MIL-T-466928
to shipment and those defective items shall be removed from the production lot. Film interpretation of the radiographs shall verify the presence and correct positioning of the following parts:
a. 0-ring, MS28775-009
b. Pin, Firing, P/N 8596416
c. Retainer, Cartridge, P/N 10521325
d. Cartridge, Impulse, M146, P/N 8596426 e. Pin, Shear, P/N 8596419
f. Piston, P/N 8596418
g. Setscrew, P/N 10521326 h. Spring, P/N 8596424
i. Ring, Sealing (2 each), P/N 10520993 j. Ring, Sealing, P/N 10520973
k. Nut, Lock, P/N 10520981 l. Head, P/N 10521324
m. Cylinder, P/N 10521323 n. Clevis, P/N 8596421
o. Pin, Locking, P/N 8596422 p. Setscrew, P/N 10543068-9
q. Pin, Shear Unlock, P/N 8596423 r. Packing, MS28775-001
s. Piston, Floating, P/N 8596417 t. Packing, MS28775-021
u. Setscrew, P/N 10543068-1
v. Plug, Protective, MIL-C-5501/10-F5
4.3.4 Functional.
4.3.4.1 Ballistics. The test sample shall be rigidly supported so that the entire thrust is bornebythethruster mountingpoints. Thesamplesshall betested within10 minutesafter removal from the temperature conditioning chamber. When this time limit is exceeded, the sample units shall be reconditioned at the original temperatures.
4.3.4.2 Temperature conditioning. Each assembled thruster shall be conditioned for not less than 4 hours nor greater than 24 hours. When reconditioning thrusters at!65EF, all condensation shall be removed from the exterior surfaces before returning the thruster to the conditioning chamber.
4.4 Inspection of packaging. The sampling and inspection of the packaging, packing, and container marking shall be in accordance with section 5.
5. PACKAGING
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