TM 1-1510-224-10
MAXIMUM TAKE-OFF WEIGHT - FLAPS UP
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-15. Maximum Take-off Weight as Limited by Tire Speed - Flaps Up
7A-31
