey Sue v uoneiedo SaJnjeoJ Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 42 6 Turn the large FMS Knob to place the cursor in the STRMSCP MODE field 7 Turn the small FMS Knob to display the Cell Strike window 8 Turn either FMS Knob to select Cell or Strike Press the ENT Key 9 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or
28. its flight plan catalog st orage location COPY A FLIGHT PLAN 1 Press the 2 Turn the s 3 Press the FPL Key on the MFD or MFD Control Unit mall FMS Knob to select the Flight Plan Catalog Page FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan 4 confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the 2 Turn the s 3 Press the FPL Key on the MFD or MFD Control Unit mall FMS Knob to select the Flight Plan Catalog Page FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Select the DELETE Softkey A Delete flight plan 1 confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 35 oipny uddx s q sjuauimasu U105 AEN 1614 S24V SoJnpa20Jd 4 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight I
29. manually in the case of PFD1 or PFD2 failure In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Manual 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 2 By pressing the DISPLAY BACKUP Button on the right audio panel NOTE The Cessna CitationJet Model 525 Airplane Flight Manual AFM always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios AUDIO PANEL FAIL SAFE OPERATION If there is a failure of both Audio Panels a fail safe circuit connects the pilot s headset and microphone directly to the COMI transceiver and the copilots headset directly to the COM2 transceiver Audio is not available on the speakers If there is a failure of one Audio Panel that side only has access to their respective on side fail safe COM NOTE Audio is not available on the
30. more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 71 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy IPM PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs servic
31. satellite network 4 Press the ENT Key OK is now highlighted 5 Press the ENT Key again to make the call Adding Another Phone to an Active Call 1 Select the CONF Softkey on the MFD 2 Press the ENT Key The cursor now highlights the phone number entry field 3 Enter the phone number as discussed earlier for making an external call on the Iridium satellite network 4 Press the ENT Key OK is now highlighted 5 Press the ENT Key again to make the call XM RADIO ENTERTAINMENT SUBSCRIPTION OPTIONAL The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 61 xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d buluueld AEN Sd5 52 olpny uqax SI3 sjuauimasu unuuy Jeuuouqy jeuonippy paezey nu U10 AEN 3 x pul Flight Instruments Nav Com XPDR Audio Fl
32. speakers in case of an Audio Panel and its cross side GIA unit simultaneous failure If there is a failure of one Audio Panel the remaining Audio Panel does not have access to the other sides COM or NAV For example if the pilot side Audio Panel 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 65 eoueproAy Senpa204d AEN 540 52 oipny uddx 53 sjueuinsu puezey ubi U105 AEN 3461 saunqee4 Jeuonippy Sue v unuuy xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operations GARMIN fails the copilot side Audio Panel has access to all the radios except for COM1 and NAVI In this case the copilot can receive the audio from NAV2 and operate COM2 for transmission reception In addition if there is a failure of one Audio Panel the following functions are no longer available on the failed side NAV ILS audio speaker cockpit cockpit passengers intercom aural warning alerts on headset entertainment inputs and digital recording radio Also if a stereo headset is in use and an Audio Panel fails only the left channel will be heard in the headphones HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are r
33. the Cockpit 1 Press the TEL Key on the appropriate audio panel 2 Select the ANSWER Softkey on the MFD Or While viewing the AUX TELEPHONE Page 1 Press the TEL Key on the appropriate audio panel 2 Press the MENU Key to display the Page Menu 3 Turn either FMS Knob to place the cursor on Answer Incoming Call 4 Press the ENT Key Selecting the IGNORE Softkey will extinguish the pop up window and leave the call unanswered Selecting the TEL Softkey will display the AUX TELEPHONE allowing additional call information to be viewed before answering 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 59 xipueddy Suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimasu Tunuuy Jeuuouqy jeuonippy paezey nu U10 AEN 3 x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features ARMIN Muting Incoming Call Alerts 1 2 3 With the AUX TELEPHONE Page displayed press the MENU Key on the MFD to display the Page Menu Turn either FMS Knob to place the cursor on Mute Incoming Call Alerts Press the ENT Key The voice alert is muted and the pop up alert will not be displayed when an incoming call is received Making a Call
34. 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 system utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the system can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Cessna CitationJet Model 525 Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the system to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING The illustrations in this guide are only examples Never use the system to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 amp Wamings Cautions amp Notes 0 GARMIN WARNING Lamp s inside this pr
35. to the Cabin 1 2 3 4 Press the TEL Key on the appropriate audio panel Select the DIAL Softkey on the MFD Press the ENT Key The cursor will move from CABIN to OK Press the ENT Key again The cabin phone ringing symbol will now be displayed To exit the call select the HANGUP Softkey Making an External Call from the Cockpit Using the Iridium Satellite Network 1 2 3 4 5 6 7 Press the TEL Key on the appropriate audio panel With the AUX Telephone Page displayed select the DIAL Softkey on the MFD Turn the small FMS Knob to select IRIDIUM Press the ENT Key The cursor has now moved to the phone number entry field Enter the desired telephone number by selecting the number softkeys on the MFD or by pressing the numeric keys on the Control Unit Press the ENT Key OK is highlighted Press the ENT Key The system will begin calling the number To exit the call select the HANGUP Softkey Placing a Call on Hold 60 Select the HOLD Softkey on the MFD Select the HOLD Softkey again to resume the call Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN Additional Features Transferring a Call 1 Select the TRANS Softkey on the MFD 2 Press the ENT Key The cursor now highlights the phone number entry field 3 Enter the phone number as discussed earlier for making an external call on the Iridium
36. uoneiedo Jeuuouqy su jy unuuy x pu ddy x pul nb TL Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 2 3 A GARMIN Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView Select the GO BACK Softkey to return to the previous page View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart will be displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Da
37. while the aircraft is at FLC Key Flight Level Change dimbing descending to the Selected Mach Hold Altitude FLC M nmn 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 16 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN No annunciation am green along the Ro 190 01130 00 Rev A le of the Attitude Indicator AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle Low Bank Limits maximum commanded roll angle HDG Heading Select Captures and tracks Selected Heading Key HDG Navigation GPS
38. with PFD Terrain or Obstacle databases TAWS B System Test Fail TAWS FAIL 57 Terrain or Obstacle database unavailable or invalid invalid TANS System software configuration system TAMS FAIL Failure audio fault 2 TAWS Not D No GPS position TAMS N A Available Excessively degraded GPS TAWS Not signal Out of database TAWS N A None Available coverage area Sufficient GPS signal received TANS None None MM after loss Available AURAL ALERTS Aural Alert Description Minimums minimums The aircra decision altitude f t has descended below the preset minimum descent altitude or Vertical track The aircra f tis one minute from Top of Descent Issued only when vertical navigation is enabled Traffic The Traffic Information Service TIS has issued a Traffic Advisory alert TIS not available The aircra t is outside the Traffic Information Service TIS coverage area not available when a TAS system is installed 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 75 s n e 4 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimasu p ezeH nubi uio AeN Yid jeuonippyv uoneiedo Jeuuouqy 3 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Appendix Index Annunciations
39. 0 Cockpit Reference Guide for the Cessna CitationJet Model 525 79 s mnp q 2 Buruuejd AEN Sd 2 olpny uqax sia siu umn sul paezey nubi nubi jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap database error exists Comments The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle d
40. 00 Rev A GARMIN Additional Features Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select the PRESETS 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 Selecting the MORE Softkey repeatedly cycles through the preset channels 3 Select the SET Softkey 4 Select any one of the PS1 PS15 softkeys to assign a number to the active channel 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 63 xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 52 olpny uqax sia sjuauimasu unuuy Jeuuouqy jeuonippy paezey nu U10 AEN 3 x pul GARMIN itional Features Add Ssjueuinijsu nubi 59 U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey So1njeoj uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 64 GARMIN Abnormal operation ABNORMAL OPERATION REVERSIONARY MODE If the system detects a failure in the MFD reversionary mode is entered automatically Reversionary mode must be entered
41. 1130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 107 uone1edo So1njeo4 aoueplony SoJnpa204d Duruue d AeN Sd5 S24JV oipny uadx 513 sjueumasu Jeuuouqy Jeuonippy puezey fila U105 AEN 3461 Sue v unuuy DR Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN Jeppesen Databases NOTE The Jeppesen aviation navigation database is now referred to as the navigation database Previously this database had been referred to as the aviation database The ChartView database should be copied to the Supplemental Data Card which will reside in the bottom card slot on the MFD The navigation database is be loaded from the Jeppesen or user supplied SD data card Contact Jeppesen www jeppesen com for subscription and update information The navigation database is loaded from an SD card inserted into the top card slot of each displayed The database is copied from the SD card in the top card slot to the displays internal memory Loading Updated Databases In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features Loading the Garmin database upd
42. C 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 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 2 Press the appropriate Frequency Transfer Key to place the frequency into the active frequency field Or 1 Press the COM or NAV Key on the MFD PFD Control Unit to select the desired COM or NAV frequency box 2 Tum the FMS Knob to tune the desired frequency large knob for MHz small knob for kHz 3 Press the Frequency Transfer Key to transfer the frequency to the active field Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Nav Com XPDR Audio Panel INTERCOM SYSTEM ICS ISOLATION Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may sele
43. CEDURE 38 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 displayed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN 5 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 Tum the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO or optional RAD ALT 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD
44. CitationJet Model 525 93 s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V oipny uadx 913 sjueumasu puezey 346 wio gt AeN ubiu jeuonippy uoneiedo Jeuuouqy Do x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ec Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message FPL TRUNC Flight plan has been truncated Comments This occurs when a newly installed navigation 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 WPT ARRIVAL Arriving at waypoint boxx 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 Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to tum 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 Airs
45. D1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 81 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy n EE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operatio
46. ENT Key During the test TAWS TEST is displayed in the center of the TAWS A Page When all is in working order TAWS System Test OK is heard Displaying the TAWS A Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS A 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 increase the display range or rotate counter clockwise to decrease the display range Terrain Obstacle Location Terrain Obstacle above or within 1007 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude EnablelDisable Aviation Data 1 While the TAWS A Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Inhibiting Enabling FLTA and PDA Alerting 1 Select the TAWS A Page 2 Press the TAWS INH Softkey to inhibit or enable TAWS A choice dependent on current state Black 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 4 AEN 540 52 orpnyyuqax sia siu umnnsul Tuo2 AEN iui Duruue d ni s mp oold paezey SH lV
47. ERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operation If the problem persists the system should be serviced 6 51 FAIL 6 51 is inoperative G S2 FAIL G S2 is inoperative 190 01130 00 Rev A A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 85 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy jns PE x pul Hight Instruments Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Additional Abnormal Operation Index Appen
48. FD Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes TAWS is also disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 68 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN Amnunciations amp Alerts ANNUNCIATIONS amp ALERTS ADVISORY ANNUNCIATIONS Annunciation Alerts Window Text Window Text AVN FAN 1 FAIL Avionics cooling fan 1 is inoperative AVN FAN 2 FAIL Avionics cooling fan 2 is inoperative PFD 1 FAN FAIL PFD 1 cooling fan is inoperative PFD 2 FAN FAIL PFD 2 cooling fan is inoperative MFD FAN FAIL MFD cooling fan is inoperative NOSE FAN FAIL Nose avionics cooling fan is inoperative PANEL FAN FAIL Instrument panel avionics cooling fan is inoperative MESSAGE ADVISORY ALERTS Alerts Window Message WOW FAULT Miscompare between weight on wheels inputs WOW INVALID Weight on wheels inputs invalid from GIA TAWS GEAR FAULT Landing gear detected in the down position TAWS FLAP FAULT Flaps detected in the landing position COMPARATOR ANNUNCIATIONS Note that operating the system in the vicinity of metal b
49. G 1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna CitationJet Model 525 A GARMIN Copyright 2010 Garmin Ltd or its subsidiaries All rights reserved 1 Garmi Tel 913 397 8200 5 Tel 503 391 3411 i Sout Tel 44 0870 8501241 Tel 886 02 2642 91 Web Site Address www garmin com Except as expressly provided herei transmitted disseminated downloaded or stored in any st without the express writt download a single copy of th other electronic storage m or printed copy of this manual or notice and provided furthe revision hereto is st Garmin is a registe 99 ictly p This manual reflects the operation of Syste CitationJet Model 525 Some differences Garmin Corporation No 68 Jangsh For after hours emergency aircraft o en edi th oh is manual and of any revision to um to be viewed for personal use prov evision must contain the complete text of this copyright distribut Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Fax 503 364 2138 m Software version 1162 00 or later for the Cessna in operation may be observed when comparing the information in this manual to earlier or later software versions nternational Inc 1200 Fast 151st Street Olathe Kansas 66062 U S A Fax 913 397 8282 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park ampton 5040 9RB U K
50. GS INH Yes 1 Yes 1 Yes Yes Yes Yes Yes Yes Yes No Yes GP INH Yes 1 Yes 1 Yes Yes Yes Yes Yes Yes Yes No Yes FLAP OVR Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Alert available unless GPS signal is invalid or unavailable VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available Only the portions of FIT Alerting based on flap position are disabled when FLAP OVR annunciation is displayed 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 73 s m SoJnpa20Jd Duruue d AEN Sd5 52 olpny uqax sia sjuauimasu 2 nubi iui jeuonippy uoneiedo Jeuuouqy PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ed Annunciations amp Alerts A GARMIN TAWS B ALERTS PFD MFD MFD Alert Type 1 TAWS B Page Aural Message M Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance Pull Up Warning RTC Imminent Terrain PULL UP Terrain Terrain Pull Up Impact Warning ITI Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Ob
51. IALS FROM OTHER 26 1 2 3 4 5 6 7 8 9 10 WAYPOINTS Turn the large FMS Knob on the Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows Garmin 61000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN FlightPlamning 11 12 13 14 15 16 a When a flight plan is active turning the small FMS Knob to the left will display a list of t
52. IDE CYCLE 0313 sjueuinasu nubi EFFECTIVE 17 0 09 EXPIRES 14 10 si Copyright 2009 Jeppesen Sanderson Inc BASEMAP BOTTOM CARD oipny uddx UI0JNeN REGION WORLDWIDE VERSION 3 00 GARMIN LTD AND ITS SUBSIDIARIES 2008 SAFETAXI BOTTOM CARD a REGION VERSION 8 z 2 Check Database Cycle Number MFD shown saunqea4 2 Buruuejd Jeuonippy paezey 16114 uoneiedo Jeuuouqy Sue v unuuy Db 5 o 3 x x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 111 GARMIN Appendix Sjueuinijsu fila 59 u102 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 112 A GARMIN A Activate a flight plan 20 Active Channel 61 ADF 12 ADS B 102 Advisory alerts 69 AHRS 87 88 89 91 92 Airport Signs 55 56 Airways 104 Air Data Computer 70 Alert messages 90 ALT 45 Altimeter setting 1 Altitude mode 45 Altitude volume 45 Antenna stabilization 53 Antenna tilt 51 AOPA s Airport Directory 58 AP 76 Attitude amp Heading Reference System 70 Audio Panel 65 Audio panel controls NAV1 NAV2 12 Autopilot 76 Barometric Alti
53. If the problem persists the system should be serviced COM1 RMT XFR COM remote transfer key is stuck COM2 RMT COM2 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 system should be serviced 84 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message with other NAVS LOI GPS integrity lost Crosscheck Comments GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 S
54. L 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 56 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN Additional Features control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Selecting the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Selecting the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Selecting the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Selecting the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by t
55. M THE FLIGHT PLAN 34 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key 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 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the 2 Tum the s 3 Press the FPL Key on the MFD or MFD Control Unit mall FMS Knob to select the Flight Plan Catalog Page 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 Flight Planning 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in
56. Planning Page 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode select the AUTO or MANUAL Softkey 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 23 oipny uddx s q sjuauimasu U10 AEN 1614 52 2 AEN 540 nubi uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 4 For a b o d Or Fo a b d Or A GARMIN Direct to planning Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the 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
57. R A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 Press the XPDR1 or XPDR2 Softkey to select the active transponder 3 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 4 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 Nav Com XPDR Audio Panel the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 11 Sjueumasu S24V olpnyyuqax sia JUI05 AEN Suelv uoneiado saunyea4 aoueplony 2 ARN 540 unuuy jeuuouqy jeuonippy paezey xipueddy x pul iui Wfl Flight Instruments Flight Planning Abnormal Additional Hazard Avoidance Annun Nav Com AFCS XPDR Audio EIS GPS Nav Procedures Appendix Alerts Operation Features Index Nav Com XPDR Audio Panel A GARMIN SELECT TRANSPONDER MODE 1 2 3 Press the XPDR Softkey If the aircraft is equipped with two transponders press the XPDR1 or XPDR2 Softkey to select the active transponder Press the desired transponder mode softkey STBY ON ALT or GND SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MI
58. R Softkey 11 190 01130 00 Rev A Garmin G10009 Cockpit Reference Guide for the Cessna CitationJet Model 525 ndex 3 sainjea4 e uepioAy 2 Duruue d AEN Sd5 24JV olpny uqax sia sjuaumasu Jeuonippy 2 ni Tuo2 NeN sub uoneiedo Jeuuouqy Sue v unuuy EN d GARMIN index Sjueuinijsu sub 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy mu 190 01130 00 Rev A Index 4 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 A GARMIN im Garmin International Inc j 1200 Fast 151st Street a _ Olathe KS 66062 U S A p 913 397 8200 f 91 WEE Tt aa o 2345 Turner Road SE ia OR 97302 USA 1 O 2010 Garmin Ltd or its subsidiaries 190 01130 00 Rev A
59. Reference Guide for the Cessna CitationJet Model 525 7 sjueuinasu sub MU xipueddy suelv uoneiedo sainjea4 aoueplony saunpadold Duruue d AEN Sd5 S241V olpny uqax junuuy Jeuuouqy Jeuonippy paezey 34 u102 AEN x pul iz Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning AFCS Procedures GPS Nav Appendix Alerts Operation Features Index A Es GARMIN The N2 readouts are located beneath the ITT display Readouts normally appear in green An N2 exceedance readout will appear in red If the readout is out of range dashes will be displayed instead of a readout Target Thrust Mode Ru N14 Ni Target Value Warning Readout Line NI Target Bug NI Readout N1 Display N2 Display TARGET N1 THRUST MODE When the system is powered up on the ground the TO GA target thrust mode is shown in light blue subdued text and the N1 target readout box displays dashes After the ground OAT is accepted the target thrust mode is shown in light blue the NI target readout box contains the target N1 percentage and the target N1 bugs are displayed along the vertical scale for each engine If the flight conditions or air data are out of range the selected target thrust mode is shown in light blue subdued text the N1 target readout is replaced with dashes and the N1 target bugs are removed from display Indication Target Thrus
60. Rudder Mistrim Left A condition has developed causing the yaw servo to provide a sustained force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Rudder Mistrim A condition has developed causing the yaw servo to Right provide a sustained force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Preflight Test yo F Performing preflight system test Upon completion of the test the aural alert will be heard uz EH BE EEE Preflight system test has failed 76 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only User waypoints imported success fully No stored flight plan data was modified The file stored on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified o flight plan files found to import Flight plan import failed The SD card c
61. Terrain Terrain Pull Up Clearance Warning RTC Pull Up Imminent Terrain Impact PULL UP Terrain Terrain Pull Up Warning ITI Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance Up Pull Up Warning ROC Imminent Obstacle Impact ETS Obstacle Obstacle Pull Warning 101 Up Pull Up Excessive Descent Rate PULL UP lt whoop gt lt whoop gt Warning EDR Pull Up Excessive Closure Rate PULL UP lt whoop gt lt whoop gt Warning ECR Pull Up Reduced Required Terrain TERRAIN CAUTION TERRAIN Caution Terrain Caution Clearance Caution RTC TERRAIN Terrain Imminent Terrain Impact TERRAIN CAUTION TERRAIN Caution Terrain Caution Caution ITI _TERRAIN Terrain Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Obstacle Clearance Caution Obstacle Caution ROC mminent Obstacle Impact TERRAIN OBSTACLE Caution Obstacle Caution 01 TERRAIN Caution Obstacle Premature Descent Alert 1 TERRATN TOOLOW TERRAIN Too Low Terrain Caution PDA Excessive Descent Rate TERRAIN SIKRE Sink Rate Caution EDR Excessive Closure Rate TERRAIN ERN Terrain Terrain Caution ECR egative Climb Rate TERRAIN DOTSK Don t Sink Caution NCR Flight Into Terrain High TERRAIN T00L04 TERRMN Too Low Terrain Speed Caution FIT TERRAIN F
62. The system automatically transitions to the next vertical waypoint The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid TRAFFIC FAIL Traffic device has failed The system is no longer receiving data from the traffic system The traffic device should be serviced NO WGS84 WPT Non WGS 84 waypoint for navigation Doox The position of the selected waypoint xxxx is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint FAILED PATH A data path has failed A data path connected to the GDU GSD 41 GSD 69A or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic cou
63. addy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 24JV oipny uddx junuuy Jeuuouqy Jeuonippy p EzeH fila u102 AEN x pul GARMIN EIS Sjueuinijsu fila SE oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 10 A GARMIN 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 Tum the small FMS Knob to enter the first character 3 Turn the large FMS Knob to select the next field 4 Tum the small FMS Knob to enter the next desired character 5 Repeat steps 3 and 4 until the desired Flight ID is entered 6 Press the ENT Key to update the Flight ID ADF TUNING OPTIONAL 1 Tune the ADF using the remote ADF control head 2 If two ADF systems are installed press the AUX Key on the desired audio panel to monitor ADF2 audio DME TUNING 1 Press the DME Softkey 2 If two DMEs are installed turn the large FMS to select the DME source field 3 Tum the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection 5 If two DMEs are installed press the AUX Key on the desired audio panel to monitor DME2 audio ENTE
64. al 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 White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot the system estimating entered by the pilot use this altitude in the altitude of the Altitude is designated 1 determining vertical aircraft as it passes for use in giving flight path guidance over the navigation vertical flight path point This altitude guidance Altitude is provided as a does not match the reference and is not published altitude in designated to be used navigation database or in determining vertical no published altitude flight path guidance exists Small Text Altitude is not Altitude is designated 1 The system cannot designated to be used for use in giving vertical use this altitude in in determining vertical flight path guidance determining vertical flight path guidance Altitude has been flight path guidance Altitude has been etrieved from the retrieved from the navigation database navigation database or has been entered by and is provided as a the pilot and matche
65. ance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The 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 the GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic
66. ard slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the bottom card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the specified PFD or MFD contains invalid data PFD1 PFD2 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the specified PFD or MFD contains invalid data 96 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A amp GARMIN APPENDIX sjuauimasu sub PFD SOFTKEY MAP optional RET SEO o os p co owe 3908 Tem REA WEST ERTS r r r S 7 um unu mu 59 CDI NAV1 oipny uddx U105 AeN 8 Top Level PFD Softkeys o optional Z wser sewsoR Pro T oss cor owe xeon T IDENT LA 75 NS v3 nn nnn n n9 Duruue d Wil optional optional optional OFF DCLTR TRAFFIC TOPO TERRAIN STRMSCP NEXRAD XM LTNG BACK ALERTS LA S EE F3 M EH 5 amp o EF TRFC 1 Select the BACK Softkey to return to the top level softkeys s snp old TRFC 2 INSET Map Softkeys ge INSET Pressing the INSET Softkey Displays Inset Map in a the PFD lower left corner uoneiedo Jeuuouqy OFF Removes Inset Map DCLTR
67. at a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload airways as needed 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna
68. atabase error exists PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU 80 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists Comments The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PF
69. ates 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the Garmin databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 4 Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 108 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN 5 Acknovvledge the Povver up Page agreement by pressing the ENT Key or DATABASE V Checklist File N A Basemap Land 2 00 SafeTaxi N A A a Terrain Data N A Airport Terrain Data N A gt lt Obstacle Data N A z l Apt Directory N A BY Chart Data N A All map and terrain data provided is only to be used as d general reference to your surrounding and as an aid to situational awareness Database Information on the Power up Screen the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Turn the small FMS Knob to select the System Status Page 8 Make sure the SYNC DBS Softkey is in the enabled state 9 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed 10 11 12
70. ather 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 vveather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Tum 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 Tum the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 4 Select the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARS SIGMETs PIREPs or AIREPs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more
71. by a Radial amp Distance from Another Waypolrt roten dra tete dite Delete a User 1 1 Create a New Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan sss 31 Enter an Airway in a Flight Plan 32 Invert An Active Flight Plan 33 Remove a Departure Arrival Approach or Airway from a Flight Plan 33 Store a Flight Plan co erae t ciet inen 34 Edit a Stored Flight Plan 34 Delete a Waypoint from the Flight Plan sss 34 Invert and Activate a Stored Flight Plan 35 Copy a Flight Plan nnn Delete a Flight Plan ticertmlis Graphical Flight Plan Creation Export a Flight Plan to an SD 36 PROCEDURES eire lb Rr a Load and Activate a Departure Procedure Activate A Departure Leg sssssesseeeeenennnnnnnnnnn Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure 38 Activate An Approach in the Active Flight 7 20 39 Activate a Vector to Final Approach Fix sse 39 Activate A Missed Approach in the Active Flight
72. cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 vievving area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN XM WEATHER SUBSCRIPTION OPTIONAL WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM We
73. ct or deselect the intercom The MAN SQ Key allows either automatic or manual control of the intercom squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator When the MAN SQ Annunciator is extinguished Automatic Squelch is on the ICS Knob controls only the volume pressing the ICS Knob has no effect on the VOL SQ selection When the MAN SQ Annunciator is illuminated Manual Squelch the ICS Knob controls either volume or squelch selected by pressing the ICS Knob and indicated by the VOL or SQ annunciation Cabin Address The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin The annunciator is lit when the cabin intercom is active on either Audio Panel When the flight crew wants to communicate with the passengers the pilot or copilot presses the CABIN Key to signal that communication is desired PASSENGER ADDRESS PA SYSTEM A passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels PA messages are one way from the flight deck to the passengers 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 13 siu umnnsu S24V olpnyygqax SE JUI05 AEN Sue v uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld ARN Sd5 yunuuy jeuuouqy jeuoni
74. d a failure The audio panel is unavailable The system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The system should be serviced 82 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations amp Alerts GMA 1347D 20 MESSAGE ADVISORIES CONT Message GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Config service req d Comments The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMA1 software mismatch communication halted o The audio panel has incorrect software installed The service Return unit for repair u GMA2 SERVICE GMA2 needs service Return unit for repair MANIFEST GMA software system should be serviced mismatch communication halted GMA1 SERVICE GMAT needs The audio panel self test has detected a problem in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message 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 config
75. dix z Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES A GARMIN CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The 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 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The system should be serviced GTX 33 33D MESSAGE ADVISORI ES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d The transponder configuration settings do not ma
76. e Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced MFD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration settings do not match backup configuration memory The system should be serviced The MFD and PFDs have different software versions installed The system should be serviced 78 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reduc
77. e FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired user waypoint d Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 32 1 2 3 4 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Flight Planning 5 Tur
78. e field 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 19 sjuauimasu nubi 59 oipny uddx JUI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony sainpadold Duruue d unuuy Jeuuouqy Jeuonippy 2 xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude constraint 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 offset distance from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT Key again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the MFD or MFD Controller and turn the small FMS Knob to display the Fligh
79. e group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Select the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 25 oipny uddx 59 sjuaumnasu U10 AEN 16114 52 2 4 AEN 540 nubi sual uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A NEW USER WAYPOINT DEFINED BY RAD
80. e there is no heading and or airspeed data available should not be used for navigation 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 67 Sjueuinijsu sub 59 2 4 Buruue d AEN 540 yi oipny sadx paezey 3461 u102 AEN saunqea4 jeuonippy xipuaddy Sue v junuuy x pul Nav Com XPDR Audio Hazard Avoidance Additional Annun Flight Instruments Flight Planning EIS AFCS Alerts Features Procedures GPS Nav Appendix Index Abnormal Operation GARMI N 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 TEESDALESERRE CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DIK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the P
81. ed database product updates these updated databases are copied to each Supplemental Data Card for each display the card that contains the FliteCharts or ChartView database resides in the MFD Since these databases are not stored internally in the displays these Supplemental Data Cards must remain in the bottom card slot of each display NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data Obtaining Garmin Database Updates The Garmin database updates can be obtained by following the instructions detailed in the Aviation Databases section of the Garmin website ly garmin com Once the updated files have been downloaded from the website a PC equipped with an appropriate SD card reader is used to unpack and copy the new databases onto the appropriate Supplemental Data Cards Equipment required to perform the update is as follows Windows compatible PC computer Windows 2000 or XP recommended SD Card Reader SanDisk SDDR 93 SanDisk SDDR 99 Verbatim 96504 or equivalent Updated database obtained from the Garmin website Existing Supplemental Database SD Card 010 00330 41 42 or 43 from the MFD The supplemental data card from the MFD should be used because all databases except the active navigation database are required to reside on this card 190 0
82. eference Guide for the Cessna CitationJet Model 525 190 01130 00 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 Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key on the MFD or MFD Control Unit to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure 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 ar
83. emoved until GPS position is again established Loss of Hazard Functions with Loss of GPS Position UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glide e AFCSAnnunciaions Setup Menu path and Vertical Flight Director Windows displayed in Deviation Indicators Command Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports 2 VNV Target Altitude Window Flight Plan Wind Data Messages Selected Heading Box Procedures Selected Course Box ADF DME Tuning Transponder Status Barometric Minimum Box Descent Altitude Box 66 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN Abnormal Operation Extreme Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and
84. endix Alerts Operation Features Index Hazard Avoidance GARMIN Adjusting Gain WARNING Changing the gain in Weather Mode will cause precipitation 52 intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN field 2 Tum the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position 3 Press the FMS Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Ground Mapping 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Select the BACK Softkey Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turn the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the
85. est recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN IMPORT A FLIGHT PLAN FROM AN SD CARD 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Select the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK Flight Planning or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing
86. f the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN 2217 11 7NM COVIE 221 9 QNM LEMYN 220 8 0NH Approach KDFH RNAV 17LcPs LPY 259 18 8NH 3 3NH 3 2NM 3 9NM RW17L map 76 5 3NM 930FT 8NM POLKE S L M Cross AT or ABOVE 5 000 fi Facing Cross AT 2 300 ft ICI Cross AT or BELOW 3 000 ft 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 Large Whi Text C Large Light Blue Tex cea zd mall Lig Blue Tex S 7 t Blue Subdued Text Small White Text with Altitude Restriction Bar 21 siu uinnsu nubi 59 oipny uadx 0105 AEN suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS Procedures Appendix Alerts Operation Features Index GPS Navigation 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 altitudes will be displayed as small light blue text Altitudes that are designated for use in vertic
87. figured a STANDBY OPERATE or NORMAL TEST and ALT MODE Softkey is displayed Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA TAS and TCAS 1 only intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA Potential collision area is within 20 to 48 seconds GOSS Traffic Advisory Off Scale Traffic Symbol Description 44 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Traffic Information Service TIS Hazard Avoidance NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS or TCAS system TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the OPERATE or NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displa
88. fore taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Select the MODE Softkey If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN Hazara avoidance 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 Adjusti
89. g 1 Enter a Transponder Code 1 Select Transponder Mode sssssssseeeen nnn 2 Selecting a COM Radio sssssseeeen nnn 2 Selecting a NAV Radio 2 NAV COM Tuning R 2 Intercom System ICS Isolation seen 3 Passenger Address PA System 3 Clearance Recorder and Player 4 AUTOMATIC FLIGHT CONTROL SYSTEM 5 Flight Director Activation sss 5 Vertical Modes ert ro Ere cado 6 Lateral Modes tnn 7 9 Direct to Navigation 9 Activate a Stored Flight Plan 20 Activate a Flight Plan Leg 20 Stop Navigating a Flight Plan 21 Vertical Navigation VNAV ssssseseee nnne 21 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 Table of Contents GARMIN FLIGHT PLANNING c a aad 23 Weight Planning 0 ccccccsusssssssssssssssssssssssssssssessssssnscsssssnscsssnssecsssnsnessssnsneesssnnneesssnness 23 Trip Planririg 5 nette aeter itte tete ene uu ds 23 Create a New User Waypoint Defined by Latitude amp Longitude 25 Create a New User Waypoint Defined by Radials from Other Waypoints 26 Create a New User Waypoint Defined
90. ge RR 2 Garmin G10009 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN table of Contents FLIGHT INSTRUMENTS 1 nato aa aaa 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure s s s si s sil 1 Change Altimeter Barometric Pressure Setting Units 1 Synchronizing the Altimeter Barometric Pressure 1 5 5 1 Synchronize CD isis sich uei orina a e HER Change Navigation Sources Enable Disable OBS Mode While Navigating with 6 5 2 GenericTimer eoo ono nn De RD HU Rm anne GaGa 2 Configure Vspeed Bugs Individually sss Turn Vspeed Bugs On or Off by Category Set Barometric Radar Altimeter RA Optional Minimum Descent Altitude 3 Displaying Wind Data 3 ENGINE INDICATION SYSTEM 5 Inter Turbine Temperature ssssssseennnnnnnnnes 6 Ground OAT Set Window 7 Engine SPool Rotation Speeds N1 and 2 7 Target N1 Thrust Mode 8 NAV COM TRANSPONDER AUDIO PANEL 1 Enter or Change Flight ID sssssee nnn 1 ADF Tuning Optionall s s s s s s S nnne 1 DME Tunilij E E ittm eem tta rmm tet t b im h
91. he air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS2 GPS AHRS2 using backup GPS source The 2 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS2 GPS AHRS2 not receiving any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced 190 01130 00 Rev A Garmin 610005 Cockpit Reference Guide for the Cessna CitationJet Model 525 87 so1njeoJ 2 Buruuejd AEN 5640 24V oipny uadx sia syu unysu paezey nubi Wil jeuonippy uoneiedo Jeuuouqy 5 PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix and Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message AHRS1 GPS AHRS1 not receiving backup GPS information Comments The 1 AHRS is not receiving backup GPS information The system should
92. he flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Tum the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint Press the ENT Key Press the FMS Knob to remove the flashing cursor 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 27 oipny uddx 59 sj
93. he pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView Optional ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts Optional FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the 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 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 57 AEN 540 52 olpny uqax sjuounasu U102 AEN eouepioAy 2 s m jeuonippy
94. 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 The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR whil
95. iced 88 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN GMU 44 MESSAGE ADVISORIES Annunciations amp Alerts Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The system should be serviced GDL 59 MESSAGE ADVISORIES Message Comments GDL59 CONFIG GDL 59 config error Config service req d GDL 59 configuration settings do not match those of backup configuration memory The system should be serviced GDL59 FAIL GDL 59 has failed GDL59 SERVICE GDL 59 needs service Return unit for repair A failure has been detected in the GDL 59 The receiver is unavailable The system should be serviced A failure has been detected in the GDL 59 The system should be serviced GDL59 RTR FAIL The GDL 59 router has failed A failure has been detected in the GDL 59 router The
96. ight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 2 3 Select the CATGRY Softkey on the XM Radio Page Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob Press the ENT Key Select an Available Channel within the Selected Category 1 2 3 While on the XM Radio Page select the CHNL Softkey Select the CH Softkey to move down through the list in the Channel Box or move up the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 2 3 4 62 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Select the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130
97. ing power usage Comments The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the system should be serviced 190 01130 00 Rev A Garmin G100
98. isplays softkeys for selecting the 1 and 2 AHRS and Air Data Computers ADCI Selects the 41 Air Data Computer ADC2 Selects the 2 Air Data Computer AHRSI Selects the 1 AHRS AHRS2 Selects the 2 AHRS Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN m tional n nnnwununnwunnnnunx sjuauimasu sub optional optional SYNVIS DFLTS WIND DME1 BRG1 BRG2 DME2 ALTUNIT STD BARO BACK ALERTS 59 nh rs nn wa Select the BACK Softkey to return to the top level softkeys olpny uqax uo2 AEN 52 COR Cae ERR E ee ets r ry rv rv EY EY EY EY S A S L Eom eme oms or L L L L J ec nenrs F3 V3 V3 HU P 09 nmn 75 75 on 74 sr ens aes S Je ee rv vumumumu mumu us PFD Configuration Softkeys Buruuejd NEN Sd5 Wil s mp 01d PFD Displays second level softkeys for additional PFD configurations aoueplony paezey SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction saunqea4 jeuonippy uoneiedo Jeuuouqy HRZN HDG Displays compass heading along the Zero Pitch line Sue v unuuy APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position Airpor
99. ive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Integrated Flight Deck Pilot s Guide 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 amp Warnings tauuens SMotes GARMIN Blank Page Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN Record of Revisions Part Number Change Summary 190 01130 00 Revision Date of Revision Affected Pages 2010 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 RR 1 Record of Revisions Ss GARMIN Blank Pa
100. l 5 FAIL ETT TAWS System Failure GPWS System Fail GPHS FAIL None GPWS System Failure System Test in progress TAWS TEST TAWSTEST None System Test pass None None TAWS System Test OK TANS System Failure GPWS System Fail Radar Altimeter invalid Altitude or Vertical Speed unavailable None MFD Terrain or Obstacle database unavailable or invalid TAWS operating with PFD Terrain or Obstacle databases None 72 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 GPWS System Failure None 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts PFD MFD Additional TAWS A P Alert Type TAWS A Page w age Aural Message ae Annunciation Annunciation TAWS Not Excessively degraded TAWS Not GPS signal or out of None Md Available database coverage area TAWS A Alert Availability TAWS A Alert Type Available TAWS A Status Annunciation RTC ITI ROC IOI PDA EDR ECR NCR FIT GSD VCO Displayed TAWS TEST No No No No No No No No No TAMS N A No No No No Yes Yes Yes Yes Yes Yes 5 FAIL No No No No No Yes Yes Yes Yes Yes Yes TAWS INH No No No No No Yes Yes Yes Yes Yes Yes GPHS FAIL Yes Yes Yes Yes Yes No No No No No Yes
101. lect the INHIBIT Softkey 1 2 3 Or Press the MENU Key Turn the small FMS Knob to select Inhibit TAWS Press the ENT Key 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 49 AEN 540 52 orpnyyuqdax sia Sjueumajsul Tuo2 AEN fid buluueld ni 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 EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey 1 2 3 Or While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key Displaying Terrain and Obstacles on the Navigation Map 1 2 With the Navigation Map displayed press the MAP Softkey Select the TERRAIN Softkey Terrain and obstacles will now be displayed on the map AIRBORNE COLOR WEATHER RADAR 50 WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode be
102. light Into Terrain Gear TERRAIN 100 00 GEAR Too Low Gear Caution FIT Flight ma Flaps TERRAIN 100 0 FLAPS Too Low Flaps Caution FIT 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 71 aoueplony SoJnpa204d buluueld AEN 540 S24JV oipny uadx sia sjueumasu puezey 346 U105 AEN 3461 jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ed Annunciations amp Alerts A GARMIN EFD MED MFD Map Page Alert Type TAWS A Page Hi Aural Message Pop Up Alert Annunciation Flight Into Terrain Takeoff TERRAIN 00 LOW TERRAIN Too Low Terrain Caution FIT Glide Slope Glide Path BEIDESLOPE GLIDESLOPE Glide Slope Caution 7 ar or vo b epends on approac Glide Path type GLIDEPATH s ra Altitude Voice Callout None None Five Hundred Four Hundred optional Three Hundred optional Two Hundred optional One Hundred optional TAWS A System Status Annunciations Terrain or Obstacle database unavallable invalid software configuration or audio unavailable PFD MFD ae Alert Type TAWS A Page ee Message A Annunciation Annunciation TAWS System Fai
103. lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The system 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 panel and displays are subject to change and may not reflect the most current system and databases Depictions of equipment may differ slightly from the actual equipment Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A amp GARMIN Femingi Cautions amp Notes NOTE This device complies vvith part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproduct
104. m one or both pitch sensors o data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Sensor Window Text Both PFDs are displaying Condition data from the n mber one Air Data Computer Both PFDs are displaying data from the n mber two Air Data Computer Both PFDs are displaying Reference System Both PFDs are displaying Reference System data from the n data from the n mber one Attitude amp Heading mber two Attitude amp Heading Both PFDs are displaying data from the n mber one GPS receiver Both PF is displaying data Ds are displaying data from the n rom the mber two GPS receiver 1 Air Data Computer is displayinq data rom the 2 Air Data Computer is displaying data from the 1 AHRS is displaying data from the 2 AHRS is displaying data from the 1 GPS is displayinq data rom the 2 GPS l 0 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts TAWS A ALERTS PFD MFD MFD Map Page Alert Type TAWS A Page prag Aural Message Pop Up Alert Annunciation Reduced Required Terrain MAMMI
105. min or the aircraft manufacturer 2 With the G1000 system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD label of SD card facing left 3 Turn the G1000 system ON A prompt similar to the following illustration is displayed DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL OUERHRITE THE ACTIVE NAVIGATION DATABASE FROM T WORLDWIDE WORLDWIDE 0912 6913 19 1 009 17 DEC 2009 8 EXPIRES 17 0 2009 14 JRN 2818 INO WILL BE ASSUMED IN 28 SECONDS UPDATING NAVIGATION DATABASE PLEASE WAIT Navigation Database Load Prompt 4 Press the YES Softkey to update the navigation database in the MFD 5 After the update completes the display starts in normal mode 6 Turn the G1000 system OFF and remove the SD card from the top card slot 7 Repeat steps 2 through 6 for PFD1 8 Repeat steps 2 through 6 for PFD2 9 Apply power to the system and press the ENT Key to acknowledge the startup screen 10 Turn the large FMS Knob to select the AUX Page group on the MFD 11 12 Press the Display Database Selection Softkey to show navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Tum the small 5 to select the System Status Page 110 Garmin G1000 Cockpit Reference Guide for the Cessna Citationlet Model 525 190 01130 00 Rev A A GARMIN Appendix MFD1 DATABASE NAVIGATION INTERNAL REGION WORLDW
106. mp Alerts GMC 710 MESSAGE ADVISORIES A GARMIN Message GMC CONFIG GMC Config error Config service req d Comments GMC 710 configuration settings do not match those of backup configuration memory The system should be serviced GMC FAIL GMC is inoperative MANIFEST GMC software mismatch Communication halted A failure has been detected in the GMC 710 The GMC 710 is unavailable The GMC 710 has incorrect software installed The system should be serviced GMC KEYSTK GMC key name Key is stuck A key is stuck on the GMC 710 bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists GTS 820 MESSAGE ADVISORIES Message Comments GTS CONFIG GTS config error Config service req d The GTS and GDU have incompatible configurations This alert is also set when the GTS has an invalid mode address configured or the mode S address does not match both XPDR mode S addresses MANIFEST GTS software mismatch communication halted The GTS has incorrect software installed The G1000 system should be serviced 92 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the system detects th
107. n Index Appendix ec Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Navigation database mismatch Xtalk is off Comments The PFDs and MFD have different navigation database versions or types Americas European etc installed Crossfill is off Install correct navigation database version or type in all displays DB MISMATCH Terrain database mismatch DB MISMATCH Obstacle database mismatch The PFDs and MFD have different terrain database versions or types installed Install correct terrain database version or type in all displays The PFDs and MFD have different obstacle database installed Install correct obstacle database 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 NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 1347D 20 MESSAGE ADVISORIES Message GMAT FAIL GMAT is inoperative GMA FAIL GMA2 is inoperative Comments The audio panel self test has detecte
108. n 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 7 Press the ENT Key The system returns to editing the flight plan with the ENT Key LOAD is highlighted new airway inserted INVERT AN ACTIVE FLIGHT PLAN 1 Press the 2 Press the FPL Key to display the active flight plan 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 a Press the MFD FPL Key and turn the small FMS Knob to select the Flight b Press stored flight plan Plan Catalog Page the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints
109. ng 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 Press the MENU Key 2 Turn the large FMS Knob to select Show Bearing Line 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 5 AeN Sd5 S24V oipny uadx sia syueuimasu u102 AEN 1014 Duruue d wold aoueploay s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav App
110. nication halted The GDL 69 has incorrect software installed The system should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX FAIL GWX is inoperative GWX 68 configuration settings do not match those of the GDU configuration The system should be serviced 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 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 90 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN GDC 74B MESSAGE ADVISORIES Annunciations amp Alerts Message ADC1 ALT EC ADC1 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 ADC2 airspeed error correc
111. nstruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index A Flight Planning GARMIN GRAPHICAL FLIGHT PLAN CREATION 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 EXPORT A FLIGHT PLAN TO AN SD CARD 1 2 3 4 5 6 7 36 Insert the SD card into the top card slot on the MFD Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Select the EXPORT Softkey Press the ENT Key to confirm the export Garmin 610007 Cockpit R
112. o the right of MINIMUMS Turn the small FMS Knob clockwise to select BARO or RAD ALT Press the ENT Key Use the small FMS Knob to enter the desired altitude Press the ENT Key To remove the window press the CLR Key or the TMR REF Softkey DISPLAYING WIND DATA 1 2 3 4 Press the PFD Softkey Press the WIND Softkey to display wind data below the Selected Heading Press one of the OPTN softkeys to change how wind data is displayed To remove the Wind Data Window press the OFF Softkey 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 Flight Instruments 3 mal ED g 2 a xipuaddy Suelv uoneiedo sainjea4 aoueplony sainpadoid Duruue d AEN Sd5 52 olpny uqax sia unuuy Jeuuouqy Jeuonippy paezey Wfl U10 AEN x pul Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Flight Instruments Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 A GARMIN 190 01130 00 Rev A A GARMIN 1 L fis ENGINE INDICATION SYSTEM A NOTE Refer to the Airplane Flight Manual AFM for engine limitations Sjueunasu 3f BS BO 524 saunyea4 eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 2 jeuonippy uoneiedo Jeuuouqy EIS Display Engine Run
113. oduct 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 variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean
114. onJet Model 525 190 01130 00 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 AFCS 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 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 acti
115. ontains no flight plan data us Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun cated The flight plan on the SD card contains more waypoints than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Way points locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or
116. or empty flight plan and again select the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint 4 Turn the small FMS Knob The Waypoint Information Window is now displayed 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 31 59 olpny uqax ui0 gt AeN 52 2 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 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 NRST airport waypoints to the aircraft s current position c Turn the larg
117. pace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach PTK FAIL Parallel track unavailable bad geometry The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver Bad parallel track geometry 94 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT 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 VNV Unavailable Unsupported leg type in flight plan The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints
118. ppy paezey xipuaddy x pul iui n Nav Com AFCS XPDR Audio EIS Abnormal Additional Hazard Annun Flight Instruments Flight Planning GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the stored memory blocks starting from the oldest block The PLAY Key controls the play function The PLAY annunciator is illuminated to indicate when play is in progress The PLAY annunciator extinguishes after playback is finished Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation Pressing the PLAY Key again during play of a memory block stops play Ifa COM input signal is detected during play of a recorded memory block play is halted Pressing the PLAY Key twice within one half second while audio is playing plays the previous block of recorded audio Each subsequent two presses of the PLAY Key within one half second backtracks through the recorded memory blocks to reach and play any recorded block 14 Garmin G1000 Cockpit Reference Guide for the Cessna Citati
119. re 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 Softkey only enabled while aircraft is in the air Softkey only enabled while aircraft is on the ground and airspeed is below 20 kias 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 105 sainjea4 eouepioAy 2 Duruue d AEN Sd5 S241V olpny uqax sia sjuauimasu jeuonippy 2 Wil swio AeN qb uoneiedo Jeuuouqy Sue v unuuy ka GARMIN DATABASE UPDATES The system uses Secure Digital SD cards to load and store various types of data For basic flight operations SD cards are required for database storage as vvell as Jeppesen navigation and Jeppesen ChartView database updates Not all SD cards are compatible with the G1000 Use only SD cards supplied by Garmin or the aircraft manufacturer Information regarding the various databases may be viewed on the AUX System Status Page AUX SYSTEM STATUS 136 975 118 888 LRU INFO AIRFRAHE STATUS SERIAL NUMBER VERSION AIRFRAME Cessna Model 525 Citotion Jet CO GUARDIAN 700 SYS SOFTWARE VERSION com 710 CONFIGURATION 10 CRG PART NUMBER SYSTEH ID
120. rea or rotate counter clockwise to display a smaller area 7 Select the FLT ID Softkey to enable or disable Flight ID displayed with the intruder information System Self Test 1 With the Traffic Map Page displayed set the range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert TAS System Test OK is heard If the self test fails the system reverts to Standby Mode and a voice alert TAS System Test Fail is heard Displaying Traffic on the Navigation Map 1 2 3 Ensure TAS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM TAWS A Optional 46 WARNING The TAWS display shows supplemental information only It should not be used for navigation 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 system is configured for a TAWS A installation Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A GARMIN Hazard avoidance Manual System Test 1 While the TAWS A Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Test TAWS System 3 Press the
121. red triangles are removed from display During an ITT exceedance pointer s are displayed in yellow or red and readout s are provided for each engine below the scale showing an exceedance Ignitor On Indication Never Exceed Inter Turbine Temperature Display Inter Turbine Temperature Display Right Engine Start Both Engines Running 6 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Es GROUND OAT SET WINDOW When the aircraft is parked or is taxiing the reported ground Outside Air Temperature OAT for the airport can be set in the Ground OAT Set Window GROUND OAT 21 C Ground OAT Set Window Setting Outside Air Temperature OAT 1 Select the TARGT N1 Softkey 2 Select the GND OAT Softkey to display the Ground OAT Set Window 3 To adjust the temperature in 1 C increments use the and OAT softkeys 4 To confirm the selected takeoff settings and close the Ground OAT Set Window select the ACCEPT Softkey Or To cancel the operation select the BACK Softkey ENGINE SPOOL ROTATION SPEEDS N1 AND N2 The N1 display ranges from 20 to 110 of maximum rotational speed If N1 drops below 20 the sliders are removed from the scale while the readouts remain displayed below Caution or warning conditions cause the exceedance pointer s and readout s to be displayed in yellow or red respectively 190 01130 00 Rev A Garmin G1000 Cockpit
122. rivals 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 Procedures 37 sjuauimasu sub 59 olpny uqax 0105 AEN 52 AEN 540 Duruue d wold s mp old uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures 0000000 GARMIN 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 TO waypoint of the desired leg 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 PRO
123. rmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the go around button Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN 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 Hazard Avoidance 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL sjuauimasu sub oipny uadx 0105 AEN 52 AEN 540 V ARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration VVeather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old 4 Strike is between 6 and 60 seconds old A Strike is between 1 and 2 minutes old Strike
124. rse angles may differ from the actual magnetic heading by more than 2 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 95 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi wio gt AeN ufi jeuonippy uoneiedo Jeuuouqy 3 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations 8 Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT SVS SVS DISABLED Out of available terrain region SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top c
125. rsor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Tum the small FMS Knob to the right to display the NRST airports to the aircraft s current position Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN c Tum the large FMS Knob to select the desired waypoint d Press the ENT Key Or Flight Planning a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 11 the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the
126. s eference a published altitude in the navigation database 22 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN FLIGHT PLANNING WEIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters Flight Planning Turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the Weight Planning Page 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field 2 Enter the 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enter the 5 Press the desired aircraft empty weight desired weight of Pilot amp Stores ENT Key 6 Continue repeating these steps until all desired weights have been entered Entering Fuel Parameters 1 If necessary press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors Or Manually 4 Press the 5 Enter the 6 Press the TRIP PLANNING enter the desired fuel quantity ENT Key The cursor is now in the FUEL RESERVES field desired reserve fuel quantity FMS Knob to remove the cursor 1 Tum the large FMS Knob to select the AUX page group 2 Tum the small FMS Knob to select the Trip
127. s for manually setting the target N1 speed asa percentage Increases the displayed Increases the displayed Decreases the displayed Decreases the displayed Disables the target N1 speed bugs and readout Accesses softkeys for setting the ground outside air temperature OAT Increases the ground OAT setting in one degree Celsius C increments Decreases the ground OAT setting in one degree Celsius C increments Confirms the ground OAT setting and returns to the previous softkey level Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map not available with TAWS A Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed 104 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN STRMSCP NEXRAD XM LING BACK DCLTR 3 SHVV CHRT Appendix Displays Stormscope weather and coverage information on Navigation Map optional feature Displays NEXRAD weather and coverage information on Navigation Map optional feature Displays XM lightning information on Navigation Map optional featu
128. self test has detected a problem in the unit The system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted AGIA mismatch has been detected where only one is WAAS capable MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The G A1 and or GIA 2 has incorrect software installed The system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain Settings are incorrect COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM may still be usable The system should be serviced when possible COM1 PTT 1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation
129. ssessnsssssssessansssssscesansssssnsess 97 LEA ALET 2 103 Database Updates eee etti 106 INDEX LL J Index 1 iv Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Flight Instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE Press the BARO Knob CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION Window 4 Turn 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 highligh
130. stacle Clearance Up Pull Up Warning ROC Imminent Obstacle PULL UP Obstacle Obstacle Pull Impact Warning Up Pull Up 101 Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance Terrain Caution RTC Imminent Terrain TERRAIN CAUTION TERRAIN Caution Terrain Caution Impact Caution ITI Terrain Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Obstacle Clearance Caution Obstacle Caution ROC Imminent Obstacle TERRAIN OBSTACLE Caution Obstacle Impact Caution 101 Caution Obstacle Premature Descent TERRAIN T00LOW TERRMN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN ME tsk Rate Caution NCR 74 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations amp Alerts TAWS B System Status Annunciations HD TAWS B Page Aural Alert Type Alert d in Annunciation Message Annunciation System Test in Progress TAWS TEST M M oo TANS System System Test Pass None None Test OK TAWS Alerting is disabled TAWS INH None None MFD Terrain or Obstacle database unavailable or invalid None TAWS operating
131. sure to 29 92 in Hg 1013 hPa Selects OBS mode on the CDI when navigating by GPS only available with active leg Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN X4X Appendix CDI Cycles through GPS VORI LOC1 2 and VOR2 LOC2 navigation sources 8 on the CDI Displays the DME Tuning Window x allowing selection of the NAV source 7 for tuning each DME oipny uadx 0105 AEN INSET SENSOR PFD OBS CDI DME IDENT 1 nena n 52 Select the BACK Softkey to return to the top level softkeys AEN Sd5 IEEE EAE 7 Tom se JE ERIS 5 5 73 75 75 7 7 7 73 79 74 74 74 Select the BACK Softkey to return to the previous level softkeys buluueld Juil s snp old Transponder Softkeys XPDR Displays transponder mode selection softkeys H 1 Selects the 1 transponder as active 685 XPDR2 Selects the 2 transponder as active ze STBY Selects Standby Mode transponder does not E H reply to any interrogations ON Selects Mode A transponder replies to identi fication interrogations i 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 Sue unuuy gt 5
132. system should be serviced REGISTER GFDS Data services are inoperative register w GFDS The GDL 59 is not registered with Garmin Flight Data Services or it s current registration data has failed authentication MANIFEST GDL software mismatch communication halted The GDL 59 has incorrect software installed The system should be serviced 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 89 saunqee4 2 AEN 5640 2 oipny uadx sia siu umn sul paezey nubi nubi jeuonippy uoneiedo Jeuuouqy IBN x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 12 Annunciations 8 Alerts GSR 56 MESSAGE ADVISORIES A GARMIN Message GSR1 FAIL GSR1 has failed Comments A failure has been detected in the 1 GSR 56 The system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The system should be serviced MANIFEST GDL software mismatch commu
133. t identifiers are displayed when the airport is within approximately 9 nm DFLIS Resets PFD to default settings including changing units to standard gt s o 3 m x x pul 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 99 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix OBS 100 WIND DMEI BRGI BRG2 DME2 ALT UNIT STD BARO OPTN 1 OPTN 2 OPTN 3 OFF METERS IN HPA A GARMIN Displays softkeys to select wind data parameters VVind direction arrovvs vvith headvvind and crosswind components Wind direction arrow and speed Wind direction arrow with direction and speed Information not displayed Select to display the DMEI 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 Select to display the DME2 information window Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter and selected altitude in meters Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals Sets barometric pres
134. t CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 1 xipueddy suelv uoneiedo sainjea4 aoueplony 2 buluueld AEN Sd5 S241V olpny uqax sia Tunuuy Jeuuouqy Jeuonippy paezey n U10 AEN x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES 1 2 3 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency Press the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Press the OBS Softkey to select OBS Mode 2 Tum the CRS Knob to select the desired course to from the waypoint Press the CRS Knob to slew the CDI Course Pointer to a course bearing directly to the waypoint 3 Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key
135. t Mode Takeoff Go Around Climb Cruise Manual Thrust Mode Indications 8 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN 000 ES NOTE The system automatically selects a target thrust mode under certain flight conditions refer to the Airplane Flight Manual Supplement AFMS for a detailed discussion of automatic thrust mode transitions Selecting Takeoff Climb or Cruise Target N1 Thrust Mode 1 Select the TARGT N1 Softkey 2 Select one of the following Softkeys TO GA Selects the Takeoff Go Around target N1 thrust mode CLB Selects the Climb target N1 thrust mode CRU Selects the Cruise target N1 thrust mode 3 To return to the top level of Softkeys without changing the target thrust mode select the BACK Softkey Manually Entering Target N1 Speed 1 Select the TARGT N1 Softkey 2 Select the MAN Softkey 3 Select the following Softkeys to adjust the target N196 readout and bugs 1 Increases the target N1 speed by 1 40 1 Increases the target N1 speed by 0 1 1 Decreases the target N1 speed by 1 01 Decreases the target N1 speed by 0 1 4 Select the BACK Softkey to return to the top level of Softkeys Removing N1 Target Speed Display 1 Select the TARGT N1 Softkey 2 Select the OFF Softkey 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 9 sjuauimasu nubi xipu
136. t 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 20 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 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN 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 GPS Navigation This 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 I
137. tch those of backup configuration memory The system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The system should be serviced MANIFEST GTX2 software The transponder has incorrect software installed mismatch communication halted The system should be serviced 86 Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Annunciations 8 Alerts GTX 33 33D MESSAGE ADVISORIES CONT Message XPDR1 SRVC XPDR1 needs service Retum unit for repair Comments 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 XPDRT is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES 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 system should be serviced AHRS2 TAS AHRS2 not receiving valid airspeed AHRS1 GPS AHRS1 using backup GPS source The 2 AHRS is not receiving true airspeed from t
138. tion 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 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 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 GCU 475 has incorrect software installed The 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 system should be serviced if the problem persists 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 91 saunqee4 sanpa20J q Buruuejd AEN 5649 24V oipny uadx sia sjuawinasu paezey u102 AEN Wil jeuonippy uoneiedo Jeuuouqy i EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations a
139. 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 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 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN Flight Planning 6 Enter the departure time Press the ENT Key vvhen finished Departure time may be entered in local or UTC time depending upon system settings 7 flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system 8 The flashing cursor moves to the
140. tude Minimums 3 Barometric pressure 100 Bearing line 51 52 C CDI 1 2 12 94 Cell 41 42 Cell mode 42 Channel Presets 63 ChartView 56 57 Clearance player 14 Index Clearance Recorder 14 Code selection softkeys 11 COM 12 65 D Databases 106 Database synchronization 109 Database updates 106 107 108 DCLTR Softkey 57 Dead Reckoning 67 Declutter 105 Declutter 66 97 Designated altitudes 22 Direct to 19 DME 11 12 DR mode 67 68 E Edit a flight plan 34 Engine display 5 Engine Stage Rotation Speeds 7 F FD 76 Hight Director 15 Flight ID 11 Flight path marker 55 FliteCharts 56 57 Frequency Transfer 12 G Gain 52 H HF 12 Horizon heading 55 Horizontal scan 51 190 01130 00 Rev A Garmin G10009 Cockpit Reference Guide for the Cessna CitationJet Model 525 ndex 1 sainjea4 e uepioAy 2 Duruue d AEN Sd5 24JV olpny uqax sia sjuaumasu Jeuonippy 2 ni Tuo2 NeN ui uoneiedo Jeuuouqy Sue v unuuy LEON Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts kel Appendix index Inhibit 49 Inhibit TAVVS 49 nset Map 97 98 ntercom isolation 13 IOI 71 74 Iridium 59 60 61 leppesen 57 L Lightning 41 42 M Map panning 43 Message advisories 78 89 9 96 MET 76 METAR 43 Minimums 75 MISCOMP 69 70 Mistrim 76 Mode 101
141. uauimasu U105 AEN 4613 52 s mp oold Duiuue d AEN Sd5 fila uoneiado SoJnjeaJ aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 28 1 2 3 4 5 6 7 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cu
142. uildings or other metal structures can cause sensor differences that may result in nuisance miscompare annunciations during start up shut down or while taxiing Comparator Condition Window Text Difference in altitude sensors is 5 200 ft If both airspeed sensors detect 35 knots this is inhibited 15 kts f either airspeed sensor detects gt 35 knots and the difference in sensors is gt If either airspeed sensor detects gt 80 knots and the difference in sensors is gt 10 kts 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 69 s m 2 buluueld AEN Sd5 24JV olpny uqax 913 sjuauimasu 2 nubi uio AeN wb jeuonippyv uoneiedo Jeuuouqy mu EE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix m Annunciations 8 Alerts A GARMIN Comparator Window Text Condition Difference in heading sen sors is gt 10 degrees Difference in pitch sensors is gt 5 degrees Difference in roll sensors is gt 6 degrees ALT NO COMP o data from one or both altitude sensors IAS NO COMP o data from one or both airspeed sensors HDG NO COMP o data from one or both heading sensors PIT NO COMP ROL NO COMP o data fro
143. uoneiedo s m junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Overriding Flaps based FIT Alerting 1 Select the TAWS A Page 2 Press the FLAP OVR Softkey Inhibiting Enabling GPWS Alerting 1 Select the TAWS A Page 2 Press the GPWS INH Softkey to inhibit or enable GPWS alerts choice dependent on current state Inhibiting Enabling GSD Alerting NOTE Only available during a 650 alert On the PFD press the GS INH or GP INH Softkey only displayed during a GSD alert to inhibit or enable GSD alerts softkey choice dependent on present GSD alert type TAWS B o 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 A NOTE TAWS operation is only available when the system is configured for 48 a TAWS B installation Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Test TAWS System 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test
144. uration settings do not match backup configuration memory The system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced 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 system should be serviced 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 83 soJnjeoJ 2 AEN Sd S24V oipny uadx sia siu umn sul paezey nubi nubi jeuonippy uoneiedo Jeuuouqy 75 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message Comments GIA1 SERVICE G A1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2
145. vates 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 The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 15 sjuauimasu nubi 59 oipny uadx u102 AEN ARN Sd5 52 Suelv 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 EIS 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 ALTS Armed window Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn Fr Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key VS nnnn rpm to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed Hi nna IAS Hold in IAS or Mach
146. y 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 AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check fly garmin com for the current database 58 Garmin 610007 Cockpit Reference Guide for the Cessna CitationJet Model 525 190 01130 00 Rev A A GARMIN View Airport Directory Information While viewing the VVPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display SATELLITE TELEPHONE COMMUNICATION OPTIONAL Additional Features NOTE An account must be established to access the Iridium satellite network for voice and low speed data transmission Control and monitoring of telephone functions are accomplished through the AUX TELEPHONE Page Viewing the Telephone Page 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select AUXILIARY COMMUNICATIONS 3 If necessary select the TEL Softkey to display the AUX TELEPHONE Page Answering a Call In
147. ying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS or TCAS I System Optional Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the OPERATE or NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 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 190 01130 00 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna CitationJet Model 525 45 AEN 540 52 olpny yqax sia siu umnsul uo2 AEN iui Duruue d ni aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance Ss GARMIN 5 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 6 Rotate the Joystick clockwise to display a larger a

Garmin CitationJet Model 525 Cockpit Reference Guide

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