TM 1-1510-224-10
MAXIMUM TAKE-OFF WEIGHT - FLAPS UP
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...........................1 6,500 LE
Figure 7-14. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Up
7-30
