Garmin GNS 530 파일럿 매뉴얼 부록 - 페이지 13

{카테고리_이름} Garmin GNS 530에 대한 파일럿 매뉴얼 부록을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 530 27 페이지. Supplement a21 to the airplane flight manual da 40 diamond com/nav/gps
Garmin GNS 530에 대해서도 마찬가지입니다: 파일럿 매뉴얼 (22 페이지), 사용 설명서 (6 페이지), 파일럿 매뉴얼 부록 (4 페이지), 빠른 참조 (16 페이지), 브로셔 (1 페이지), 빠른 참조 (23 페이지), 파일럿 매뉴얼 부록 (22 페이지), 설치 매뉴얼 (14 페이지), 매뉴얼 (35 페이지)

To begin tracking intruder aircraft

1. Turn the cursor on and highlight STBY.

2. Turn the small right knob to select OPER.

3. Press ENT to conﬁ rm operating mode and begin tracking intruder aircraft.

The FAILED message occurs when the system detects an error that prohibits further trafﬁ c

display operation as long as this message stays on the screen.

User-initiated Test

A user-initiated test can only be performed when in standby or failed mode.

In addition to the power-up test, the SKYWATCH performs a continuous self-test. This continuous

self-test is performed several times per minute. A user-initiated test of the SKYWATCH Interface can also

be performed.

To perform a user-initiated test:

1. Turn the small right knob to select the Trafﬁ c Page.

2. From the Trafﬁ c Page, press MENU to display the Page Menu.

3. Turn the small right knob to select 'Self Test?' and press ENT.

See the SKYWATCH Pilot' s Guide for information on voice announcements.

The unit must be in operating mode for trafﬁ c to be displayed. The ability to switch out of standby

into operating mode on the ground is especially useful for scanning the airspace around the airport before

takeoff.

Getting Started

Section 3

SKYWATCH Interface

Main Page Sequence

Operating Mode is conﬁ rmed by the display of

'OPER' in the upper right-hand corner of the

Trafﬁ c Page.