TM 1-1510-254-CL
EMERGENCY PROCEDURES
ENGINE MALFUNCTION
ENGINE MALFUNCTION BEFORE
V1 (ABORT)
2. Braking -- As required.
3. Reverse -- As required.
IF INSUFFICIENT RUNWAY REMAINS FOR STOP-
PING:
4. CONDITION levers -- FUEL CUTOFF.
5. FUEL FIREWALL SHUTOFF VALVES
-- CLOSED.
6. MASTER SWITCH -- OFF.
ENGINE MALFUNCTION AFTER V1
1. POWER -- Maximum allowable.
2. LDG GEAR CONTROL -- UP (positive
rate of climb conirmed).
3. Propeller -- Verify feathered. If propeller
does not autofeather, perform manual
feather.
4. FLAPS (after Vyse) -- UP.
5. TCAS -- Set TA.
6. Engine Cleanup checklist -- Perform.
ENGINE MALFUNCTION DURING
FLIGHT
1. Autopilot/yaw damper -- Disengage.
2. POWER -- As required.
3. Affected engine -- Identify.
4. PROP lever (affected engine) --
FEATHER.
5. TCAS -- Set TA.
E-1