TM 1-1510-253-CL
ENGINE FAILURE TAKEOFF
CONTINUED
If engine failure is accompanied by LEFT
ESS bus failure ensure landing gear con-
trol power switch is transferred to right
essential bus. Failure to comply could
result in personnel injury or damage to
equipment.
1. POWER -- SET MAX ALLOWABLE
2. LANDING GEAR -- UP
3. ENGINE STOP & FEATHER -- PULL
4. FLAPS (V2 + 5 KIAS and 500' Minimum)
-- UP
5. AIRSPEED -- VYSE
6. WATER INJECTION Switch -- SET As
Required
7. POWER -- SET As Required
8. TRIM -- SET As Required
O 9. CMWS -- SELECT ARM
10. Engine Cleanup - Failed Engine
a. FUEL SHUT OFF Switch -- CLOSED
b. HYDRAULIC SHUT OFF Switch --
CLOSED
c. FUEL BOOST PUMP Switch -- OFF
d. GENERATOR Switch -- OFF
e. BLEED AIR Switch -- OFF
f. IGNITION / ICE PROTECTION --
OFF
11. Engine Cleanup -- Operating Engine
a. BLEED AIR SWITCH -- SET As
Required
E-2