G1000 TM pilot’s guide appendices
Record of Revisions Revision Date of Revision Revision Page Range A 11/30/04 A-1 – A-2 B-1 – B-6 C-1 – C-4 D-1 – D-2 E-1 – E-2 F-1 – F-4 G-1 – G-3 Description Initial release. Garmin G1000 Pilot’s Guide Appendices 190-00383-02 Rev.
APPENDIX A SD CARD USE 4. 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 terrain database storage as well as aviation database updates. After the update completes, the PFD starts in normal mode. Remove the aviation database update SD card from the PFD. 5. Turn the G1000 system OFF. 6. Repeat steps 1 through 4 for the MFD. The MFD and PFD aviation databases are now updated. 7.
APPENDIX A This page intentionally left blank. A-2 Garmin G1000 Pilot’s Guide Appendices 190-00383-02 Rev.
APPENDIX B Abbreviation or Acronym ADF AF AFM AFMS AGL AHRS AIM AIRMET ALT AMPS ANNUNC APPR APR APT ARINC ARSPC ARTCC ARV AS ASB ATC ATCRBS AUTOSEQ AUX Definition Automatic Direction Finder Arc to fix Aircraft Flight Manual Aircraft Flight Manual Supplement Above Ground Level Attitude and Heading Reference System Airman’s Information Manual Airman’s Meteorological Information Altitude Amperes Annunciation Approach Approach Airport Aeronautical Radio Incorporated Airspace Air Route Traffic Control Center Arriv
APPENDIX B B-2 Abbreviation or Acronym FMS FOB FPL FPM FREQ FRZ FSS ft Definition Flight Management System Fuel On Board Flight Plan Feet Per Minute Frequency Freezing Flight Service Station Foot/feet G/S GAL GDC GDU GEA GIA GL GMU GND GPH GPS GRS GS GTX Glideslope Gallon(s) Garmin Air Data Computer Garmin Display Unit Garmin Engine/Airframe Unit Garmin Integrated Avionics Unit Gallon(s) Garmin Magnetometer Unit Ground Gallons per Hour Global Positioning System Garmin Reference System Ground Speed Garmi
APPENDIX B Abbreviation or Acronym NDB Nexrad nm NRST Definition Non-directional Beacon Next Generation Radar Nautical Mile(s) Nearest O OAT OBS Outer Marker Outside Air Temperature Omni Bearing Selector P ALT PA PASS PFD PI POSN P.
APPENDIX B B-4 Abbreviation or Acronym VD VERT VFR VHF VI VLOC VM VMC VNAV VOL VOR VPROF VR VS Vspeed Definition Heading Vector to DME Distance Vertical Visual Flight Rules Very High Frequency Heading Vector to Intercept VOR/Localizer Receiver Heading Vector to Manual Termination Visual Meteorological Conditions Vertical Navigation Volume VHF Omnidirectional Range VNAV Profile Heading Vector to Radial Vertical Speed Airspeed WAAS WGS-84 WPT WPTS WW WX Wide Area Augmentation System World Geodetic System -
APPENDIX B Navigation Term Bearing Calibrated Airpseed Course Course to Steer Crosstrack Error Cumulative Distance Dillution of Precision Desired Track Efficiency Endurance Enroute Safe Altitude Estimated Position Error Estimated Time of Arrival Estimated Time Enroute Fuel Flow Fuel On Board Groundspeed Heading 190-00383-02 Rev. A Definition The compass direction from your present position to a destination waypoint. Indicated airspeed corrected for installation and instrument errors.
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APPENDIX C QUESTIONS & ANSWERS This Appendix answers common questions regarding G1000 system operational capabilities. If a particular subject is not covered in this Appendix, the index may be used to find the appropriate section in this manual. If a sufficient answer is still not found, an authorized Garmin dealer or contact Garmin directly (see Copyright page). Garmin is dedicated to supporting its products and customers.
APPENDIX C mation from the current database to define the waypoints. If the database is changed or updated, the G1000 system automatically updates the information, provided the procedure has not been modified. Should an approach, departure, or arrival procedure no longer be available, the flight plan becomes locked until the procedure is deleted from the flight plan. Can “slant Golf” (“/G”) be filed using the G1000? “/G” may be filed for a flight plan.
APPENDIX C Why does the G1000 not automatically sequence to the next waypoint? The G1000 only sequences flight plan waypoints when automatic sequencing is enabled (i.e., no “OBS” or “SUSP” annunciation). For automatic sequencing to occur, the aircraft must also cross the “bisector” of the turn being navigated. The bisector is a perpendicular line between two flight plan legs which crosses through the waypoint common to both legs.
APPENDIX C After a missed approach, how can the same approach be re-selected? How can a new approach be activated? After flying the missed approach procedure, the pilot may reactivate the same approach for another attempt from the Procedures Page. Once the clearance is given for another attempt, activate the approach from the Procedures Page by highlighting “Activate Approach?”, then pressing the ENT key.
APPENDIX D G1000 MAP DATUMS The G1000 system supports the following map datums. WARNING: WGS 84 is the default datum and should be used in all situations except when another datum is specifically required for safe navigation. Pilots using map datums other than WGS 84 do so at their own risk.
APPENDIX D G1000 MAP DATUMS (CONT.
APPENDIX E GENERAL TIS INFORMATION INTRODUCTION The Traffic Information Service (TIS) provides traffic advisory information in the cockpit of non-TCAS equipped aircraft. TIS is a ground-based service providing relative location of all ATCRBS Mode-A and Mode-C transponder equipped aircraft within a specified service volume. The TIS ground sensor uses real time track reports to generate traffic notification. The G1000 system displays TIS traffic information on the Traffic Map Page of the MFD.
APPENDIX E NOTE: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in mountainous regions. TIS information is collected during a single radar sweep. Collected information is then sent through the Mode S uplink on the next radar sweep. Because of this, the surveillance information is approximately five seconds old. TIS ground station tracking software uses prediction algorithms to compensate for this delay.
APPENDIX F MAP SYMBOLS BASEMAP AIRPORT Item Interstate Highway – 2-digit drawn inside Item Symbol Symbol Unknown Airport Interstate Highway – 3-digit drawn inside Non-towered, Non-serviced Airport State Highway – 2-digit drawn inside Towered, Non-serviced Airport State Highway – 3-digit drawn inside Non-towered, Serviced Airport State Highway – 4-digit drawn inside State Highway – 5-digit drawn inside Towered, Serviced Airport US Highway – 2-digit drawn inside Restricted (Private) Airport U
APPENDIX F TRAFFIC MISCELLANEOUS Item Symbol Traffic Item ARTCC Frequency or FSS Frequency Proximate Traffic Default Map Cursor Symbol Elevation Pointer Cursor Traffic Advisory, Out of Range Measuring Cursor Traffic Advisory Overzoom Indicator (map toolbar) LIGHTNING STRIKE Item Lightning Strike – Age is 0-6 Seconds Lightning Strike – Age is 6-20 Seconds Terrain Proximity Enabled (map toolbar) Symbol Traffic Enabled (map toolbar) User Waypoint Wind Vector Lightning Strike – Age is 20-60 Seconds L
APPENDIX F LINE SYMBOLS Item ICAO Control Area Class B Airspace Symbol Mode C Tower Area Warning Area Alert Area Caution Area Danger Area Prohibited Area Restricted Area Training Area Unknown Area Class C Terminal Radar Service Area Mode C Area Military Operations Area (MOA) State or Province Border International Border Road Railroad Lattitude/Longitude 190-00383-02 Rev.
APPENDIX F OBSTACLE DATABASE Obstacle Color RED YELLOW GRAY Indication WARNING: Obstacle height is at or above 100 ft below the current aircraft altitude. CAUTION: Obstacle height is between 100 ft and 1000 ft below the current aircraft altitude. SAFE: Obstacle height is lower than 1000 ft below the current aircraft altitude.
APPENDIX G G1000 SYSTEM SPECIFICATIONS GDU 1040 MFD & PFD GIA 63 INTEGRATED AVIONICS UNITS Physical Specifications Physical Specifications Height: Width: Depth: Weight: Voltage Range: Display: 7.70 inches (19.56 cm) 11.80 inches (29.97 cm) 3.55 inches (9.02 cm) 6.6 lb (2.99 kg) 9 – 33 Vdc 10.
APPENDIX G GDC 74A AIR DATA COMPUTER GEA 71 ENGINE/AIRFRAME UNIT Physical Specifications Physical Specifications Height: Width: Length: Weight: Voltage Range: 3.23 inches (8.20 cm) 3.05 inches (7.75 cm) 6.45 inches (16.38 cm) 1.69 lb (0.77 kg) 10 – 33 Vdc Pressure Altitude Range: -1,400 feet to 50,000 feet Vertical Speed Range: -20,000 fpm to +20,000 fpm Airspeed Range: 450 knots Airspeed Mach Range: <1.
APPENDIX G GRS 77 AHRS AHRS Performance Physical Specifications Height: Width: Length: Weight: Voltage Range: 3.25 inches (8.36 cm) 3.75 inches (9.53 cm) 8.5 inches (21.59 cm) 2.40 lb (1.08 kg) 10 – 33 Vdc Bank/Pitch Error: Maneuvers Range: Rotation Rate: Heading: ±1.
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