TM 1-1510-224-10
TAKE-OFF DISTANCE - FLAPS APPROACH
ASSOCIATED CONDITIONS:
POWER.........................................STATIC TAKE-OFF POWER SET
........................................................BEFORE BRAKE RELEASE.
VR. V50........................................AS SCHEDULED IN TABLE
........................................................OF TAKE-OFF SPEEDS.
LANDING GEAR..........................RETRACTED AFTER LIFT-OFF
RUNWAY ......................................PAVED. DRY SURFACE
EXAMPLE:
FAT ........................................................15C
FIELD PRESSURE ALTITUDE.........3499 FT
WEIGHT................................................16,000 LBS
RUNWAY GRADIENT........................1.9%
DN
HEADWIND COMPONENT...............10 KTS
GROUND ROLL ..................................2909 FT
TOTAL DISTANCE OVER
50-FT OBSTACLE...............................3886 FT
Figure 7-26. Take-off Distance Over 50 Foot Obstacle - Flaps Approach
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