|
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
%
Doc. No. 6.01.05-E Revision 3 26-May-2003 Page 4A - 15
4A.3.7 TAKE-OFF
Normal take-off procedure
1.
Transponder......................... ON/ALT
2.
Power lever ......................... MAX
WARNING
The proper performance of the engine at MAX should be checked early in the take-off procedure, so that the take-off can be aborted if necessary.
3.
Elevator ............................ neutral
4.
Rudder ............................. maintain direction
NOTE
In strong crosswinds steering can be augmented by use of the toe brakes. It should be noted, however, that this method increases the take-off roll, and should not generally be used.
5. Nose wheel lift-off .................... at vR = 59 KIAS (1150 kg, 2535 lb) at vR = 55 KIAS (1000 kg, 2205 lb) at vR = 49 KIAS (850 kg, 1874 lb)
% 6. Airspeed for initial climb ................ 66 KIAS
above a safe height:
7. Landing light......................... OFF
%
Doc. No. 6.01.05-E Revision 3 26-May-2003 Page 4A - 16
4A.3.8 CLIMB
Procedure for best rate of climb
1.
Flaps .............................. T/O
2.
Airspeed............................ 66 KIAS (1150 kg, 2535 lb)
% NOTE % With lower mass the air speeds can be reduced as given % below:
% 1000 kg / 2205 lb 60 KIAS % 850 kg / 1874 lb 54 KIAS % The engine temperatures must be observed then.
3.
Power lever ......................... MAX
4.
Engine instruments ................... in green range
5.
Trim ............................... as required
CAUTION
If the oil temperature and/or coolant temperature reaches the % yellow range during climb, flight should be continued with an % airspeed increased by 5 kts and power reduced by 10 % % (reduced climb rate) for better engine cooling.
%
Doc. No. 6.01.05-E Revision 3 26-May-2003 Page 4A - 17
Cruise climb
1.
Flaps .............................. UP
2.
Airspeed............................ 73 KIAS (1150 kg, 2535 lb)
% NOTE % With lower mass the air speeds can be reduced as given % below:
% 1000 kg / 2205 lb 68 KIAS % 850 kg / 1874 lb 60 KIAS % The engine temperatures must be observed then.
3.
Power lever ......................... MAX
4.
Engine instruments ................... in green range
5.
Trim ............................... as required
%
Doc. No. 6.01.05-E Revision 3 26-May-2003 Page 4A - 18
4A.3.9 CRUISE
1.
Flaps .............................. UP
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址：钻石40飞机飞行手册 DA 40 Airplane Flight Manual(33)
| 
