G1000 ® Integrated Flight Deck Cockpit Reference Guide for the Cessna Citation Mustang
FLIGHT INSTRUMENTS 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 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0435.07 or later for the Cessna Citation Mustang. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.
Warnings, Cautions & Notes WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system.
Warnings, Cautions & Notes 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. 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.
Warnings, Cautions & Notes WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airman’s Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.
Part Number 190-00600-00 Rev A Change Summary Initial release Revision Date of Revision Affected Pages Description A October, 2006 i through Index-2 Production release B November, 2006 41-44 Added Additional Features section 190-00600-00 Rev.
Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-00 Rev.
Table of Contents FLIGHT INSTRUMENTS ................................................................................................................ 1 Selecting the Altimeter Barometric Pressure Setting ...................................................... 1 Selecting Standard Barometric Pressure (29.92 in Hg) .................................................... 1 Changing Altimeter Barometric Pressure Setting Units ..................................................
Table of Contents Invert An Active Flight Plan.................................................................................................. 21 Remove a Departure, Arrival, Approach, or Airway from a Flight Plan ..................... 21 Store a Flight Plan .................................................................................................................. 22 Edit a Stored Flight Plan .......................................................................................................
Table of Contents ANNUNCIATIONS & ALERTS................................................................................................... 49 CAS Messages .......................................................................................................................... 49 Comparator Annunciations................................................................................................... 51 Reversionary Sensor Annunciations .....................................................................
Table of Contents Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-00 Rev.
Flight Instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting. SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG) 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the STD BARO Softkey. OR Push the BARO Knob to select standard pressure. CHANGING ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey.
Flight Instruments CHANGE NAVIGATION SOURCES 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency. 3) Press the CDI Softkey a third time to return to GPS.
Flight Instruments 4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field 5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 6) To remove the window, press the CLR Key or the TMR/REF Softkey. TURN VSPEED BUGS ON OR OFF BY CATEGORY 1) Press the MENU Key. 2) Turn the FMS Knob to highlight the desired option. 3) Press the ENT Key. Press the TMR/REF Softkey to remove the window. SET BAROMETRIC MINIMUM DESCENT ALTITUDE 1) Press the TMR/REF Softkey.
Flight Instruments Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-00 Rev.
Nav/Com/XPDR/Audio Panel NAV/COM/TRANSPONDER/AUDIO PANEL ENTER OR CHANGE FLIGHT ID 1) Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the Flight ID field. 2) Turn the small FMS Knob to enter the first character. 3) Turn the large FMS Knob to select the next field. 4) 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 to update the Flight ID.
Nav/Com/XPDR/Audio Panel 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 DIGITAL CLEARANCE RECORDER AND PLAYER NOTE: Only the audio for the selected COM MIC Key is recorded. Record 1) Press the REC Key to begin recording. 2) Press the REC Key again to stop recording. Play 1) Press the PLAY Key once to play the latest recorded memory block. 2) Press the PLAY Key once while playing to stop. 3) Press the PLAY Key twice quickly while playing to begin playing the previously recorded block.
Nav/Com/XPDR/Audio Panel Blank Page 8 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-00 Rev.
AFCS AUTOMATIC FLIGHT CONTROL SYSTEM NOTE: If sensor information (other than attitude) required for a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis. NOTE: If the attitude information required for the default flight director modes becomes invalid or unavailable, the flight director automatically disengages.
AFCS LATERAL MODES Lateral Mode Roll Hold Control (default) Low Bank BANK Key Heading Select Navigation, VOR Enroute Arm/Capture/Track Navigation, GPS Arm/Capture/Track Navigation, LOC Arm/Capture/Track (No Glideslope) Backcourse Arm/Capture/Track Approach, GPS Arm/Capture/Track Approach, VOR Arm/Capture/Track Approach, ILS Arm/Capture/Track (Glideslope Mode automatically armed) Go-Around (in air) Takeoff (on ground) HDG Key NAV Key Annunciation ROL Green arc displayed over the roll attitude scale HDG
GPS Navigation GPS NAVIGATION DIRECT-TO NAVIGATION Direct-to Navigation from the MFD 1) 2) 3) 4) 5) 6) 7) 8) 9) 10) 11) 12) Press the Direct-to ( ) Key. Enter the destination waypoint identifier. Press the ENT Key to confirm the identifier. The ‘Activate?’ field is highlighted. If no altitude constraint or course is desired, press the ENT Key to activate. To enter an altitude constraint, proceed to step 5. Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field. Enter the desired altitude.
GPS Navigation 8) Press the ENT Key. The option to select MSL or AGL is now displayed. 9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 10) Press the ENT Key. The cursor is placed in the ‘VNV’ offset distance field. 11) Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct-to. 12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘COURSE’ field. 13) Turn the small FMS Knob to enter the desired course to the waypoint.
GPS Navigation STOP NAVIGATING A FLIGHT PLAN 1) Press the FPL Key to display the Active Flight Plan Page. 2) Press the MENU Key to display the Page Menu Window. 3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan. VERTICAL NAVIGATION The navigation database only contains altitudes for procedures that call for “Cross at” altitudes.
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 speed and deviation guidance. Note that these altitudes will be displayed as blue text up to, but not including the FAF. The FAF will always be a “reference only” altitude and cannot be designated, unless the selected approach does not provide vertical guidance.
Flight Planning FLIGHT PLANNING WEIGHT PLANNING All procedures apply to the MFD unless otherwise stated. Entering Weight Parameters The Weight Planning Page is displayed after system power-up. If it is necessary to return to this page, turn the large FMS Knob to select the ‘AUX’ page group. Turn the small FMS Knob to select the first rectangular page icon. 1) Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field. 2) Enter the desired aircraft empty weight. 3) Press the ENT Key.
Flight Planning 4) For Direct-to planning: a) Select the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). b) If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’. c) Press the ENT Key and the flashing cursor moves to the ending waypoint field. d) Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint. OR 5) For point-to-point planning: a) Enter the identifier of the starting waypoint.
Flight Planning 8) Enter the departure time. Press the ENT Key when finished. Departure time may be entered in local or UTC time, depending upon system settings. 9) Enter the fuel flow. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow is provided by the system. 10) 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.
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. 7) 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 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the identifier of the departure waypoint. 6) Press the ENT Key. 7) Repeat step number 3, 4, and 5 to enter the identifier for each additional flight plan waypoint. 8) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new flight plan is now in the list.
Flight Planning 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 a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed. b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints to the aircraft’s current position. c) Turn the large FMS Knob to select the desired waypoint.
Flight Planning 8) Turn either FMS Knob to scroll through the list of available exit points. 9) With the desired exit point highlighted, press the ENT Key. 10) With ‘LOAD?’ highlighted, press the ENT Key. INVERT AN ACTIVE FLIGHT PLAN 1) Press the FPL Key to display the active flight plan. 2) Press the MENU Key to display the Page Menu. 3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’. 4) Press the ENT Key.
Flight Planning STORE A FLIGHT PLAN 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan. EDIT A STORED FLIGHT PLAN 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor.
Flight Planning 5) Once all changes have been made, press the FMS Knob to remove the cursor. INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) Press the FPL Key. 2) Turn the small FMS Knob to select the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor. 4) Turn the large FMS Knob to highlight the desired flight plan. 5) Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ will be displayed. 6) With ‘OK’ highlighted, press the ENT Key.
Flight Planning GRAPHICAL FLIGHT PLAN CREATION 24 1) Press the FPL Key to display the Active Flight Plan Page. 2) Press the Joystick to activate the map pointer. Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan. 3) The default insertion point is at the end of the flight plan. If the selected waypoint is to be placed anywhere other than the end of the flight plan, press the FMS Knob to activate the cursor.
Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a list of available departures. 4) Turn the large FMS Knob to highlight the desired departure. 5) Press the ENT Key. A list of runways may be displayed for the departure. If so, turn either FMS Knob to select the desired runway. 6) Press the ENT Key.
Procedures 4) Turn the large FMS Knob to highlight the desired arrival. 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 is 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. 11) The arrival will become part of the active flight plan.
Procedures 7) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’ highlighted. 8) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’. Selecting ‘LOAD?’ will enter the selected approach procedure into the active flight plan, but will not be currently active. Selecting ‘ACTIVATE?’ will enter the selected approach procedure into the active flight plan and immediately activate it. 9) Press the ENT Key. ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1) Press the PROC Key.
Procedures Blank Page 28 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-00 Rev.
Hazard Avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select ‘Weather’ to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic. 3) Press the small FMS Knob to return to the Navigation Map Page.
Hazard Avoidance 4) Select the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list. Press the small FMS Knob or the ENT Key to return to the map. Map Panning Information – Weather Data Link Page 1) Push in the Joystick to display the panning arrow. 2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs, or SIGMETs. 3) Press the ENT Key to display pertinent information for the selected product.
Hazard Avoidance Weather Product Age Weather Product SIGMETs/AIRMETs City Forecasts County Warnings Cyclone Warnings Echo Tops Freezing Levels METARs Lightning NEXRAD Cell Movement Surface Analysis TFRs Winds Aloft TAFs Clouds Tops Expires After Refresh Rate (minutes) (minutes) 60 12 60 12 60 5 60 12 30 7.5 60 12 90 12 30 5 30 5 30 1.
Hazard Avoidance 4) Select the STANDBY Softkey to place the system in the Standby Mode. ‘TIS STANDBY’ will be displayed in the Traffic Mode field. 5) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area. Displaying Traffic on the Navigation Map 1) Ensure TIS is operating. With the Navigation Map displayed, press the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic will now be displayed on the map.
Hazard Avoidance Display Terrain on the TAWS Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS Page. 3) If desired, select the VIEW Softkey to access the ARC and 360 softkeys. When the ARC Softkey is selected, a radar-like 120° view is displayed. Select the 360 Softkey to return to the 360° default display. 4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Hazard Avoidance Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) Phase of Flight Level Flight Descending Enroute 700 ft 500 ft Terminal 350 ft 300 ft Approach 150 ft 100 ft Departure 100 ft 100 ft Terrain & Obstacle Clearance Thresholds for Alerting Premature Descent Alert (PDA) ��������������������������� ��� ��� ��� ��� ��� ����������������� ��� ��� � ��� ������ ��������� ��� ��� ��� ��� ��� ��� ��� ��� ��� ��� ��� ��� ��� �� �����������������������
Hazard Avoidance Excessive Descent Rate Alert (EDR) ���� ���� Height Above Terrain (Feet) ���� ���� E" AT ���� "S ���� I R NK ���� ���� ���� ���� "PULL UP" ���� ��� � ����� ����������������������������������������������������� ������ ��������� ������������� Excessive Descent Rate Alerting Negative Climb Rate After Takeoff Alert (NCR) ��������������������������� The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the pilot when the system determines
Hazard Avoidance “Five-Hundred” Aural Alert The purpose of the aural alert message “Five-hundred” is to provide an advisory alert to the aircrew that the aircraft is five-hundred feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “Five-hundred” is heard. 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 Displaying Weather on the Weather Radar Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Radar Page. 3) Select the MODE Softkey. 4) If the aircraft is on the ground, select the STANDBY Softkey to initiate the one minute warm-up period. After the warm-up is complete, the radar will enter the Standby Mode. After the aircraft is airborne, select the WEATHER Softkey.
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’. 3) Press the ENT Key.
Hazard Avoidance 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. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to place the cursor in the ‘TILT’ field. 6) Adjust the antenna tilt angle by turning the small FMS Knob to position the ground returns as desired. 7) Press the FMS Knob to remove the cursor.
Hazard Avoidance Weather Attenuated Color Highlight (WATCH™) To activate or deactivate the Watch™ feature, select the WATCH Softkey. This feature is only available in the Horizontal Scan Mode. Weather Alert To activate or deactivate Weather Alert, select the WX ALRT Softkey. Activating and deactivating will also enable or inhibit the alert on the PFD. Automatic Standby When the weather radar system is in the Weather or Ground Map Mode, upon landing the system will automatically switch to Standby Mode.
Additional Features ADDITIONAL FEATURES NOTE: The availability of SafeTaxi™, ChartView, or FliteCharts™ in electronic form does not preclude the requirement to carry paper charts aboard the aircraft. See AC 120-76A for more information. SAFETAXI™ SafeTaxi™ is an enhanced feature that gives greater map detail when zooming in on airports at close range.
Additional Features OR Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey. 2) Press the DP, STAR, APR, WX, and NOTAM softkeys to access charts for departures, arrivals, approaches, weather and NOTAMs. 3) Press the GO BACK Softkey to return to the previous page. VIEW CHARTS FROM THE ACTIVE FLIGHT PLAN PAGE 1) While viewing the Active Flight Plan Page, press the FMS Knob to activate the cursor.
Additional Features XM® RADIO ENTERTAINMENT The XM® Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio. Selecting the XM Radio Page 1) 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) Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled.
Additional Features Entering a Channel Directly 1) While on the XM Radio Page, press the CHNL Softkey. 2) Press the DIR CH Softkey. The channel number in the Active Channel Box will be highlighted. 3) Press the numbered softkeys located on the bottom of the display to directly select the desired channel number. 4) Press the ENT Key to activate the selected channel. Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number.
Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE In the event of PFD1 or MFD failure, the G1000 system automatically switches to Reversionary (or backup) Mode. Reversionary Mode is a mode of operation in which all important flight information is presented identically on at least one of the remaining displays. Flight parameters are presented in the same format as in normal mode. Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display problem.
Abnormal Operation UNUSUAL ATTITUDES The PFD will ‘declutter’ when the aircraft enters an unusual attitude. Only the primary functions will be displayed in these situations.
Abnormal Operation 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 will automatically revert to Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position combined with continuously updated airspeed and heading data (when available) to calculate and display the aircraft’s current estimated position.
Abnormal Operation 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 will be computed based upon an estimated position and will be displayed as yellow text on the display to denote degraded navigation source information.
Annunciations & Alerts ANNUNCIATIONS & ALERTS CAS MESSAGES Inhibits Warning Caution 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 CB L-R* AFT JBOX LMT L-R* ANTISKID FAIL BATTERY O’TEMP BATTERY O’TEMP BATT TEMP FAIL CABIN ALT CABIN ALT CABIN DOOR CHECK DOORS DUCT O’HEAT L-R* ENG A/I CO
Annunciations & Alerts Inhibits Warning Caution Description Advisory NO TIRE SPINDOWN OIL PRESS LO L-R* OXYGEN OFF P/S HTR L-R* PRESS CTRL STALL WARN FAIL STALL WARN HTR T2 HTR FAIL L-R* TAIL CONE BLD LK TAIL DE-ICE FAIL W/S A/I FAIL L-R* W/S O’HEAT L-R* WING DE-ICE FAIL WOW MISCOMPARE Antiskid control spindown function not working Oil pressure less than redline low limit Oxygen supply off No current detected to pitot static heater PRESS CTRL Pressure controller loss of integrity Air Source Select
Annunciations & Alerts COMPARATOR ANNUNCIATIONS Comparator Window Text ALT MISCOMP Condition Difference in altitude sensors is > 200 ft. If both airspeed sensors detect < 35 knots, this is inhibited. IAS MISCOMP If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts. If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts. HDG MISCOMP Difference in heading sensors is > 6 degrees. PIT MISCOMP Difference in pitch sensors is > 5 degrees.
Annunciations & Alerts G1000 SYSTEM FAILURE ANNUNCIATIONS GIA 63W Integrated Avionics Units GIA 63W Integrated Avionics Units GDC 74B Air Data Computer GEA 71 Engine Airframe Unit OR GIA 63W Integrated Avionics Unit GRS 77 AHRS OR GMU 44 Magnetometer FADEC GDC 74B Air Data Computer G1000 System Failure Annunciations GIA 63W Integrated Avionics Units GTX 33/33D Transponder OR GIA 63W Integrated Avionics Units System Annunciation Red ‘X’ Messages Window Message Softkey Annunciation G1000 System Mess
Annunciations & Alerts MFD & PFD Message Advisories Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. PFD2 SERVICE – PFD2 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair. MANIFEST – PFD1 software mismatch. Communication halted. MANIFEST – PFD2 software mismatch. Communication halted. MANIFEST – MFD1 software mismatch.
Annunciations & Alerts MFD & 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. Reducing power usage. PFD1 “KEY” KEYSTK – Key is stuck. PFD2 “KEY” KEYSTK – Key is stuck. MFD1 “KEY” KEYSTK – Key is stuck. Comments The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the G1000 system should be serviced.
Annunciations & Alerts 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. MFD1 DB ERR – MFD1 terrain database error exists. PFD1 DB ERR – PFD1 terrain database error exists. PFD2 DB ERR – PFD2 terrain database error exists. MFD1 DB ERR – MFD1 obstacle database error exists. PFD1 DB ERR – PFD1 obstacle database error exists.
Annunciations & Alerts Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 Chartview database error exists. MFD1 DB ERR – MFD1 FliteCharts database error exists. DB MISMATCH – Aviation database version mismatch. Xtalk is off. DB MISMATCH – Aviation database type mismatch. Xtalk is off. DB MISMATCH – Terrain database version mismatch. Xtalk is off. DB MISMATCH – Terrain database type mismatch. Xtalk is off. DB MISMATCH – Obstacle database version mismatch.
Annunciations & Alerts GMA 1347D Message Advisories Message GMA1 FAIL – GMA1 is inoperative. GMA2 FAIL – GMA2 is inoperative. GMA XTALK – GMA crosstalk error has occurred. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. An error has occurred in transferring data between the two GMAs. The G1000 system should be serviced. GMA1 CONFIG – GMA1 configuration The audio panel configuration settings do not error. Config service req’d.
Annunciations & Alerts GIA 63W Message Advisories (Cont.) Message GIA1 COOLING – GIA1 temperature too low. GIA2 COOLING – GIA2 temperature too low. GIA1 COOLING – GIA1 over temperature. GIA2 COOLING – GIA2 over temperature. GIA1 SERVICE – GIA1 needs service. Return the unit for repair. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. HW MISMATCH – GIA hardware mismatch. GIA1 communication halted. HW MISMATCH – GIA hardware mismatch. GIA2 communication halted. MANIFEST – GIA1 software mismatch.
Annunciations & Alerts GIA 63W Message Advisories (Cont.) Message COM1 PTT – COM1 push-to-talk key is stuck. COM2 PTT – COM2 push-to-talk key is stuck. COM1 RMT XFR – COM1 remote transfer key is stuck. COM2 RMT XFR – COM2 remote transfer key is stuck. LOI – GPS integrity lost. Crosscheck with other NAVS. GPS NAV LOST – Loss of GPS navigation. Insufficient satellites. GPS NAV LOST – Loss of GPS navigation. Position error. GPS NAV LOST – Loss of GPS navigation. GPS fail. ABORT APR – Loss of GPS navigation.
Annunciations & Alerts GIA 63W Message Advisories (Cont.) Message NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair.
Annunciations & Alerts GTX 33 & GTX 33D Message Advisories Message Comments XPDR1 CONFIG – XPDR1 config error. The transponder configuration settings do not Config service req’d. match those of backup configuration memory. The G1000 system should be serviced. XPDR2 CONFIG – XPDR2 config error. The transponder configuration settings do not Config service req’d. match those of backup configuration memory. The G1000 system should be serviced. MANIFEST – GTX1 software The transponder has incorrect software mismatch.
Annunciations & Alerts GRS 77 Message Advisories (Cont.) Message AHRS1 GPS – AHRS1 using backup GPS source. Comments The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The G1000 system should be serviced when possible. AHRS2 GPS – AHRS2 using backup The #2 AHRS is using the backup GPS path. GPS source. Primary GPS path has failed. The G1000 system should be serviced when possible. The #1 AHRS is not receiving any or any AHRS1 GPS – AHRS1 not receiving any GPS information.
Annunciations & Alerts GRS 77 Message Advisories (Cont.) Message Comments AHRS2 SRVC – AHRS2 Magnetic-field The #2 AHRS earth magnetic field model is model needs update. out of date. Update magnetic field model when practical. GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits South, no magnetic compass. for approved AHRS operation. Heading is GEO LIMITS – AHRS2 too far North/ flagged as invalid. South, no magnetic compass.
Annunciations & Alerts GDL 69A Message Advisories Message GDL69 CONFIG – GDL 69 configuration error. Config service req’d. 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 MANIFEST – GDL software mismatch. The GDL 69 has incorrect software installed. Communication halted.
Annunciations & Alerts GCU 475 Message Advisories (Cont.) Message GCU FAIL – GCU is inoperative. Comments A failure has been detected in the GCU 475. The GCU 475 is unavailable. MANIFEST – GCU software mismatch. The GCU 475 has incorrect software installed. Communication halted. The G1000 system should be serviced. GMC 710 Message Advisories Message GMC CONFIG – GMC Config error. Config service req’d. GMC FAIL – GMC is inoperative. MANIFEST – GMC software mismatch. Communication halted.
Annunciations & Alerts Miscellaneous Message Advisories Message FPL WPT LOCK – Flight plan waypoint is locked. Comments Upon power-up, the G1000 system detects that a stored flight plan waypoint is locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.
Annunciations & Alerts Miscellaneous Message Advisories (Cont.) Message LOCKED FPL – Cannot navigate locked flight plan. WPT ARRIVAL – Arriving at waypoint -[xxxx] STEEP TURN – Steep turn ahead. INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm. LEG UNSMOOTH – Flight plan leg will not be smooth. APPR INACTV – Approach is not active. SLCT FREQ – Select appropriate frequency for approach.
Annunciations & Alerts Miscellaneous Message Advisories (Cont.) Message PTK FAIL – Past IAF, parallel offset not activated. UNABLE V WPT – Can’t reach current vertical waypoint. Comments 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 will automatically transition to the next vertical waypoint. VNV – Unavailable.
Annunciations & Alerts AFCS ALERTS Condition Annunciation Description Pitch Failure Pitch axis control failure. AP is inoperative. Roll Failure Roll axis control failure. AP is inoperative. MET Switch Stuck, or Pitch Trim Axis Control Failure If annunciated when AP is engaged, a failure has occurred in the pitch trim system. If annunciated when AP is not engaged, a failed or stuck switch is causing the annunciation. System Failure AP and MET are unavailable. FD may still be available.
Annunciations & Alerts TAWS ALERTS SUMMARY Alert Type PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message Excessive Descent Rate Warning (EDR) Reduced Required Terrain Clearance Warning (RTC) Imminent Terrain Impact Warning (ITI) “Pull Up” or * “Terrain, Terrain; Pull Up, Pull Up”* or “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up” or * Reduced Required Obstacle Clearance Warning (ROC) Imminent Obstacle Impact Warning (IOI) or * “Obstacle, Obstacle; Pull Up, Pull Up”* or “Obstacle Ah
Annunciations & Alerts Alert Type PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Reduced Required Obstacle Clearance Caution (ROC) * “Caution, Obstacle; Caution, Obstacle”* or Imminent Obstacle Impact Caution (IOI) Aural Message or “Obstacle Ahead; Obstacle Ahead” or * Premature Descent Alert Caution (PDA) Altitude Callout “500” “Obstacle Ahead; Obstacle Ahead” or “Caution, Obstacle; Caution, Obstacle”* “Too Low, Terrain” None None “Five-Hundred” Excessive Descent Rate Caution (EDR) “Sink
Annunciations & Alerts OTHER G1000 AURAL ALERTS Aural Alert Description “Minimums, minimums” The aircraft has descended below the preset barometric minimum descent altitude. “Vertical track” “Traffic” “TIS not available” 72 The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled. The Traffic Information Service (TIS) has issued a Traffic Advisory alert The aircraft is outside the Traffic Information Service (TIS) coverage area.
Appendix APPENDIX PFD SOFTKEY MAP Top Level PFD Softkeys Select the BACK or OFF Softkey to return to the top-level softkeys. Inset Map Softkeys Displays Inset Map in PFD lower left corner INSET OFF Removes Inset Map DCLTR (3) Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except the active flight plan 190-00600-00 Rev.
Appendix TRAFFIC Displays traffic information on Inset Map TOPO Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map Displays terrain information on Inset Map TERRAIN NEXRAD XM LTNG Displays NEXRAD weather and coverage information on Inset Map (optional feature) Displays XM lightning information on Inset Map (optional feature) SENSOR ADC1 ADC2 AHRS1 AHRS2 BACK MSG Select the BACK Softkey to return to the top level softkeys.
Appendix FD FRMT ALT UNIT Select the STD BARO or BACK Softkey to return to the top-level softkeys METERS IN HPA SNGL CUE X POINTR PFD Configuration Softkeys Displays second-level softkeys for additional PFD configurations Displays the softkeys for selecting the two flight director formats PFD FD FRMT SNGL CUE Selects the single cue flight director format X POINTR Selects the cross pointer flight director format OPTN 1 Resets PFD to default settings, including changing units to standard Displays sof
Appendix OPTN 3 OFF Cycles the Bearing 1 Information Window through NAV1 or GPS/waypoint identifier and GPS-derived distance information, and ADF/frequency. Cycles the Bearing 2 Information Window through NAV2 or GPS/waypoint identifier and GPS-derived distance information, and ADF/frequency.
Appendix MSG Select the BACK Softkey to return to the top-level softkeys. MSG Select the IDENT or BACK Softkey to return to the top-level softkeys.
Appendix 0—7 Use numbers to enter code BKSP Removes numbers entered, one at a time 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 Messages Window IDENT MFD SOFTKEY MAP CAS ↑ CAS ↓ DCLTR MAP (optional) (optional) SHW CHRT CHKLIST DCLTR-1 DCLTR-2 DCLTR-3 TRAFFIC TOPO TERRAIN AIRWAYS Select the BACK Softkey on this le
Appendix TRAFFIC Displays traffic information on Navigation Map Displays topographical data (e.g.
Appendix SD CARD USE The G1000 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 well as Jeppesen aviation and ChartView database updates. Jeppesen Databases The Jeppesen aviation database is updated on a 28-day cycle. 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.
Appendix 3) Press the ENT Key to start the database update. A prompt similar to the following is displayed: Database Update Confirmation 4) After the update completes, the PFD starts in normal mode. 5) Turn the G1000 System OFF and remove the SD card. 6) Repeat steps 1 through 4 for the MFD. The MFD and PFD databases are now updated. Remove the SD card when finished. 7) Verify that the correct update cycle is loaded during startup of the MFD.
Appendix Data Card containing identical database versions must be kept in each display unit. The basemap database contains data for the topography and land features, such as rivers, lakes and towns. It is updated only periodically, with no set schedule. There is no expiration date. The terrain and airport terrain databases contain the terrain mapping and airport diagram data. They are updated periodically and have no expiration date.
Appendix After the data has been copied to the appropriate data cards, perform the following steps: 1) Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of the PFD. The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD. 2) Apply power to the G1000 System. View the MFD power-up splash screen. Check that the databases are initialized and displayed on the scrolling window of the splash screen.
Appendix Blank Page 84 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-00 Rev.
Index A Activate a flight plan 12 Active Channel 43 ADF 5, 6 Age 31 AHRS 52, 61, 62, 63, 64, 65 Airways 20, 79 Air Data Computer 51, 52 Alert messages 65 Antenna stabilization 39 Antenna tilt 37 AP 69 APR Softkey 42 Attitude & Heading Reference System 51 Audio panel controls NAV1, NAV2 6 Aural alerts 72 Automatic Flight Control System (AFCS) Alerts 69 Database Updates 79 DCLTR Softkey 41 Dead Reckoning 47 Declutter 46, 73, 79 Direct-to 11 DME 5, 6 DR mode 47, 48 E Edit a flight plan 22 EDR 35 F FD 69 Five-
Index J P Jeppesen 41, 80 Jeppesen aviation database 80 PDA 34 PIT 51 Play 7 Playback 7 L Lighted obstacle 33 M Map panning 30 Message advisories 53 – 57, 60 – 68 MET 69 METAR 29 Minimums 72 MISCOMP 51 Mistrim 69 Mode S 77 Mode selection softkeys 6 Multi Function Display (MFD) Softkeys 78 R RADIO softkey 43 ROC 70, 71 S SafeTaxi™ 41 Sector scan 39 Secure Digital (SD) card 80 Sensor 51 STAB 39 Standby 37 STAR Softkey 42 Store Flight Plan 21 N T NACO 41 NAV 6, 10 NAV1 2, 6 NAV2 2, 6 Navigation datab
Index V Vertical deviation guidance 14 Vertical Navigation Altitude Capture 9 Vertical Path Tracking 9 Vertical speed guidance 14 Vertical track 72 VNV 9, 11, 12, 46, 68 Vspeed 2 W WAAS 26, 58 WATCH 40 Weather Attenuated Color Highlight 40 Weather data link page 29 Weather radar 36 Wind data 75 WX Softkey 42 X XM lightning 74, 79 XM weather 29 XPDR softkey 6 190-00600-00 Rev.
Index Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-00 Rev.
Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/0870.851241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com © 2006 Garmin Ltd.
