TM 1-1510-223-10
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
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 CUMB GRADIENT .................................0.00 %
* CA Decrease net climb gradient by 0.1 percentage points.
Figure 7-31. Net Take-off Flight Path - First Segment - Flaps Approach IR
7-42 Change 2
