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钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 2(19)

时间:2011-10-28 13:41来源:蓝天飞行翻译 作者:admin
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1.
Rudder .............................  apply for directional control


2.  
Power levers ......................... retard as required to maintain
directional control


3.  
Airspeed ............................ vYSE = 82 KIAS / above vmCA = 68 KIAS as required

4.  
Operative engine...................... increase power as required if
directional control has been
re-established

 

Establish minimum / zero sideslip condition (approx. half ball towards good engine; 3° to 5° bank).
5.  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 Section 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
Page 3 - 32  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 


(b) Engine Failure during Initial Climb at Airspeeds above vmCA = 68 KIAS
1.
Rudder .............................  maintain directional control


2.  
Airspeed ............................ vYSE = 82 KIAS/ above vmCA = 68 KIAS as required

3.  
Operative engine ..................... increase power as required if
directional control has been
established

 

Establish minimum / zero sideslip condition (approx. half ball towards good engine; 3° to 5° bank).
4.  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 Section 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
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 3 - 33 


(c) Engine Failure during Flight
1.
Rudder .............................  maintain directional control


2.  
Airspeed ............................ as required /
above vmCA = 68 KIAS


3.  
Operative engine...................... increase power as required if
directional control has been
established

 

Establish minimum / zero sideslip condition. (approx. half ball towards good engine; 3° to 5° bank)
4.  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 Section 3.5.7 - LANDING WITH ONE ENGINE INOPERATIVE.
 
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