TM 1-1510-223-10
MAXIMUM TAKE-OFF WEIGHT - FLAPS APPROACH
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 ..............................................16,200 LBS
NOTE:
FOR OPERATION WITH ICE VANES EXTENDED, ADD
1200 FEET TO FIELD PRESSURE ALTITUDE BEFORE
ENTERING GRAPH.
* CA Reduce maximum take-off weight by 110 pounds.
Figure 7-25. Maximum Take-off Weight to Achieve Positive One Engine Inoperative Climb at Liftoff - Flaps Approach
7-36 Change 2
