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3.5.5 ENGINE FAILURE DURING TAKE-OFF
a) Engine failure during ground roll
-abort take-off
1.
POWER lever ........................ IDLE / BOTH
2.
Rudder ............................. maintain directional control
3.
Brakes ............................. asrequired
CAUTION
If sufficient time is remaining, the risk of fire in the event of a collision with obstacles can be reduced as follows:
4.
ENGINE MASTER .................... both OFF
5.
FUEL SELECTOR .................... both OFF
6.
ELECT. MASTER ..................... OFF
END OF CHECKLIST
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 3 - 29
b) Engine Failure after lift off
If landing gear is still extended and the remaining runway / surface is adequate:
-abort the take-off & land straight ahead, turning to avoid obstacles
If the remaining runway / surface is inadequate:
-decide whether to abort or to continue the take-off
Continued take-off:
WARNING
A continued take-off is not recommended if the steady rate of climb according to Section 5.3.9 - ONE ENGINE INOPERATIVE CLIMB performance is less than 3.3 %. Under certain combinations of ambient conditions, such as turbulence, crosswinds and wind shear as well as pilot skill the resulting climb performance may nevertheless be insufficient to continue the take-off successfully. Therefore a continued take-off with a failed engine has to be avoided if at all possible.
1.
Power lever .......................... MAX
2.
Rudder ............................. maintain directional control
3.
Airspeed ............................ vYSE = 82 KIAS / as required
4.
Landing Gear ........................ UP to achieve a positive ROC
5.
FLAPS.............................. check UP
CONTINUED
Page 3 - 30 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
' 6. Inoperative engine .................... secure according to
3.5.3 - ENGINE SECURING (FEATHERING) PROCEDURE
Continue according to Section 3.5.9 - FLIGHT WITH ONE ENGINE INOPERATIVE and land as soon as possible according to 3.5.7 - LANDING WITH ONE ENGINE INOPERATIVE.
If the situation allows, you may climb to a safe altitude for troubleshooting (3.5.2 - ENGINE TROUBLESHOOTING) in order to try to restore engine power.
END OF CHECKLIST 3.5.6 ENGINE FAILURES IN FLIGHT
Doc. No. 7.01.05-E Rev. 5 15-Nov-2007 Page 3 - 31
(a) Engine Failure during Initial Climb at Airspeeds below vmCA = 68 KIAS
WARNING
As the climb is a flight condition which is associated with high power settings, airspeeds lower than vmCA = 68 KIAS should be avoided as a sudden engine failure can lead to loss of control. In this case it is very important to reduce the asymmetry in thrust to regain directional control.
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本文链接地址：钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 2(18)
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