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![]() 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
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