TM 1-1510-223-10
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
NOTE:
FOR
OPERATION
WITH
ICE
VANES
EXTENDED,
DECREASE
NET
CLIMB
GRADIENT BY 1.0 PERCENTAGE POINT.
EXAMPLE:
FAT ........................................................15C
FIELD PRESSURE ALTITUDE ..............3499 FT
WEIGHT .................................................16,000 LBS
HEADWIND COMPONENT ....................10 KTS
NET CLIMB GRADIENT .........................-0.32 %
* CA Decrease net climb gradient by 0.1 percentage points.
Figure 7-22. Net Take-off Flight Path - First Segment - Flaps Up IR
Change 2 7-33
