Garmin GNS 530W 파일럿 매뉴얼 부록 - 페이지 36

{카테고리_이름} Garmin GNS 530W에 대한 파일럿 매뉴얼 부록을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 530W 50 페이지. For continued airworthiness bell 206b
Garmin GNS 530W에 대해서도 마찬가지입니다: 파일럿 매뉴얼 부록 (24 페이지), 파일럿 매뉴얼 부록 (50 페이지), 파일럿 매뉴얼 부록 (24 페이지), 보충 설명서 (12 페이지), 빠른 참조 (23 페이지), 빠른 참조 (25 페이지), 사용 설명서 (23 페이지)

Part Three: Section 2

TAWS Operation

TAWS Manual Test

Garmin TAWS provides a manual test capability

which veriﬁes the proper operation of the aural and

visual annunciations of the system prior to a ﬂight.

"Test Terrain" selection

To manually test the TAWS system:

Select the TAWS Page and press MENU.

Select the "Test Terrain?" option.

Press ENT to conﬁrm the selection.

An aural message is played giving the test results:

• "TAWS System Test, OK" if the system passes the

test

• "TAWS System Failure" if the system fail the test

NOTE: TAWS System Testing is disabled when ground

speed exceeds 30 knots so as not to impede TAWS

alerting.

The symbols depicted below are used to represent

obstacles and potential impact points on the TAWS

Page. Note that obstacle symbols are shown on display

zoom ranges up to 10 NM.

Alerts are issued when ﬂight conditions meet

parameters that are set within TAWS software algo-

rithms that detect a potentially hazardous situation.

TAWS alerts typically employ either a CAUTION or a

WARNING alert severity level, or both. When an alert

is issued, visual annunciations are displayed. Aural

alerts are simultaneously issued.