Garmin Cessna Caravan G1000 비행기 비행 매뉴얼 보충 자료 - 페이지 25
{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
Emergency Gear Extension (RED) Handle
Oil Temperature
CHT
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Parking Brake
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TAKEOFF
Proper engine operation should be checked early in the takeoff roll. Any
significant indication of rough or sluggish engine response is reason to
discontinue takeoff. When takeoff must be made over a gravel surface,
it is important that the throttle be applied SLOWLY. This will allow the
aircraft to start rolling before high RPM is developed, and gravel or loose
material will be blown back from the propeller area instead of being
pulled into it.
TAKEOFF (NORMAL)
Power
. . . . . . . . . . . . . . . . . . . . . . . . . .
Mixture
. . . . . . . . . . . . .
Annunciator
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Engine Instruments
Lift Off/Climb Speed
Landing Gear
. . . . . . . .
Wing Flaps
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TAKEOFF (HIGH ALTITUDE)
For maximum engine power, the mixture should be adjusted during the
initial takeoff roll to the top of the white arc on the EGT. The power in-
crease is significant above 3000 feet and this procedure should always
be employed for field elevations greater than 5000 feet above sea level.
If maximum performance takeoffs are desired obtain full pow-
er before brake release. Use lift off and climb speed as speci-
fied in Section V.
CLIMB
If applicable, use noise abatement procedures as required.
See Section V, for rate of climb graph.
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
. . . . . . . . . . . . . . . . . . . . . . . . . .
Check and set at top of the white arc on EGT
. . . . . . . . . . . . . . . .
.
As specified in SECTION V (Takeoff Distance)
RETRACT IN CLIMB after clearing obstacles
NOTE:
NOTE:
AFM SUPPLEMENT
. .
DOWN and LATCHED
75_F(24_C) minimum
250_F(121_C) minimum
FULL THROTTLE (2500 RPM)
CHECK for proper indications
RELEASE
CHECK
UP
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FAA APPROVED