Garmin GNS 430 파일럿 운영 핸드북 - 페이지 10

{카테고리_이름} Garmin GNS 430에 대한 파일럿 운영 핸드북을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 430 10 페이지. Friendlypanels gps for microsoft fs9 & fsx
Garmin GNS 430에 대해서도 마찬가지입니다: 파일럿 매뉴얼 (22 페이지), 사용 설명서 (6 페이지), 파일럿 매뉴얼 부록 (27 페이지), 파일럿 매뉴얼 부록 (4 페이지), 빠른 참조 (23 페이지), 파일럿 매뉴얼 부록 (22 페이지), 사양 (2 페이지), 빠른 참조 (17 페이지), 운영 매뉴얼 (27 페이지)

Section 9

Supplements

side of the GNS 430 front panel. Frequency tuning is accomplished by

rotating the large and small concentric knobs to select a standby

frequency and then transferring the frequency to the active window.

The COM frequency display window is at the upper left corner of the

GNS 430 display. Auto-tuning can be accomplished by entering a

frequency from a menu. The COM 1 antenna is located above the

cabin on the airplane centerline. 28 VDC for transceiver operating is

controlled through the Avionics Master Switch and supplied through

the 7.5-amp COM1 circuit breaker on the Avionics Essential Bus.

TERRAIN Interface*

*TERRAIN functionality is a standard feature found in GNS

430 units with main software version 5.01 or above and valid

terrain and obstacle databases installed.

Garmin TERRAIN is a terrain awareness system incorporated into

GNS 430 units to increase situational awareness and aid in reducing

controlled flight into terrain. The TERRAIN function displays altitudes

of terrain and obstructions relative to the aircraft's altitude and are

advisory in nature only. Individual obstructions may be shown if

available in the database, however, not all obstructions may be

available in the database and data may be inaccurate. TERRAIN

information should be used as an aid to visual acquisition and not use

to navigate or maneuver to avoid terrain.

For for a more detailed description of the TERRAIN function, refer to

the Garmin GNS 430 Pilot's Guide and Reference, P/N 190-00140-00,

Revision H dated May 2006 or later revision.

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• Note •

Cirrus Design

SR20

P/N 11934-S22

Revision 2: 08-15-07