TM 1-1510-224-10
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
CLIMB SPEED........................................V2
EXAMPLE:
FAT.................................................................15C
FIELD PRESSURE ALTITUDE.......................3499 FT
WEIGHT..........................................................16,000 LBS
HEADWIND COMPONENT.............................10 KTS
NET CLIMB GRADIENT..................................2.32%
Figure 7A-30. Net Take-off Flight Path - Second Segment - Flaps Approach
7A-48
