TM 55-1510-221-10
TAKEOFF WEIGHT - FLAPS 0%
TO ACHIEVE POSITIVE ONE-ENGINE-INOPERATIVE CLIMB AT LIFT-OFF
ASSOCIATED CONDITIONS:
POWER
.
.
.
TAKEOFF
FLAPS
0%
EXAMPLE:
PRESSURE ALTITUDE
FAT
. . . . 5233 FT
...... 28°C
LANDING GEAR ................ DOWN
INOPERATIVE PROPELLER
FEATHERED
TAKEOFF WEIGHT ........... 13,480 LBS
....
Figure 7-11. Takeoff Weight - Flaps 0%, To Achieve Positive One-Engine Climb at Lift-Off
7-16
