TM 1-1510-224-10
MAXIMUM TAKE-OFF WEIGHT - FLAPS APPROACH
TO ACHIEVE POSITIVE ONE-ENGlNE-INOPERATIVE CLIMB AT LIFT-OFF
ASSOCIATED CONDITIONS:
EXAMPLE:
POWER ....................................... TAKEOFF
FIELD PRESSURE ALTITUDE .................3499 FT
LANDING GEAR........................... DOWN
FAT.........................................................15C
INOPERATIVE PROPELLER......... FEATHERED
TAKE-OFF WEIGHT................................16,500 LBS
Figure 7A-23. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Approach
7A-40
