TM 1-1510-224-10
ACCELERATE-STOP - FLAPS APPROACH
ASSOCIATED CONDITIONS:
EXAMPLE:
POWER .......................STATIC TAKE-OFF POWER SET
FAT......................................................15C
BEFORE BRAKE RELEASE.
FIELD PRESSURE ALTITUDE ..............3499 FT
AUTOFEATHER
ARMED
WEIGHT...............................................16,000 LBS
V1 ..............................AS SCHEDULED IN TABLE
RUNWAY GRADIENT...........................1.9% DN
OF TAKE-OFF SPEEDS.
HEADWIND COMPONENT . .................10 KTS
POWER LEVERS .........GROUND FINE AT V1
ACCELERATE-STOP DISTANCE..........5047 FT
BRAKING.....................MAXIMUM WITHOUT SLIDING TIRES
RUNWAY.....................PAVED, DRY SURFACE
Figure 7A-27. Accelerate Stop - Flaps Approach
7A-45
