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MIL-T-60694B
moved slowly back past the compass. This procedure shall be repeated for each 90 degree rotation of the
assembly for four full passes.
4.5.7 Shear pin strength. After application of protective finish, the pin shall be subjected to the shear
pin strength test to determine compliance with 3.5. 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 8858440 and 8858441. Level B shall be in
accordance with Drawings 8858441 and 9217560.
5.2 Air Force packaging. Air Force packaging shall be in accordance with TPO 00-607-0314.
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)
d. Any special instruction requirements (see 4.2)
e. Level of packing and marking (see 5.1)
6.3 Definitions.
6.3.1 Mechanical failure. Mechanical failure is any deformation or breakage of a part, the occurrence
of which is other than a design function.
6.3.2 Exterior components. Remanufactured exterior components are: firing pin housing, reservoir
assembly, body, ring nut, rod end, and piston rod.
15

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