MIL-I-60513A
d. Firing pin housing P/N 8595408 e. Cartridge retainer P/N 8593313 f. CAP P/N 8595404 g. 3-Ball MS19060-3
h. Spring, initiator P/N 8595406 i. Pin, initiator P/N 8595403 j. 0-ring MS28775-214 k. Pin, safety P/N 8595405
4.3.5 Functional.
4.3.5.1 Ballistics. The test sample shall be rigidly supported in the fixture. The sample shallbetestedwithin5minutesafterremovalfromthetemperatureconditioningchamber. When this time limit is exceeded, the sample units shall be reconditioned. Required pressure readings shall be taken as specified in 3.8.1.
4.3.5.2 Temperature conditioning. Each assembled initiator shall be conditioned for not less than 4 hours nor greater than 24 hours. When reconditioning initiators at!65EF, all condensation shall be removed from the exterior surfaces before returning the initiator 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
5.1 Packing and marking. Packing and marking shall be Level A or B, as specified by the contractingactivity(see6.2). LevelAshallbeinaccordancewithDrawings8796826and8796827. Level B shall be in accordance with Drawings 8796826 and 9216824.
5.1.1 Lot numbers. Lot numbers shall be in accordance with MIL-STD-1168.
5.2 Air Force packaging. Air Force packaging shall be in accordance with TP0 00-845-1058.
6. NOTES
(This section contains information of a general or explanatory nature that may be helpful but is not mandatory.)
6.1 Intended use. The initiator assembly is used in conjunction with other propellant actuated devices in Aircrew Emergency Escape Systems.
6.2 Acquisition requirements. Acquisition documents must specify the following:
a. Title, number, and revision letter of this specification
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