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|  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.
O-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
shall be tested within 5 minutes after removal from the temperature conditioning chamber. 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 65 F, 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
contracting activity (see 6.2). Level A shall be in accordance with Drawings 8796826 and 8796827.
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 TPO 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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