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アビオニクス・ディスプレイ Garmin GTN 635のPDF マニュアルの補足をオンラインで閲覧またはダウンロードできます。Garmin GTN 635 31 ページ。 Gps/sbas navigation system as installed in cessna 172r
Garmin GTN 635 にも：アクティベーション手順 (46 ページ), ユーザーマニュアル (20 ページ), 正誤表 (4 ページ), ユーザーマニュアル (22 ページ), フライトマニュアル (49 ページ), パイロット・マニュアル (28 ページ)

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

Street

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

MARCH 18, 2011

NAVIGATION SYSTEM

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