Page 1-16
GNS 400W Series Installation Manual
Rev. G
190-00356-08
equipment may be required to obtain operational approval to utilize RNP-4 performance. This does not
constitute an operational approval.
The Garmin GNSS navigation system complies with the accuracy, integrity, and continuity of function,
and contains the minimum system functions required for P-RNAV operations in accordance with JAA
Administrative & Guidance Material Section One: General Part 3: Temporary Guidance Leaflets, Leaflet
No 10 (JAA TGL-10 Rev 1). The GNSS navigation system has [a TSO-C146a Class 3 approved Garmin
GNS 430W] navigation unit[s]. The Garmin GNSS navigation system complies with the accuracy,
integrity, and continuity of function, and contains the minimum system functions required for B-RNAV
operations in accordance with EASA AMC 20-4. The Garmin GNSS navigation system complies with
the equipment requirements for P-RNAV and B-RNAV/RNAV-5 operations in accordance with AC 90-
96A CHG 1. This does not constitute an operational approval.
Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with AC 20-153
for database integrity, quality, and database management practices for the navigation database. Flight
crew and operators can view the LOA status at
FlyGarmin.com
then select ―Type 2 LOA Status.‖
Navigation information is referenced to the WGS-84 reference system.
For FAA approved installations in non- U.S. registered aircraft:
For installations outside the United States of America or in non-U.S. registered aircraft, installations
should comply with applicable regulations and guidance of the cognizant Civil Aviation Authority.
Note that for some types of aircraft operation and for operation in non-U.S. airspace, separate operational
approval(s) may be required in addition to equipment installation and airworthiness approval.
GARMIN GNSS (GPS/SBAS) NAVIGATION SYSTEM LIMITATIONS
The flight crew must confirm at system initialization that the navigation database is current. The
navigation database is expected to be current for the duration of the flight. If the AIRAC cycle will
change during flight, the flight crew must ensure the accuracy of navigation data, including suitability of
navigation facilities used to define the routes and procedures for flight. If an amended chart affecting
navigation data is published for the procedure, the database must not be used to conduct the procedure.
GPS/SBAS based IFR en route, oceanic, and terminal navigation is prohibited unless the flight crew
verifies and uses a valid, compatible, and current navigation database or verifies each waypoint for
accuracy by reference to current approved data.
Discrepancies that invalidate a procedure must be reported to Garmin International. The affected
procedure is prohibited from being flown using data from the navigation database until a new navigation
database is installed in the aircraft and verified that the discrepancy has been corrected. Navigation
database discrepancies can be reported at
FlyGarmin.com
then select ―Aviation Data Error Report.‖
Flight crew and operators can view navigation database alerts at
FlyGarmin.com
then select ―NavData
Alerts.‖
For flight planning purposes, in areas where SBAS coverage is not available, the pilot must check RAIM
availability.
Within the
United States
, RAIM availability can be determined using the Garmin WFDE
Prediction program, Garmin part number 006-A0154-03 (included in GNS trainer) software
version 3.00 or later approved version with Garmin approved antennas, or the FAA‘s en route
and terminal RAIM prediction website:
, or by contacting a Flight
Service Station.
Within
Europe
, RAIM availability can be determined using the Garmin WFDE Prediction
program or Europe‘s AUGER GPS RAIM Prediction Tool at
http://augur.ecacnav.com/augur/app/home
For
other areas
, use the Garmin WFDE Prediction program.
Содержание GPS 400W
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Страница 152: ...Page F 6 GNS 400W Series Installation Manual Rev G 190 00356 08 Figure F 4 GPS 400W Mounting Rack Installation...
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Страница 159: ...GNS 400W Series Installation Manual Page H 3 190 00356 08 Rev G Figure H 1 400W Series System Interface Diagram...
Страница 160: ...Page H 4 GNS 400W Series Installation Manual Rev G 190 00356 08 Figure H 2 GNS 430W Typical Installation Sheet 1 of 2...
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Страница 164: ...Page H 8 GNS 400W Series Installation Manual Rev G 190 00356 08 Figure H 4 GPS 400W Typical Installation Sheet 1 of 2...
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Страница 169: ...GNS 400W Series Installation Manual Page H 13 190 00356 08 Rev G Figure H 6 Altitude Gray Code Interconnect...
Страница 173: ...GNS 400W Series Installation Manual Page H 17 190 00356 08 Rev G Figure H 11 ARINC 429 EFIS Interconnect Sheet 1 of 2...
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Страница 184: ...Page H 28 GNS 400W Series Installation Manual Rev G 190 00356 08 Figure H 17 GTX 330 Interconnect...
Страница 187: ...GNS 400W Series Installation Manual Page H 31 190 00356 08 Rev G Figure H 19 Audio Panel Interconnect Sheet 1 of 2...
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Страница 189: ...GNS 400W Series Installation Manual Page H 33 190 00356 08 Rev G Figure H 20 VOR ILS Indicator Interconnect...
Страница 190: ...Page H 34 GNS 400W Series Installation Manual Rev G 190 00356 08 Figure H 21 RMI OBI Interconnect...
Страница 191: ...GNS 400W Series Installation Manual Page H 35 190 00356 08 Rev G Figure H 22 King Serial Panel DME Tuning Interconnect...
Страница 192: ...Page H 36 GNS 400W Series Installation Manual Rev G 190 00356 08 Figure H 23 King Serial Remote DME Tuning Interconnect...
Страница 193: ...GNS 400W Series Installation Manual Page H 37 190 00356 08 Rev G Figure H 24 Parallel 2 of 5 DME Tuning Interconnect...
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Страница 204: ...Page H 48 GNS 400W Series Installation Manual Rev G 190 00356 08 Figure H 36 Garmin GAD 42 Interconnect...
Страница 205: ...GNS 400W Series Installation Manual Page H 49 190 00356 08 Rev G Figure H 37 Garmin GDU 620 Interconnect...
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