TM 1-1510-224-10
TAKE-OFF DISTANCE - FLAPS APPROACH
ASSOCIATED CONDITIONS:
EXAMPLE
POWER .......................STATIC TAKE-OFF POWER SET
FAT.........................................................15C
BEFORE BRAKE RELEASE.
FIELD PRESSURE ALTITUDE .................3499 FT
VR. V50.......................AS SCHEDULED IN TABLE
WEIGHT..................................................16,000 LB
OF TAKE-OF SPEEDS.
RUNWAY GRADIENT..............................1.9%. DN
LANDING GEAR...........RETRACTED AFTER LIFT-OFF
HEADWIND COMPONENT ......................10 KTS
RUNWAY.....................PAVED, DRY SURFACE
GROUND ROLL ......................................2960 FT
TOTAL DIS TANCE OVER
50-FT OBSTACLE ................................4150 FT
Figure 7A-26. Take-off Distance Over 50 Foot Obstacle - Flaps Approach
7A-44
