Garmin GNS 530AW 파일럿 매뉴얼 부록 - 페이지 42
{카테고리_이름} Garmin GNS 530AW에 대한 파일럿 매뉴얼 부록을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 530AW 50 페이지. For continued airworthiness bell 206b
Garmin GNS 530AW에 대해서도 마찬가지입니다: 파일럿 매뉴얼 부록 (24 페이지), 파일럿 매뉴얼 부록 (24 페이지), 보충 설명서 (12 페이지), 빠른 참조 (23 페이지), 빠른 참조 (25 페이지), 사용 설명서 (23 페이지)
페이지 인쇄
Part Three: Section 3
TAWS Alerts
WARNING—Estimated potential impact in approximately 30
seconds after pop-up alert and annunciation. RTC/ITI warning
alerts are accompanied by the aural message "Terrain, Terrain;
Pull Up, Pull Up" or "Terrain Ahead, Pull Up; Terrain Ahead,
Pull Up". Similarly, a "Obstacle, Obstacle; Pull Up, Pull Up"
or "Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up" alert is
also provided.
Phase of Flight
En Route
Terminal
Approach
Departure
Minimum TERRAIN Clearance Values for RTC/ITI Alerts
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38
Level Flight
Descending
700 ft.
500 ft.
350 ft.
300 ft.
150 ft.
100 ft.
100 ft.
100 ft.
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During the final approach phase of flight, RTC/ITI
alerts are automatically inhibited when the aircraft is
below 200 feet AGL while within 0.5 NM of the approach
runway or is below 125 feet AGL while within 1.0 NM of
the runway.
Premature Descent Alerting (PDA)
The TERRAIN system issues a Premature Descent
Alert (PDA) when the system detects that the aircraft
is significantly below the normal approach path to
a runway. PDA begins when the aircraft is within 15
NM of the destination airport. PDA ends when the
aircraft is either 0.5 NM from the runway threshold
or is below an altitude of 125 feet AGL while within
1.0 NM of the threshold.
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