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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)

Supplement A21

DA 40 AFM

GNS 530

5. PERFORMANCE

No change.

Upon removal or installation of the GNS 530 the change of empty mass and

corresponding center of gravity of the airplane must be recorded according to Chapter

6 of the Airplane Flight Manual.

7.14 AVIONICS

The GNS 530 System is a fully integrated, panel mounted instrument, which contains

a VHF Communications Transceiver, a VOR/ILS receiver, and a Global Positioning

System (GPS) Navigation computer. The system consists of a GPS antenna, GPS

Receiver, VHF VOR/LOC/GS antenna, VOR/ILS receiver, VHF COMM antenna and a

VHF Communications Transceiver. The primary function of the VHF Communication

portion of the equipment is to facilitate communication with Air Traffic Control. The

primary function of the VOR/ILS Receiver portion of the equipment is to receive and

demodulate VOR, Localizer, and Glide Slope signals. The primary function of the GPS

portion of the system is to acquire signals from the GPS system satellites, recover

orbital data, make range and Doppler measurements, and process this information in

real-time to obtain the user's position, velocity, and time.

Doc. # 6.01.01-E

Rev. 0

01 Dec 2001

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