Garmin Cessna Caravan G1000 Guide de configuration
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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Garmin Ltd. Or its subsidiaries
c/o Garmin International
1200 E. 151st Street
Olathe, KS 66062 USA
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
LOG OF REVISIONS
Revision
Number Page
Number(s) Description FAA
Approved Date of
Approval
1 All Initial Release Robert
Murray 7/26/2007
2 All Add Software Levels Robert
Murray 9/6/2007
3 All Add Software Levels Robert
Murray 2/28/2008
4 All Add Software Levels Robert
Murray 4/4/2008
5 All
Update Software Levels
for non-WAAS See Page
1 See Page
1
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
Table of Contents
SECTION I
GENERAL..........................................................................................................7
(NOT FAA APPROVED)
SECTION II
LIMITATIONS................................................................................................14
(FAA APPROVED)
SECTION III
EMERGENCY PROCEDURES.....................................................................26
(NOT FAA APPROVED)
SECTION IVA
NORMAL PROCEDURES.............................................................................40
(NOT FAA APPROVED)
SECTION IVB
ABNORMAL PROCEDURES.......................................................................58
(NOT FAA APPROVED)
SECTION V
PERFORMANCE............................................................................................58
(NOT FAA APPROVED)
SECTION VI
WEIGHT AND BALANCE............................................................................58
(NOT FAA APPROVED)
SECTION VII
SYSTEM DESCRIPTIONS............................................................................59
(NOT FAA APPROVED)
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 7 of 65
SECTION I
GENERAL
(Not FAA Approved)
G1000
The G1000 Integrated Avionics System is a fully integrated flight, engine,
communication, navigation and surveillance instrumentation system. The
system consists of a Primary Flight Display (PFD), Multi-Function Display
(MFD), audio panel, Air Data Computer (ADC), Attitude and Heading
Reference System (AHRS), engine sensors and processing unit (GEA), and dual
integrated avionics units (GIA) each containing VHF communications, VHF
navigation, and GPS (Global Positioning System).
GIA 63 units are standard and provide non-WAAS GPS position information in
accordance with TSO-C129a class A1. Optional GIA 63W units provide
WAAS augmented GPS position. If the optional GIA63W units incorporate
GPS software level 3.0 or later, the GPS system meets the requirements of TSO-
C145a.
The primary function of the PFD is to provide attitude, heading, air data,
navigation, and alerting information to the pilot. The PFD may also be used for
flight planning. The primary function of the MFD is to provide engine
information, mapping, terrain information, and flight planning. The audio panel
is used for selection of radios for transmitting and listening, intercom functions,
and marker beacon functions.
The primary function of the VHF Communication portion of the G1000 is to
enable external radio communication. The primary function of the VOR/ILS
Receiver portion of the equipment is to receive and demodulate VOR, Localizer,
and Glide Slope signals. The primary function of the GPS portion of the system
is to acquire signals from the GPS system satellites (and WAAS satellites if so
equipped), recover orbital data, make range and Doppler measurements, and
process this information in real-time to obtain the user's position, velocity, and
time.
If the optional TAWS function is installed in the G1000, the pilot will receive
appropriate aural warnings and cautions for terrain and obstacles. The pilot
should refer to the DA 40/DA 40F Pilot’s Guide for the terrain warning and
caution messages and system information.
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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Operational Approvals
G1000 GPS NAVIGATION SYSTEM, GIA 63 INSTALLED
GIA 63 units are standard and provide position information in accordance with
TSO-C129a class A1. The Garmin G1000 system has been demonstrated
capable of, and has been shown to meet the accuracy requirements for the
following operations provided it is receiving usable navigation data:
•The G1000 Integrated Avionics system as installed in this aircraft
complies with AC 20-138A for navigation within the U.S. National
Airspace System using GPS for IFR en-route, terminal area, and non-
precision approach operations (including those approaches titled “GPS”,
“or GPS”, and “RNAV (GPS)” approaches).
•The G1000 Integrated Avionics system as installed in this aircraft has
been found to comply with the requirements for GPS as a Primary Means
of Navigation for oceanic and remote navigation – RNP-10, per FAA AC
20-138A, FAA Order 8400-12A, and FAA Order 8700-1. Both GPS
receivers are required to be operating and receiving usable signals except
for routes requiring only one Long Range Navigation sensor. This does
not constitute operational approval.
•North Atlantic (NAT) Minimum Navigational Performance
Specifications (MNPS) Airspace per AC 91-49 and AC 120-33. Both
GPS receivers are required to be operating and receiving usable signals
except for routes requiring only one Long Range Navigation sensor. This
does not constitute operational approval.
NOTE
Each GIA 63 computes an independent navigation solution based on its GPS
sensor. The G1000 will use the GPS sensor with the highest signal quality and
will automatically revert to the other sensor if the active sensor fails or if the
secondary sensor is determined to be more accurate. An “AHRS 1 GPS – “
message means that one of the GPSs has failed. Refer to the MFD AUX-GPS
STATUS page to determine the state of the GPSs.
•Enroute and Terminal including RNP5/BRNAV and PRNAV (RNP-1) -
In accordance with JAA TGL-10 Rev 1, ACJ 20X4, AC 90-96A, and AC
90-100A provided the FMS is receiving usable navigation information
from one or more GPS/SBAS receivers.
•The G1000 Integrated Avionics system as installed in this is aircraft is
eligible for B-RNAV in accordance with AMJ20X2.
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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•The G1000 Integrated Avionics system as installed in this aircraft is
eligible for PRNAV in accordance with PRNAV requirements: JAA
Administrative & Guidance Material Section One: General Part 3:
Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and
Operational Approval for Precession RNAV Operations in Designated
European Airspace 7.1 Required Functions.
•Navigation information is referenced to WGS-84 reference system, and
should only be used where the Aeronautical Information Publication
(including electronic data and aeronautical charts) conform to WGS-84 or
equivalent.
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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G1000 GPS/SBAS NAVIGATION SYSTEM, GIA 63W INSTALLED,
G1000 SYSTEM SW 0321.17OR LATER USING GPS SW 3.0 OR LATER
The Garmin G1000 GPS/SBAS receivers, GIA 63W, incorporating SW version
3.0 or later approved version and GA35 (PN 013-00235-00) antennas are
approved under TSO-C145a/TSO-C146a equipment Class 3 and installed in
accordance with AC 20-138A. The Garmin G1000 system has been
demonstrated capable of, and has been shown to meet the accuracy requirements
for the following operations provided it is receiving usable navigation data:
•The G1000 Integrated Avionics system as installed in this aircraft
complies with AC 20-138A for navigation using GPS and WAAS (within
the coverage of a Space-Based Augmentation System complying with
ICAO Annex 10) for IFR en route, terminal area, and non-precision
approach operations (including those approaches titled “GPS”, “or
GPS”, and “RNAV (GPS)” approaches). The G1000 Integrated Avionics
system installed in this aircraft is approved for approach procedures with
vertical guidance including “LPV”, “LNAV/VNAV”, and “LNAV + V”
within the U.S. National Airspace System.
•The G1000 Integrated Avionics system as installed in this aircraft has
been found to comply with the requirements for GPS as a Primary Means
of Navigation for oceanic and remote navigation – RNP-10, (per FAA
AC 20-138A, FAA Order 8400-12A, and FAA Order 8700-1), when
used in conjunction with Garmin WAAS Fault Detection/Exclusion
(WFDE) Prediction Program, part number 006-A0154-01 or later
approved version with GA35 (PN 013-00235-00) antennas selected. Both
GPS/SBAS receivers are required to be operating and receiving usable
signals except for routes requiring only one Long Range Navigation
(LRN) sensor. This does not constitute an operational approval.
•The G1000 WFDE predication program works in combination with the
Garmin AT, Inc. Route Planning Software, version 1.2, or later approved
version. The route planning and WFDE prediction program can be
downloaded from Garmin G1000 website on the Internet. For
information on using the WFDE Prediction Program, refer to Garmin
WAAS FDE Prediction Program, part number 190-00643-01, ‘WFDE
Prediction Program Instructions’.
•North Atlantic (NAT) Minimum Navigational Performance
Specifications (MNPS) Airspace per AC 91-49 and AC 120-33. Both
GPS/SBAS receivers are required to be operating and receiving usable
signals except for routes requiring only one Long Range Navigation
sensor. This does not constitute operational approval.
Autres manuels pour Cessna Caravan G1000
46
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