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ENGINE FAILURE IN FLIGHT
DOUBLE ENGINE FAILURE

Operator and Crewmember Checklist for C-26E Aircraft
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TM 1-1510-253-CL
NOTE
Compute single engine landing dis-
tance by adding 66% to two engine
landing distance.
Autopilot may be engaged after com-
pletion of memory items.
ENGINE FAILURE FINAL APPROACH
1. POWER -- SET As Required
2. LANDING GEAR -- RECHECK DOWN
IN FLIGHT RELIGHT
NOTE
If reason for inadvertent flameout is
known and relight will not aggravate
conditions use steps below for relight
procedures.
Engine relight should be expected to
occur automatically if Ignition Switch is
in AUTO and fuel is available at igniters.
1. POWER Lever -- SET Approx. 1/4"
Forward of Flight Idle
2. SPEED Lever -- SET Approx. 97%
RPM
3. Airspeed -- Maintain 100 - 180 KIAS
4. START Button -- PRESS (Until Ign, Fuel
Flow & EGT Rise)
5. EGT -- Monitor During Start (770C
Max)
6. RPM -- CHECK Stabilized
7. "SRL OFF" Light -- CONFIRM
EXTINGUISHED
8. POWER -- SET As Required
E-4


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