TM 1-1510-224-10
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 16,500 LBS
Figure 7A-24. Maximum Take-off Weight as Limited by Tire Speed - Flaps Approach
7A-41
