TM 1-1510-223-10
NET TAKE-OFF FLIGHT PATH - THIRD SEGMENT
ONE ENGINE INOPERATIVE
VENR = 130 KNOTS (ALL WEIGHTS)
ASSOCIATED CONDITIONS:
POWER ......................................MAXIMUM CONTINUOUS
INOPERATIVE PROPELLER .....FEATHERED
LANDING GEAR ........................UP
FLAPS ........................................UP
CLIMB SPEED ...........................VENR
NOTE:
FOR
OPERATION
WITH
ICE
VANES
EXTENDED.
DECREASE
NET
CLIMB
GRADIENT BY 1.3 PERCENTAGE POINTS.
EXAMPLE:
FAT ........................................................15C
FIELD PRESSURE ALTITUDE ..............3499 FT
WEIGHT .................................................16.000 LBS
HEADWIND COMPONENT ....................10 KTS
NET CLIMB GRADIENT..........................1.47%
Figure 7-36. Net Take-off Flight Path - Third Segment
Change 2 7-47
