Garmin GTN 625 Manual Supplement - Page 8
Browse online or download pdf Manual Supplement for Car Navigation system Garmin GTN 625. Garmin GTN 625 31 pages. Gps/sbas navigation system as installed in cessna 172r
Also for Garmin GTN 625: Activation Instructions (46 pages), User Manual (20 pages), Errata (4 pages), User Manual (22 pages), Flight Manual (49 pages), Pilot's Manual (28 pages)
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GARMIN Ltd. or its Subsidiaries, c/o
Garmin International 1200 E. 151
Olathe, KS 66062 USA
The Garmin GNSS navigation system, as installed in this aircraft, 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 [one or more] TSO-C146c Class 3 approved Garmin GTN Navigation
Systems. The Garmin GNSS navigation system as installed in this aircraft
complies with the equipment requirements for P-RNAV and B-RNAV/RNAV 5
operations in accordance with AC 90-96A CHG 1 and JAA TGL-10 Rev 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 WGS-84 reference system.
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.
1.3
Electronic Flight Bag
The GTN as installed in this aircraft supports approval of AC 120-76A Hardware
Class 3, Software Type C Electronic Flight Bag (EFB) electronic aeronautical
chart applications when using current FliteChart or ChartView data. Additional
operational approvals may be required. For operations under 14 CFR Part 91,
Garmin suggests that a secondary or back up source of aeronautical information
necessary for the flight be available to the pilot in the airplane. The secondary or
backup information may be either traditional paper-based material or displayed
electronically. If the source of aeronautical information is in electronic format,
operators must determine non-interference with the GTN system and existing
aircraft systems for all flight phases.
190-01007-A2 Rev. 1
FAA APPROVED DATE: _________________
AIRPLANE FLIGHT MANUAL SUPPLEMENT or
st
Street
SUPPLEMENTAL AIRPLANE FLIGHT MANUAL
for STC SA02019SE-D GARMIN GTN
MARCH 18, 2011
NAVIGATION SYSTEM
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