Typical Loads

TM 55-2320-289-14

30 January 1987

4-6. Typical Loads

The following tiedown diagrams (figs 4-1 through 4-3) and tiedown data (tables 4-1 through 4-3) provide a

guide for securing the CUCVs aboard US Air Force aircraft. Final tiedown procedures will be at the discre-

tion of the Air Force loadmaster. The figures show a typical tiedown pattern of a representative CUCV for

each aircraft. The tables give the type and capacity of tiedown devices required, location points on the

vehicles, and aircraft fittings to which the devices are secured.

4-2