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.....................2.33 %
VENR = 130 KNOTS (ALL WEIGHTS)
Figure 7-34. Net Take-off Flight Path - Third Segment
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