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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

OPERATION

POWERING UP THE GNS 530

The GNS 530´s power and COM volume are controlled using the COM power/volume

knob (5) at the top left corner of the unit. Rotating it clockwise will turn unit power on

and increase the COM radio volume. After turning the unit on, a 'welcome page' will be

displayed while the unit performs a self test, followed by a 'land data page'.

The database confirmation page will appear next, which shows the current database

information on the NavData card (with the valid operating dates, cycle number and

database type indicated). The database is updated every 28 days, and must be

current for approved instrument approach operations. Information on database

subscriptions is available inside your GNS 530 package.

To acknowledge the database information, press the ENT-key.

Once the database has been acknowledged, the instrument panel self-test page will

appear. To ensure that the GNS 530 and any connected instruments are working

properly, check for the following indications on your HSI and external annunciators:

•

Course deviation - half left /

no flag

•

TO/FROM flag - TO

The instrument panel self-test page indicates the currently selected OBS course, fuel

capacity ('CAP'), fuel on board ('FOB') and fuel flow ('FF'). The fuel capacity, fuel on

board and fuel flow are entered manually.

Doc. # 6.01.01-E

Rev. 0

01 Dec 2001

•

All external annunciators - on

•

Glideslope - half up / no flag

Supplement A21

GNS 530

Page 9 - A21 - 17