TM 1-1510-224-10
NET TAKE-OFF FLIGHT PATH - THIRD SEGMENT
ONE ENGINE INOPERATIVE
ASSOCIATED CONDITIONS:
POWER...................................................MAXIMUM CONTINUOUS
INOPERATIVE PROPELLER..................FEATHERED
LANDING GEAR.....................................UP
FLAPS.....................................................UP
CLIMB SPEED........................................VENR
EXAMPLE:
FAT.................................................................15C
FIELD PRESSURE ALTITUDE.......................3499 FT
WEIGHT..........................................................16,000 LBS
HEADWIND COMPONENT.............................10 KTS
NET CLIMB GRADIENT..................................2.07%
Figure 7A-34. Net Take-off Flight Path - Third Segment
7A-52
