TM 1-1510-223-10
NET TAKE-OFF FLIGHT PATH - SECOND SEGMENT - FLAPS APPROACH
ONE ENGINE INOPERATIVE
ASSOCIATED CONDITIONS:
POWER ..........................STATIC TAKE-OFF POWER SET
BEFORE BRAKE RELEASE
INOPERATIVE PROPELLER .........FEATHERED
LANDING GEAR.............................UP
CUMB SPEED ...............................V2
NOTE: FOR OPERATION WITH ICE VANES EXTENDED,
DECREASE NET CLIMB GRADIENT BY 0.9
PERCENTAGE POINT.
EXAMPLE:
FAT ........................................................15C
FIELD PRESSURE ALTITUDE ..............3499 FT
WEIGHT .................................................16,000 LBS
HEADWIND COMPONENT ....................10 KTS
NET CLIMB GRADIENT .........................1.94%
* CA Decrease net climb gradient by 0.1 percentage points.
Figure 7-32. Net Take-off Flight Path - Second Segment - Flaps Approach IR
Change 2 7-43
