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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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