TM 1-1510-224-10
NET TAKE-OFF FLIGHT PATH - FIRST SEGMENT - FLAPS APPROACH
ONE ENGINE INOPERATIVE
ASSOCIATED CONDITIONS:
POWER.........................................STATIC TAKE-OFF
POWER SET BEFORE
BRAKE RELEASE
INOPERATIVE PROPELLER....FEATHERED
LANDING GEAR..........................DOWN
CLIMB SPEED.............................V2
EXAMPLE:
FAT ........................................................15C
FIELD PRESSURE ALTITUDE.........3499 FT
WEIGHT................................................16,000 LBS
HEADWIND COMPONENT...............10 KTS
NET CLIMB GRADIENT......................0.11 %
Figure 7-29. Net Take-off Flight Path - First Segment - Flaps Approach
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