MIL-DTL-60515C
4.6.5 Protective finish. Test procedures for protective finish shall be in accordance with the
applicable specification referenced on the applicable drawing.
4.6.6 Residual magnetism. The assembly shall be tested for excessive residual magnetism using
an approved compass in an area free of local magnetic effects by placing the assembly 5 inches from the
end and at the same height as the compass, in a north-south horizontal position (cap end at south) with the
compass set in an east-west heading. The assembly shall be moved at a speed no greater than 10 feet per
minute past the compass for its entire length, rotated 90 degrees in the horizontal position about its
longitudinal axis and moved slowly back past the compass. This procedure shall be repeated for each 90
degree rotation of the assembly for four full passes.
4.7 Inspection of packaging. The sampling and inspection of the packaging, packing, and container
marking shall be in accordance with the requirements of section 5.
5. PACKAGING
5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the
contract or order (see 6.2). When packaging of materiel is to be performed by DoD or in-house contractor
personnel, these personnel need to contact the responsible packaging activity to ascertain packaging
requirements. Packaging requirements are maintained by the Inventory Control Point's packaging
activities within the Military Service or Defense Agency, or within the military service's system
commands. Packaging data retrieval is available from the managing Military Department's or Defense
Agency's automated packaging files, CD-ROM products, or by contacting the responsible packaging
activity.
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. Since the initiator was developed specifically for use in
military aircraft it has no commercail application.
6.2 Acquisition requirements. Acquisition documents should specify the following:
a. Title, number, and date of this specification
b. Issue of DODISS to be cited in the solicitation and, if required, the specific issue of individual
documents referenced (see 2.1.1 and 2.1.2)
c. If first article inspection is required (see 3.1 and 6.3)
d. The responsible inspection activity (see 4.1)
e. Any special inspection requirements (see 4.3)
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