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.............................16,500 LBS
Figure 7A-14. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Up
7A-30
