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 11 of 65
NOTE
Each GIA 63W 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 displayed in the ALERTS window 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.
•
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.
G1000 GPS/SBAS NAVIGATION SYSTEM, GIA 63W INSTALLED,
G1000 SYSTEM SW 0369.13 USING GPS SW 2.40
The Garmin G1000 GPS/SBAS receivers, GIA 63W, incorporating SW version
2.40 do not comply with US 14 CFR Part 91, SFAR 97 requirements for TSO-
C145a/TSO-C146a equipment. See Limitations Section for requirements to the
use GPS for navigation.
The Garmin G1000 system with GPS SW 2.40 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
Summary of Contents for Cessna Caravan G1000
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