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Diamond
®
G1000 Pilot’s Guide
DA40/40F
®
Integrated Flight Deck
G1000
Pilot’s Guide
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.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:8
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Untitled-1 1 11/13/2007 9:15:37 AM
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SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX
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Copyright © 2006-2009 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0321.20 or later for the Diamond DA40 or DA40F. 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.
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LIMITED WARRANTY LIMITED WARRANTY This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, mis
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WARNINGS, CAUTIONS, AND NOTES WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
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WARNINGS, CAUTIONS, AND NOTES WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic. The aircraft should be maneuvered based only upon ATC guidance or positive visual acquisition of conf
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WARNINGS, CAUTIONS, AND NOTES NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, ar
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REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190-00592-00 A 11/10/05 i – I-6 Optional fuel pressure gauge information added 190-00592-01 A 6/16/06 i – I-4 GFC 700 information added 190-00592-02 A 7/20/06 i – I-4 TAWS information added GDL 69A crew muting information added 190-00592-03 A 4/20/07 i – I-6 EIS updated Airways information added WAAS information added VNV information added Charts information added Stormscope information added TAS600 informa
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TAbLE OF CONTENTS SECTION 1 SYSTEM OVERVIEW 2.4 Abnormal Operations ........................................... 74 Abnormal GPS Conditions ........................................... 74 1.1 Line Replaceable Units ........................................... 2 Unusual Attitudes ....................................................... 75 1.2 Secure Digital (SD) Cards ....................................... 7 SECTION 3 ENGINE INDICATION SYSTEM 1.3 System Power-up ...................................
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TAbLE OF CONTENTS Entertainment Inputs ................................................ 128 Flight Plan Views ...................................................... 219 Closest Point of FPL .................................................. 221 4.6 Audio Panel Preflight Procedure ....................... 129 5.7 Vertical Navigation ............................................. 222 4.7 Abnormal Operation ........................................... 130 Altitude Constraints .........................
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TAbLE OF CONTENTS TAS Voice Alerts ........................................................ 353 SECTION 8 ADDITIONAL FEATURES System Status ........................................................... 354 8.1 Synthetic Vision System (SVS) (Optional) ......... 404 SVS Operation .......................................................... 405 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM SVS Features ............................................................ 407 7.1 AFCS Controls ....................
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SYSTEM FLIGHT AUDIO PANEL FLIGHT HAZARD ADDITIONAL EIS AFCS APPENDICES INDEX OVERVIEW INSTRUMENTS & CNS MANAGEMENT AVOIDANCE FEATURES SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the GFC 700 AFCS. The G1000 Integrated Flight Deck System presents flight instrumentation, position, navigation, communication, and identification information using flat-panel color displays. The system is distributed across the following
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SYSTEM OVERVIEW 1.1 LINE REPLACEAbLE UNITS • GDU 1040/1042/1044 (2) – A GDU 1040 is configured as the Primary Flight Display (PFD) and a GDU 1040, 1042 or 1044 (1042/1044 for airframes equipped with the GFC 700) as a Multi Function Display (MFD). Both displays feature 10.4-inch LCD screens with 1024 x 768 resolution. The displays communicate with each other through a High-speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet connection to an IAU. The thr
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SYSTEM FLIGHT AUDIO PANEL FLIGHT HAZARD ADDITIONAL EIS AFCS APPENDICES INDEX OVERVIEW INSTRUMENTS & CNS MANAGEMENT AVOIDANCE FEATURES SYSTEM OVERVIEW GDC 74A – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface. • GEA 71 – The Engi
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SYSTEM OVERVIEW • GMU 44 – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with it via an RS-485 digital interface. • GDL 69/69A – The Data Link Satellite Radio Receiver provides real-time weather information to MFD maps and the PFD Inset Map. The GDL 69A model is also capable of providing digital audio entertainment. The Data Link Receiver comm
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SYSTEM FLIGHT AUDIO PANEL FLIGHT HAZARD ADDITIONAL EIS AFCS APPENDICES INDEX OVERVIEW INSTRUMENTS & CNS MANAGEMENT AVOIDANCE FEATURES SYSTEM OVERVIEW High-Speed Data Bus (Ethernet) GMA 1347 GDU 1040 (PFD) GDU 1040/1042/1044 (MFD) Audio Panel Reversionary Reversionary Control Control GDC 74A Air Data Computer OAT No. 1 GIA 63/63W No. 2 GIA 63/63W Airspeed Integrated Avionics Unit Integrated Avionics Unit Altitude Vertical Speed System Inegration Processors System Integrat
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SYSTEM OVERVIEW High-Speed Data Bus (Ethernet) No. 2 GIA 63/63W Integrated Avionics Unit GDL 69/69A System Integration Processors Data Link Receiver I/O Processors Real-time Weather and VHF COM Digital Audio Entertainment VHF NAV/LOC (subscription-based service) GPS/WAAS Glideslope L3 Becker Avidyne Honeywell Honeywell Stormscope RA 3502-(1) KN 63 TAS600-series KAP 140 Lightning Strike and DME Autopilot ADF Receiver T raffic Information Thunderstorm Detection (optional) (optional) (optional)
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SYSTEM FLIGHT AUDIO PANEL FLIGHT HAZARD ADDITIONAL EIS AFCS APPENDICES INDEX OVERVIEW INSTRUMENTS & CNS MANAGEMENT AVOIDANCE FEATURES SYSTEM OVERVIEW 1.2 SECURE DIGITAL (SD) CARDS NOTE: Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to Appendix B for instructions on updating databases. The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels. Each display bezel is equipped with two SD card slo
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SYSTEM OVERVIEW 1.3 SYSTEM POWER-UP NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. NOTE: Refer to Appendix A for system-specific annunciations and alerts. The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features that exercise the proce
