TM 1-1510-224-10
NET TAKE-OFF FLIGHT PATH - FIRST SEGMENT - FLAPS UP
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
-0.16 %
Figure 7A-20. Net Take-off Flight Path - First Segment - Flaps Up
7A-37
