Garmin Cessna Caravan G1000 비행기 비행 매뉴얼 보충 자료 - 페이지 19
{카테고리_이름} Garmin Cessna Caravan G1000에 대한 비행기 비행 매뉴얼 보충 자료을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin Cessna Caravan G1000 33 페이지. Integrated flight deck
Garmin Cessna Caravan G1000에 대해서도 마찬가지입니다: 파일럿 매뉴얼 (16 페이지), 파일럿 매뉴얼 (6 페이지), 파일럿 매뉴얼 (32 페이지), 파일럿 매뉴얼 (25 페이지), 파일럿 매뉴얼 (34 페이지), 파일럿 매뉴얼 (21 페이지), 파일럿 매뉴얼 (22 페이지)
페이지 인쇄
MOONEY
M20R
d) ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS
Loss of an engine parameter is indicated by a red X through
the data field. Erroneous information may be identified by in-
dications which do not agree with other system information.
Erroneous indications may be determined by comparing a
display with other displays and other system information.
1. Set power based on throttle lever position, engine noise and speed.
2. Monitor other indications to determine the health of the engine.
3. Use known power settings in the POH Chapter V for approximate
fuel flow values.
4. Use other system information, such as annunciator messages, fuel
quantity and flow, to safely complete the flight.
e) ERRONEOUS OR LOSS OF WARNING/CAUTION
ANNUNCIATORS
Loss of an annunciator may be indicated when engine or fuel
displays show an abnormal or emergency situation and the
annunciator is not present. An erroneous annunciator may
be identified when an annunciator appears which does not
agree with other displays or system information.
1. If an annunciator appears, treat it as if the condition exists. Refer to
the POH/AFM Emergency or Abnormal procedures or the proce-
dures contained in this AFMS.
2. If a display indicates an abnormal condition but no annunciator is
present, use other system information, such as engine displays, fuel
quantity and flow, to determine if the condition exists. If it cannot be
determined that the condition does not exist, treat the situation as if
the condition exists. Refer to the POH/AFM Emergency or Abnormal
procedures or the procedures contained in this AFMS.
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
NOTE:
NOTE:
AFM SUPPLEMENT
19 of 33
FAA APPROVED