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 7-24. Maximum Take-off Weight as Limited by Tire Speed - Flaps Approach
7-41
