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TM 1-<strong>1520</strong>-<strong>240</strong>-<strong>10</strong><br />

8-3-6. Aerodynamic Loads.<br />

Aerodynamic loads, su<strong>ch</strong> as tow targets, drones, light<br />

aircraft, aircraft parts, wings and tail sections have certain<br />

inherent dangers because of their aerodynamic lift<br />

capabilities. There<strong>for</strong>e , the lift capabilities of external<br />

loads must be eliminated be<strong>for</strong>e they are lifted. Airspeed<br />

and bank angles will be governed by the reaction of the<br />

load to the airspeed. Drogue <strong>ch</strong>utes shall also be used<br />

to streamline the load. However, the <strong>ch</strong>ute must be atta<strong>ch</strong>ed<br />

to the load with a swivel fitting.<br />

8-3-2<br />

8-3-7. Multi-Hook Loads.<br />

Handling <strong>ch</strong>aracteristics are improved when loads are<br />

slung using two-point (<strong>for</strong>ward and aft hook) sling suspension.<br />

Load motion is substantially reduced. Potentially<br />

unstable loads are directionally restrained by two-point<br />

suspension; airspeed capability is increased above the<br />

airspeed <strong>for</strong> single-point suspension. When low density<br />

high-drag cargo is carried, the risk of single hook failure<br />

in two-point suspension is reduced by the addition of a<br />

safety sling from the center hook to the <strong>for</strong>ward load<br />

atta<strong>ch</strong>ment point. The multi-hook configuration also enables<br />

the carrying of three independent loads within the<br />

CG limit.

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