TM 1-1510-223-10
MAXIMUM TAKE-OFF WEIGHT - FLAPS APPROACH
AS LIMITED BY TIRE SPEED
EXAMPLE:
FAT ................................................................15C
FIELD PRESSURE ALTITUDE ......................3499 FT
HEADWIND COMPONENT ............................10 KTS
WEIGHT .........................................................EXCEEDS STRUCTURAL LIMIT OF 16,200 LBS
Figure 7-26. Maximum Take-off Weight as Limited by Tire Speed - Flaps Approach
Change 2 7-37
