TM 55-1510-222-CL
EMERGENCY PROCEDURES
NOTE
The urgency of certain emergencies requires immediate and instinctive action by the pilot.
The most important single consideration is aircraft control. All procedures are subordinate to
this requirement.
ENGINE MALFUNCTION
ENGINE MALFUNCTION PRIOR TO OR AT V1, (ABORT)
1.
Power levers - GROUND FINE.
2.
Braking - As required.
3.
Reverse thrust - As required.
(4).
Condition levers - FUEL CUTOFF.
(5).
Fire pull handles - Pull.
(6).
Master switch - OFF.
ENGINE FAILURE AFTER V1
1.
Power - Maximum allowable.
2.
Gear - UP (two positive climb indications).
3.
Propeller - Verify feathered.
4.
Flaps - UP after V enr (121 KIAS).
5.
Landing lights - OFF.
6.
Engine cleanup - Perform.
7.
Land as soon as practicable.
ENGINE MALFUNCTION DURING FLIGHT
1.
Autopilot/Yaw Damp - Disengage.
2.
Power - As required.
3.
Dead engine - Identify.
E-1
