MIL-DTL-81014B
4.5.2.11 Low temperature test. The hook shall be tested in accordance with MIL-STD-810,
Method 502.4, Procedure II. The hook temperature shall be stabilized at 65 °F. The hook shall
be tested through one cycle of each of the tests specified in 4.5.2.1.
4.5.2.12 Salt spray test. The hook shall be tested in accordance with ASTM-B117 for a
period of 48 hours. The hook shall be tested through one cycle of each of the tests specified in
4.5.2.1 without removal of any salt deposits resulting from the test.
4.5.2.13 Sand test. The hook shall be tested in accordance with MIL-STD-810,
Method 510.4, Procedure II, except that the sand velocity through the test chamber shall be
maintained at 2,500 ± 500 feet per minute through the first half of the test and between 100 and
500 feet per minute through the second half of the test. Upon completion of the test, the hook
shall be inspected for deterioration and shall be operated through one cycle of each the tests
specified in 4.5.2.1.
4.5.2.14 Altitude test. The hook shall be tested in accordance with MIL-STD-810, Method
500.4, Procedure I, at an altitude of 20,000 feet and an ambient temperature of 65 °F. The hook
shall be operated through one cycle of each test condition specified in 4.5.2.1 after the test.
4.5.2.15 Water immersion tests. The hook shall be tested by immersion in sea water or
water of equivalent salinity, to a depth of five feet for 15 minutes, and after being withdrawn the
hook shall be operated through one cycle of each test condition specified in 4.5.2.1. A fresh
water washdown is permissible after completion of operations.
4.5.2.16 Fungus test. The hook shall be tested in accordance with MIL-STD-810, Method
508.5 for 28 days. Upon completion of this test, the hook shall be operated through one cycle of
each test condition specified in 4.5.2.1.
4.5.2.17 Shock test. The hook shall be tested in accordance with MIL-STD-810, Method
516.5, Procedure I, functional test for flight equipment. Three shocks in each direction shall be
made for a total of 18 shocks. Upon completion of this test, a load shall be attached and dropped
so as to induce a shock loading equivalent to 20,000 pounds at 3 g's. The hook shall successfully
sustain ten such shocks. Upon completion of this test the hook shall be operated through one
cycle of each test condition specified in 4.5.2.1.
5. PACKAGING
5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in
the contract or order (see 6.2). When actual packaging of materiel is to be performed by DoD
personnel, these personnel need to contact the responsible packaging activity to ascertain requisite
packaging requirements. Packaging requirements are maintained by the Inventory Control Point's
packaging activity within the Military Department or Defense Agency, or within the Military
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