TM 1-1510-224-10
MAXIMUM TAKE-OFF WEIGHT - FLAPS APPROACH
TO ACHIEVE POSITIVE ONE-ENGINE-INOPERATIVE CLIMB AT LIFT-OFF
ASSOCIATED CONDITIONS:
POWER.........................................TAKEOFF
LANDING GEAR..........................DOWN
INOPERATIVE PROPELLER....FEATHERED
EXAMPLE
FIELD PRESSURE ALTITUDE.........3499 FT
FAT ........................................................15C
TAKE-OFF WEIGHT...........................16,500 LBS
Figure 7-23. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Approach
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