TM 1-1510-223-10
NET TAKE-OFF FLIGHT PATH - SECOND SEGMENT - FLAPS UP
ONE ENGINE INOPERATIVE
ASSOCIATED CONDITIONS:
POWER ..........................STATIC TAKE-OFF POWER SET
BEFORE BRAKE RELEASE
INOPERATIVE PROPELLER .....FEATHERED
LANDING GEAR ........................UP
CLIMB SPEED ...........................V2
NOTE: FOR OPERATION WITH ICE VANES EXTENDED,
DECREASE NET CLIMB GRADIENT BY 1.1
PERCENTAGE POINTS.
EXAMPLE:
FAT ........................................................15C
FIELD PRESSURE ALTITUDE ..............3499 FT
WEIGHT .................................................16,000 LBS
HEADWIND COMPONENT ....................10 KTS
NET CLIMB GRADIENT .........................1.97%
* CA Decrease net climb gradient by 0.1 percentage points.
Figure 7-23. Net Take-off Flight Path - Second Segment - Flaps Up IR
7-34 Change 2
