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| MIL-T-60696A(OS)
4.5.3 Structural strength. The thruster shall be subjected to the structural strength test in accordance
with the requirements of 3.3. The test shall be performed in a fixture in conjunction with a tensile testing
machine or other device.
4.5.4 Protective finish. Test procedures for protective finish shall be in accordance with the applicable
specification referenced on the applicable drawing.
4.5.5 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 (head 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.
4.5.6 Shear pin strength. After application of protective finish, the pin shall be subjected to the shear
pin strength test to determine compliance with 3.6. The test shall be performed in a fixture in conjunction with
a tensile testing machine.
4.6 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 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 8797633 and 8797634. Level B shall be in
accordance with Drawings 8797633 and 9235819.
5.2 Air Force packaging. Air Force packaging shall be in accordance with TPO 00-921-5048.
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 thruster 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 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. The responsible inspection activity (see 4.1)
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