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カーナビゲーションシステム Garmin GNS 530のPDF マニュアルをオンラインで閲覧またはダウンロードできます。Garmin GNS 530 35 ページ。 Supplement a21 to the airplane flight manual da 40 diamond com/nav/gps
Garmin GNS 530 にも：パイロット・マニュアル (22 ページ), 取扱説明書 (6 ページ), パイロット・マニュアル補遺 (27 ページ), パイロット・マニュアル補遺 (4 ページ), クイック・リファレンス (16 ページ), パンフレット (1 ページ), クイック・リファレンス (23 ページ), パイロット・マニュアル補遺 (22 ページ), インストレーション・マニュアル (14 ページ)

DA 40 AFM

In some areas datums other than WGS-84 may be used. If

the GNS 530 is authorized for use by the appropriate

Airworthiness authority, the required geodetic datum must

be set in the GNS 530 prior to its use for navigation.

The accuracy of the data base information is only assured if it is used before the

end of the effectivity period. Use of out of date data base information is done

entirely at the user´s own risk.

3. EMERGENCY PROCEDURES

If GNS 530 navigation information is not available or invalid, utilize remaining

operational navigation equipment as required.

If 'RAIM POSITION WARNING' message is displayed the system will flag and no

longer provide GPS based navigational guidance. The crew should revert to the

GNS 530 VOR/ILS receiver or an alternate means of navigation other than the

GNS 530's GPS Receiver.

If 'RAIM IS NOT AVAILABLE' message is displayed in the en route, terminal, or

initial approach phase of flight, continue to navigate using the GPS equipment or

revert to an alternate means of navigation other than the GNS 530's GPS

receiver appropriate to the route and phase of flight. When continuing to use

GPS navigation, position must be verified every 15 minutes using the GNS 530's

VOR/ILS receiver or another IFR-approved navigation system.

Doc. # 6.01.01-E

NOTE

Rev. 0

01 Dec 2001

Supplement A21

GNS 530

Page 9 - A21 - 8