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 7-15. Maximum Take-off Weight as Limited by Tire Speed - Flaps Up
7-31
