TM 55-1510-221-10
MAXIMUM TAKEOFF WEIGHT PERMITTED BY ENROUTE
ASSOCIATED CONDITIONS:
CLIMB REQUIREMENT
EXAMPLE:
POWER ....................... MAXIMUM CONTINUOUS
INOPERATIVE PROPELLERS ........ FEATHERED
LANDING GEAR ...................... UP
FLAPS . . . . . . . . . . . . . . . . . . . . . . . 0%
MAXIMUM TAKEOFF
WEIGHT
NOTE:
ONE-ENGINE-INOPERATIVE PERFORMANCE WEIGHT LIMIT IS FOR
RATE-OF-CLIMB CAPABILITIES AT 5000 FT PRESSURE ALTITUDE.
REFER TO THE l CLIMB - ONE ENGINE INOPERATIVE’ GRAPH
FOR ACTUAL CLIMB CAPABILITIES APPLICABLE TO THE
PARTICULAR TEMPERATURE AND ALTITUDE BEING CONSIDERED.
PRESSURE ALTITUDE . . . . . . 5233 FT
FAT . . . . . . 28°C
14.200 LBS
Figure 7-10. Maximum Takeoff Weight Permitted by Enroute Climb Requirement
7-15
