G1000 ® Integrated Flight Deck Cockpit Reference Guide for the Cessna Citation Mustang
Flight Instruments EICAS Nav/Com/Transponder/Audio Panel Automatic Flight Control System GPS Navigation Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annunciations & Alerts Appendix INDEx
Copyright © 2006-2008 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0435.11 or later for the Cessna Citation Mustang. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Warnings, Cautions & Notes WARNING: The G1000 TAWS feature does not relieve the pilot from the responsibility of being aware of surroundings during flight. The TAWS 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.
Warnings, Cautions & Notes Warning: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: The Garmin G1000, as installed in the Cessna Citation Mustang aircraft, has a very high degree of functional integrity.
Warnings, Cautions & Notes WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/aboutGarmin/ environment/disposal.jsp. WARNING: Because of anomalies in the earth’s magnetic field, operating the G1000 within the following areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south of 70° South latitude.
Warnings, Cautions & Notes NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65.
Warnings, Cautions & Notes Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
Record of Revisions Part Number 190-00600-00 Rev A Change Summary Initial release Rev B 190-00600-01 Rev A Added Additional Features section Rev B Added CAS INOP system messages Rev C Added COM 3 function for HF Added TAS Removed automatic Reversionary Mode operation Added Synthetic Vision Added other GDU 9.01 parameters 190-00600-02 Production release Revision Date of Revision Affected Pages A April, 2008 All 190-00600-02 Rev.
Record of Revisions Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
Table of Contents Flight Instruments. ............................................................................................................... 1 Selecting the Altimeter Barometric Pressure Setting....................................................... 1 Selecting Standard Barometric Pressure.............................................................................. 1 Change Altimeter Barometric Pressure Setting Units.......................................................
Table of Contents Flight Planning....................................................................................................................... 19 Weight Planning....................................................................................................................... 19 Trip Planning............................................................................................................................. 19 Create a New User Waypoint..................................................
Table of Contents Abnormal Operation.......................................................................................................... 49 Reversionary Mode................................................................................................................. 49 Abnormal COM Operation..................................................................................................... 49 Hazard Displays with Loss of GPS Position................................................................
Table of Contents Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
Flight Instruments Flight Instruments Flight Instruments Selecting the Altimeter Barometric Pressure Setting EICAS Turn the BARO Knob to select the desired setting. Nav/Com/ XPDR/Audio Selecting Standard Barometric Pressure Press the BARO Knob. AFCS Change Altimeter Barometric Pressure Setting Units 2) Select the ALT UNIT Softkey. 3) Select the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).
Change Navigation Sources Select the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 2) Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency. 3) Select the CDI Softkey a third time to return to GPS. Flight Planning 1) Select the OBS Softkey to select OBS Mode.
Flight Instruments 5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 6) To remove the window, press the CLR Key or the TMR/REF Softkey. EICAS Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field Flight Instruments 4) Turn Vspeed Bugs On or Off by Category 2) Press the MENU Key. 3) Turn the FMS Knob to highlight the desired option. 4) Press the ENT Key. Press the TMR/REF Softkey to remove the window. AFCS Press the TMR/REF Softkey.
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Flight Instruments Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
EICAS 2 6 1 Nav/Com/ XPDR/Audio 5 EICAS 1 Flight Instruments Engine Indication & Crew Alerting System AFCS 5 7 GPS Nav 3 Flight Planning 8 Procedures 6 2 Hazard Avoidance 3 4 7 Abnormal Operation 10 Additional Features 9 8 EICAS Display (Normal Mode) 3 Fuel Display 4 CAS Display 190-00600-02 Rev.
Crew Alerting System (CAS) NOTE: Refer to the Annunciations and Alerts section for specific CAS messages. NOTE: Refer to the Airplane Flight Manual (AFM) for emergency procedures. NOTE: If there is a mismatch between databases or software on the PFDs, CAS is inoperative. When CAS messages are present while in reversionary mode, the CAS Window appears on the display along with the flight instruments and EIS.
Nav/Com/XPDR/Audio Panel Flight Instruments Nav/Com/Transponder/Audio Panel Enter or Change Flight ID 2) Turn the small FMS Knob to enter the first character. 3) Turn the large FMS Knob to select the next field. 4) Turn the small FMS Knob to enter the next desired character. 5) Repeat steps 3 and 4 until the desired Flight ID is entered. 6) Press the ENT Key. In the FLT ID field, ‘updating’ is momentarily displayed. Do not perform any other G1000 functions until ‘updating’ is no longer displayed.
Enter 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 the entry is cancelled and restored to the previous code.
Nav/Com/XPDR/Audio Panel Press the PILOT and/or COPLT Key on either audio panel to select those isolated from hearing the Nav/Com radios and music.
Digital Clearance Recorder and Player EICAS Flight Instruments Nav/Com/XPDR/Audio Panel NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is not recorded for COM3 MIC. Nav/Com/ XPDR/Audio Record 1) Press the REC Key to begin recording. 2) Press the REC Key again to stop recording. Flight Planning GPS Nav AFCS Play 1) Press the PLAY Key once to play the latest recorded memory block. 2) Press the PLAY Key once while playing to stop.
AFCS Note: If the attitude information required for the default flight director modes becomes invalid or unavailable, the autopilot automatically disengages.
Vertical Modes Vertical Mode Pitch Hold Selected Altitude Armed Altitude Hold Vertical Speed VNAV VNAV Target Altitude Armed Abnormal Operation Glidepath Glideslope Go Around Control Annunciation Holds the current aircraft pitch attitude; may be used to climb/descend to the (default) Selected Altitude AFCS armed to capture the altitude displayed in the Selected Altitude * window Holds the current Altitude Reference ALT Key Maintains the current aircraft vertical speed; may be used to climb/descend VS K
AFCS Lateral Mode Roll Hold Heading Select Captures and tracks Selected Heading HDG GPS Captures and tracks selected navigation source (GPS, VOR, LOC) NAV Key VOR Flight Planning LOC BC Key BC Hazard Avoidance Captures and tracks a localizer signal for backcourse approaches Procedures GPS Captures and tracks selected navigation APR Key source (GPS, VOR, LOC) Additional Features VAPP Abnormal Operation LOC Disengages autopilot and commands a constant pitch angle and wings level GA Switch A
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments AFCS Blank Page 14 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
GPS Navigation Flight Instruments GPS Navigation Direct-to Navigation EICAS Direct-to Navigation using the MFD 2) 3) 6) 9) 12) 1) 2) 5) 190-00600-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 15 Index 6) Appendix 4) ) on the PFD or controller. Turn the large FMS Knob to place the cursor in the desired selection field. Turn the small FMS Knob to begin selecting the desired identifier, location, etc. Press the ENT Key. The cursor is now flashing on ‘ACTIVATE?’.
EICAS Flight Instruments GPS Navigation 7) Turn the small FMS Knob to enter the desired altitude. 8) 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. 9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. Nav/Com/ XPDR/Audio 10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.
GPS Navigation Flight Instruments Stop Navigating a Flight Plan 2) Press the MENU Key to display the Page Menu Window. 3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan. Vertical Navigation (VNAV) AFCS GPS Nav The navigation database only contains altitudes for procedures that call for “Cross at” altitudes.
AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments GPS Navigation 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.
Flight Planning Flight Instruments Flight Planning Weight Planning EICAS All procedures apply to the MFD unless otherwise stated. Entering Weight Parameters Procedures 3) Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors. Additional Features Turn the large FMS Knob to place the cursor in the ‘Fuel On Board’ field. Or: Annun/ Alerts Press the FMS Knob to remove the cursor. Abnormal Operation Manually enter the desired fuel quantity.
Flight Planning Flight Instruments 4) For Direct-to planning: a) Select the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). EICAS b) If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’. Nav/Com/ XPDR/Audio c) Press the ENT Key and the flashing cursor moves to the ending waypoint field. AFCS d) Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint.
Flight Planning Enter the fuel flow. Press the ENT Key when finished. Note that in ‘automatic’ page mode, fuel flow is provided by the system. 8) The flashing cursor moves to the fuel onboard field. Modify the fuel onboard. Press the ENT Key when finished. In ‘AUTOMATIC’ mode, fuel onboard is provided by the entry made on the Weight Planning Page. 9) The flashing cursor moves to the calibrated airspeed field. Enter a calibrated airspeed. Press the ENT Key when finished.
Flight Planning Flight Instruments a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. EICAS 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. After pressing the ENT Key, the cursor is displayed in the ‘RAD’ (radial) field. Enter the desired radial from the reference waypoint. 8) Press the ENT Key. 9) The cursor is now displayed in the ‘DIS’ (distance) field.
Flight Planning Press the FPL Key. 2) Turn the small FMS Knob to display the Flight Plan Catalog Page. 3) Select the NEW Softkey to display a blank flight plan for the first empty storage location. 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the identifier of the departure waypoint. Nav/Com/ XPDR/Audio 6) Press the ENT Key. 7) Repeat step number 4, 5, and 6 to enter the identifier for each additional flight plan waypoint.
1) Press the FPL Key to display the active flight plan. 2) If necessary, press the FMS Knob to activate the cursor. EICAS Insert a Waypoint in the Active Flight Plan 3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The new waypoint is inserted before the highlighted waypoint. Nav/Com/ XPDR/Audio Flight Instruments Flight Planning 4) Turn the small FMS Knob. The Waypoint Information Window is now displayed.
Flight Planning Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted. GPS Nav 6) Invert An Active Flight Plan Press the MENU Key to display the Page Menu. 3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’. 4) Press the ENT Key. The original flight plan remains intact in its flight plan catalog storage location.
3) Press the CLR Key to display a confirmation window. 4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure or airway. Store a Flight Plan AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Flight Planning 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan.
Flight Planning 4) With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. Flight Instruments 5) Once all changes have been made, press the FMS Knob to remove the cursor. EICAS Nav/Com/ XPDR/Audio Invert and Activate a Stored Flight Plan Press the FPL Key for the MFD. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor.
5) Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is displayed. 6) With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. Graphical Flight Plan Creation 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the Joystick to activate the map pointer.
Procedures Flight Instruments Procedures Load and Activate a Departure Procedure EICAS 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.
Nav/Com/ XPDR/Audio EICAS Flight Instruments Procedures 5) Press the ENT Key. A list of transitions is displayed for the selected arrival. 6) Turn either FMS Knob to select the desired transition. 7) Press the ENT Key. A list of runways may be displayed for the selected arrival. 8) Turn the large FMS Knob to highlight the desired runway. 9) Press the ENT Key. 10) With ‘LOAD?’ highlighted, press the ENT Key. AFCS 11) The arrival becomes part of the active flight plan.
Procedures 8) If desired, the DA/MDA for the selected approach procedure may be entered and displayed on the PFD. Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO. 9) Press the ENT Key. The cursor moves to the altitude field. Turn the small FMS Knob to enter the published DA/MDA for the selected approach procedure. Nav/Com/ XPDR/Audio Press the ENT Key. The cursor moves to the MINIMUMS field.
Activate A Missed Approach in the Active Flight Plan Nav/Com/ XPDR/Audio EICAS Flight Instruments Procedures 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. A confirmation window is displayed. 4) With ‘ACTIVATE’ highlighted, press the ENT Key. Or: Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Press the go-around button.
Hazard Avoidance Flight Instruments Hazard Avoidance Customizing the Hazard Displays on the Navigation Map EICAS 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. GPS Nav XM Weather (Optional) Select the NEXRAD or XM LTNG Softkey to display the desired weather.
Hazard Avoidance Flight Instruments 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. Nav/Com/ XPDR/Audio EICAS Map Panning Information – Weather Data Link Page 1) Push in the Joystick to display the panning arrow. 2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs, or SIGMETs.
Hazard Avoidance Description Flight Instruments Traffic Symbol Non-Threat Traffic (intruder is beyond 5 nm and greater than 1200’ vertical separation) EICAS Proximity Advisory (PA) (TAS only) (intruder is within 5 nm and less than 1200’ vertical separation) Nav/Com/ XPDR/Audio Traffic Advisory (TA) (closing rate, distance, and vertical separation meet TA criteria) Traffic Advisory Off Scale AFCS Traffic Symbol Description GPS Nav Traffic Information Service (TIS) NOTE: Traffic Information Serv
Hazard Avoidance Flight Instruments Traffic Advisory System (TAS) (Optional) 1) 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.
Hazard Avoidance NOTE: TAWS operation is only available when the G1000 is configured for a TAWS-B installation. AFCS NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. Nav/Com/ XPDR/Audio EICAS WARNING: The TAWS display shows supplemental information only. It should not be used for navigation.
Hazard Avoidance EICAS Flight Instruments Enable/Disable Aviation Data 1) While the TAWS 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.
Hazard Avoidance Nav/Com/ XPDR/Audio AFCS CAUTION: In Standby Mode, the antenna is parked at the center line. It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly. EICAS 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.
AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Hazard Avoidance Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left. Monitor the displayed bearing value in the BEARING field. 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’.
Hazard Avoidance Select the MODE Softkey. 2) Select the GROUND Softkey to place the radar in Ground Map Mode. 3) Select the BACK Softkey. EICAS 1) Flight Instruments Ground Mapping 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.
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Hazard Avoidance Blank Page 42 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
Additional Features Flight Instruments Additional Features Synthetic Vision Flight Planning Procedures Hazard Avoidance Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. 4) Press the BACK Softkey to return to the previous page. Abnormal Operation 2) Additional Features Press the PFD Softkey. Displaying Pathways 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.
Additional Features Nav/Com/ XPDR/Audio EICAS Flight Instruments Displaying Heading on the Horizon 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. AFCS GPS Nav 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.
Additional Features ChartView Hazard Avoidance Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey. Annun/ Alerts Select the GO BACK Softkey to return to the previous page. Abnormal Operation 3) View Charts from the Active Flight Plan Page 2) Turn the large FMS Knob to select the departure airport, destination airport, departure, arrival, or approach. 3) Select the SHW CHRT Softkey. The appropriate chart is displayed, if available for the item selected.
Additional Features Flight Instruments 4) Change Day/Night View While viewing a chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR SCHEME’ Options. 4) Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen Options. 5) Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’ Options.
Additional Features EICAS Nav/Com/ XPDR/Audio AFCS The Category Box of the XM Radio Page displays the currently selected category of audio. 1) Select the CATGRY Softkey on the XM Radio Page. 2) Select the CAT + and CAT - softkeys to cycle through the categories. Or: Turn the small FMS Knob to display the ‘Categories’ list. Highlight the desired category with the small FMS Knob. 3) Press the ENT Key.
EICAS Flight Instruments Additional Features 3) Select any one of the (PS1 - PS15) softkeys to assign a number to the active channel. 4) Select the SET Softkey on the desired channel number to save the channel as a preset. Nav/Com/ XPDR/Audio Adjusting Volume Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Radio volume is controlled at each passenger station.
Abnormal Operation Flight Instruments Abnormal Operation Reversionary Mode Hazard Avoidance Additional Features 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.
Unusual Attitudes The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary functions are displayed in these situations.
Abnormal Operation GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/ Alerts Appendix 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.
EICAS Flight Instruments Abnormal Operation 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.
Annunciations & Alerts Flight Instruments Annunciations & Alerts CAS Messages Advisory Tailcone baggage door not fully secured Start control circuit breaker (located in aft j-box) tripped Current limiter blown (located in aft j-box) Antiskid Control Unit cannot perform anti-skid functions Overheated NiCad battery (optional) AFT DOOR AFT JBOX LMT L-R* BATTERY O’TEMP BATTERY O’TEMP BATT TEMP FAIL CABIN ALT X X Battery temperature sensor failure X X Cabin altitude potentially unsafe X X CABIN DOOR
Annunciations & Alerts Advisory Description ESI TOPI AIR LOPI ESDI EMER GND Flight Instruments EICAS Caution MFD COLD MFD temperature is below -20° C One or both nose baggage doors not NOSE DOOR L-R* fully secured Antiskid control spindown function NO TIRE SPINDOWN not working OIL PRESS LO L-R* Oil pressure less than redline low limit X OXYGEN OFF P/S HTR L-R* AFCS Nav/Com/ XPDR/Audio Warning GPS Nav PRESS CTRL Flight Planning STALL WARN FAIL Procedures STALL WARN HTR T2 HTR FAIL L-R* TAIL
Annunciations & Alerts Comparator Window Text Condition Difference in altitude sensors is > 200 ft. EICAS ALT MISCOMP Flight Instruments Comparator Annunciations If both airspeed sensors detect < 35 knots, this is inhibited. If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts. Nav/Com/ XPDR/Audio IAS MISCOMP If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts.
Reversionary Sensor Window Text USING AHRS2 USING GPS1 USING GPS2 Condition PFD1 is displaying data from the #2 AHRS. PFD2 is displaying data from the #1 GPS. PFD1 is displaying data from the #2 GPS. AFCS Alerts Condition Annunciation Description Pitch Failure Pitch axis control failure. AP is inoperative. Roll Failure Roll axis control failure. AP is inoperative.
Annunciations & Alerts Alert Type MFD Pop-Up Alert Aural Message Reduced Required Terrain Clearance Warning (RTC) or * * or * “Caution, Terrain; Caution, Terrain”* or Appendix * “Terrain Ahead; Terrain Ahead” or “Caution, Terrain; Caution, Terrain”* Annun/ Alerts or “Terrain Ahead; Terrain Ahead” Abnormal Operation Imminent Terrain Impact Caution (ITI) or “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” or “Obstacle, Obstacle; Pull Up, Pull Up”* Additional Features Reduced Required Te
Alert Type MFD Pop-Up Alert or Imminent Obstacle Impact Caution (IOI) Aural Message * or * “Caution, Obstacle; Caution, Obstacle”* or “Obstacle Ahead; Obstacle Ahead” “Obstacle Ahead; Obstacle Ahead” or “Caution, Obstacle; Caution, Obstacle”* Premature Descent Alert Caution (PDA) Altitude Callout “500” “Too Low, Terrain” None None “Five-Hundred” Excessive Descent Rate Caution (EDR) “Sink Rate” Negative Climb Rate Caution (NCR) or “Don’t Sink”* or “Too Low, Terrain” * * Default configuratio
Annunciations & Alerts PFD1 FAN FAIL – The cooling fan for PFD1 is inoperative. PFD2 FAN FAIL – The cooling fan for PFD2 is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative. AV FAN FAIL – The cooling fan for remote avionics has failed.
MFD & PFD Message Advisories (Cont.) Message MANIFEST – PFD1 software mismatch, communication halted. MANIFEST – PFD2 software mismatch, communication halted. MANIFEST – MFD1 software mismatch, communication halted. PFD1 CONFIG – PFD1 config error. Config service req’d. PFD2 CONFIG – PFD2 config error. Config service req’d. MFD1 CONFIG – MFD1 config error. Config service req’d. CAS INOP – No Dispatch. Software correction required. PFD1 COOLING – PFD1 has poor cooling. Reducing power usage.
Annunciations & Alerts Comments The PFD1 configuration module backup memory has failed. The G1000 system should be serviced. The PFD1 voltage is low. The G1000 system should be serviced. The PFD2 voltage is low. The G1000 system should be serviced. The MFD voltage is low. The G1000 system should be serviced. EICAS Nav/Com/ XPDR/Audio AFCS GPS Nav Message CNFG MODULE – PFD1 configuration module is inoperative. PFD1 VOLTAGE – PFD1 has low voltage. Reducing power usage PFD2 VOLTAGE – PFD2 has low voltage.
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Annunciations & Alerts Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 terrain database missing. PFD1 DB ERR – PFD1 terrain database missing. PFD2 DB ERR – PFD2 terrain database missing. MFD1 DB ERR – MFD1 obstacle database error exists. PFD1 DB ERR – PFD1 obstacle database error exists.
Annunciations & Alerts Comments AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/ Alerts Appendix The MFD and/or PFDs detected a failure in the ChartView database (optional feature). Ensure that the data card is properly inserted. Replace data card. If problem persists, The G1000 system should be serviced. MFD1 DB ERR – MFD1 FliteCharts The MFD and/or PFDs detected a failure in the database error exists. FliteCharts database (optional feature).
Database Message Advisories (Cont.) Message DB MISMATCH – Obstacle database version mismatch. DB MISMATCH – Airport Terrain database mismatch. CAS INOP – No Dispatch. Database correction required. Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Annunciations & Alerts Comments The PFDs and MFD have different obstacle database versions installed.
Annunciations & Alerts The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The G1000 system should be serviced. AFCS The GIA1 and/or GIA2 have an error in the audio configuration. The G1000 system should be serviced. Nav/Com/ XPDR/Audio GPS Nav The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature. Flight Planning The GIA1 and/or GIA2 temperature is too high.
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Annunciations & Alerts GIA 63W Message Advisories (Cont.) Message COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. Comments The system has detected an over temperature condition in COM1 and/or COM2. The transmitter is operating at reduced power.
Annunciations & Alerts Flight Planning Abnormal Operation A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The G1000 system should be serviced when possible. Additional Features G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. Hazard Avoidance G/S2 FAIL – G/S2 is inoperative.
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Annunciations & Alerts GEA 71 Message Advisories Message Comments GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match Config service req’d. those of backup configuration memory. The G1000 system should be serviced. GEA2 CONFIG – GEA2 config error.
Annunciations & Alerts Index 69 Appendix Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Annun/ Alerts 190-00600-02 Rev. A Abnormal Operation AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode. AHRS2 GPS – AHRS2 operating exclusively in no-GPS mode. AHRS MAG DB – AHRS magnetic model database version mismatch. Additional Features AHRS2 GPS – AHRS2 not receiving backup GPS information. Hazard Avoidance AHRS1 GPS – AHRS1 not receiving backup GPS information.
Message AHRS1 SRVC – AHRS1 Magneticfield model needs update. AHRS2 SRVC – AHRS2 Magneticfield model needs update. GEO LIMITS – AHRS1 too far North/South, no magnetic compass. GEO LIMITS – AHRS2 too far North/South, no magnetic compass. MANIFEST – GRS1 software mismatch, communication halted. MANIFEST – GRS2 software mismatch, communication halted. Comments The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical.
Annunciations & Alerts AFCS MANIFEST – GDL software mismatch, communication halted. Nav/Com/ XPDR/Audio GDL69 FAIL – GDL 69 has failed. Comments GDL 69 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced The GDL 69 has incorrect software installed. The G1000 system should be serviced. EICAS Message GDL69 CONFIG – GDL 69 config error.
GDC 74B Message Advisories Message ADC1 ALT EC – ADC1 altitude error correction is unavailable. ADC2 ALT EC – ADC2 altitude error correction is unavailable. ADC1 AS EC – ADC1 airspeed error correction is unavailable. ADC2 AS EC – ADC2 airspeed error correction is unavailable. MANIFEST – GDC1 software mismatch, communication halted. MANIFEST – GDC2 software mismatch, communication halted. Comments GDC1 or GDC2 is reporting that the altitude error correction is unavailable.
Annunciations & Alerts Error in the configuration of the GMC 710. A failure has been detected in the GMC 710. The GMC 710 is unavailable. The GMC 710 has incorrect software installed. The G1000 system should be serviced. A key is stuck on the GMC 710 bezel. Attempt to free the stuck key by pressing it several times. The G1000 system should be serviced if the problem persists. Nav/Com/ XPDR/Audio AFCS MANIFEST – GMC software mismatch. Communication halted. GMC KEYSTK – GMC [key name] Key is stuck.
Miscellaneous Message Advisories (Cont.) Message DB CHANGE – Database changed. Verify user modified procedures. DB CHANGE – Database changed. Verify stored airways. FPL TRUNC – Flight plan has been truncated. Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Annunciations & Alerts LOCKED FPL – Cannot navigate locked flight plan.
Annunciations & Alerts Invalid leg type for parallel offset. Annun/ Alerts Appendix Index 75 Abnormal Operation Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Additional Features IAF waypoint for parallel offset has been passed. The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint.
Miscellaneous Message Advisories (Cont.) Message VNV – Unavailable. Parallel course selected. NO WGS84 WPT – Non WGS 84 waypoint for navigation -[xxxx] TRAFFIC FAIL – Traffic device has failed. FAILED PATH – A data path has failed. MAG VAR WARN – Large magnetic variance. Verify all course angles. SVS – SVS DISABLED: Out of available terrain region. SVS – SVS DISABLED: Terrain DB resolution too low. SCHEDULER [#] – .
Appendix Flight Instruments Appendix PFD Softkey Map EICAS Nav/Com/ XPDR/Audio AFCS GPS Nav Top Level PFD Softkeys Flight Planning Procedures TRFC-1 Hazard Avoidance Select the BACK or OFF Softkey to return to the top-level softkeys.
Appendix Cycles through traffic display options: TRFC-1: Traffic displayed on inset map TRFC-2: Traffic Map Page is displayed in the inset map window Displays topographical data (e.g.
Appendix Flight Instruments SYN VIS ALT UNIT EICAS IN AFCS METERS Nav/Com/ XPDR/Audio Select the STD BARO or BACK Softkey to return to the top-level softkeys HPA GPS Nav PATHWAY SYN TERR HRZN HDG APTSIGNS Flight Planning PFD Configuration Softkeys 79 Index Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Appendix 190-00600-02 Rev.
Appendix Flight Instruments WIND EICAS OPTN 1 OPTN 2 Nav/Com/ XPDR/Audio OPTN 3 Flight Planning GPS Nav AFCS OFF Select to display the DME information window BRG1 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.
Appendix Flight Instruments MSG EICAS Select the BACK Softkey to return to the top-level softkeys. Nav/Com/ XPDR/Audio MSG AFCS Select the BACK Softkey to return to the top-level softkeys. Transponder Softkeys GPS Nav ALT GND VFR Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Index 190-00600-02 Rev.
AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Appendix TMR/REF Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen Displays Timer/References Window NRST Displays Nearest Airports Window MSG Displays Message Window IDENT MFD Softkey Map CAS ↓ DCLTR MAP GPS Nav CAS ↑ (optional) SHW CHRT CHKLIST DCLTR-1 Flight Planning DCLTR-2 Procedures DCLTR-3 TRAFFIC TOPO TERRAIN AIRWAYS Select the BACK Softkey on thi
Appendix Displays topographical data (e.g.
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Appendix Blank Page 84 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
Index DCLTR Softkey 44 Dead Reckoning 51 Declutter 50, 77, 83 Designated altitudes 18 Direct-to 15 DME 7, 8 DR mode 51, 52 Hazard Avoidance G Gain 40 Additional Features H HF 8 Horizontal scan 40 Horizon heading 43 Abnormal Operation I Annun/ Alerts Inhibit 38 Inhibit TAWS 38 Inset Map 77, 78 Intercom isolation 9 IOI 57, 58 Index Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang Appendix 190-00600-02 Rev.
Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Index J R Jeppesen 45 Reversionary Mode EICAS 5 Reversionary mode 49 ROC 57, 58 M Map panning 34 Message advisories 59 – 64, 67, 69, 70, 72 – 76 MET 56 METAR 33 Minimums 59 MISCOMP 55 Mistrim 56 Mode S 81 Mode selection softkeys 8 Multi Function Display (MFD) Softkeys 82 SafeTaxi® 44 Sector scan 41 Sensor 55 STAB 41 Standby 39 Store Flight Plan 26 SVS 43, 76 Synthetic Vision System 43 OBS 2 Obstacles 64, 65 Overspeed Prote
Index Flight Instruments W EICAS WAAS 65 WATCH® 41 Weather Attenuated Color Highlight 41 Weather data link page 33 Weather radar 39 Wind data 80 Nav/Com/ XPDR/Audio X AFCS XM lightning 78, 83 XM weather 33 GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun/ Alerts Appendix Index 190-00600-02 Rev.
Index Appendix Annun/ Alerts Abnormal Operation Additional Features Hazard Avoidance Procedures Flight Planning GPS Nav AFCS Nav/Com/ XPDR/Audio EICAS Flight Instruments Index Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev.
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