TM 1-1510-223-10
MAXIMUM TAKE-OFF WEIGHT
PERMITTED BY ENROUTE CLIMB REQUIREMENTS
ASSOCIATED CONDITIONS:
POWER ..................................................MAXIMUM CONTINUOUS
INOPERATIVE PROPELLER .................FEATHERED
FLAPS ....................................................UP
LANDING GEAR.....................................UP
EXAMPLE:
FIELD PRESSURE ALTITUDE ..............................3499 FT
FAT.........................................................................15C
TAKE-OFF WEIGHT ..............................................16200 LBS
NOTES: 1. THIS GRAPH PROVIDES THE ONE-ENGINE-INOPERATIVE CLIMB PERFORMANCE WEIGHT LIMIT
(WHICH IS FOR RATE-OF-CLIMB CAPABILITIES AT 5000 FT PRESSURE ALTITUDE) AS A
FUNCTION OF FIELD PRESSURE ALTITUDE AND TEMPERATURE. REFER TO THE "CLIMB ONE
ENGINE INOPERATIVE" GRAPH FOR ACTUAL CLIMB CAPABILITIES APPLICABLE TO THE
PARTICULAR TEMPERATURE AND ALTITUDE BEING CONSIDERED.
2. FOR OPERATION WITH ICE VANES EXTENDED, ADD 5500 FEET TO FIELD PRESSURE ALTITUDE
BEFORE ENTERING GRAPH.
Figure 7-15. Maximum Take-off Weight Permitted by Enroute Climb Requirements IR
7-26 Change 2
