TM 1-1510-223-10
TAKE-OFF DISTANCE - FLAPS APPROACH
ASSOCIATED CONDITIONS:
POWER ..........................STATIC TAKE-OFF POWER SET
........................................BEFORE BRAKE RELEASE.
VR, V 50 ............................AS SCHEDULED IN TABLE
........................................OF TAKE-OFF SPEEDS.
LANDING GEAR ............RETRACTED AFTER LIFT-OFF
RUNWAY .......................PAVED. DRY SURFACE
NOTES:
1.
FOR
OPERATION
WITH
ICE
VANES
EXTENDED, INCREASE TOTAL DISTANCE
BY 9%.
2. CONSULT "MAXIMUM TAKE-OFF WEIGHT -
FLAPS APPROACH - AS LIMITED BY TIRE
SPEED"
GRAPH
FOR
POSSIBLE
TAILWIND PROHIBITIONS.
EXAMPLE:
FAT ................................................................15C
FIELD PRESSURE ALTITUDE ......................3499 FT
WEIGHT .........................................................16,000 LBS
RUNWAY GRADIENT ....................................1.9% DN
HEADWIND COMPONENT.............................10 KTS
TOTAL DISTANCE OVER
50-FT OBSTACLE .........................................3892FT
* CA Increase total distance by 5%.
Figure 7-28. Take-off Distance Over 50 Foot Obstacle - Flaps Approach IR
Change 2 7-39
