MIL-T-46632B(08)
4.6.3 Structural strength. The thruster shall be subjected to the structural strength test in accordance with the requirements of 3.6.
4.6.4 Shear pin strength. After application of protective finish, the pin shall be subjected to the shear pin strength test to determine compliance with 3.7. The test shall be performed in a fixture in conjunction with a tensile testing machine.
4.6.5 Breakaway torque. A torque wrench capable of measuring the torque requirements specified in 3.5.2 shall be used with an appropriate adapter to determine the adequacy of the joints. The thruster body shall be secured and the torque applied to the holding ring.
4.6.6 Protective finish. Test procedures for protective finish shall be in accordance with the applicable specification referenced on the applicable drawing.
4.6.7 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 atsouth) withthecompasssetinaneast-west heading. The assembly shall be moved at a speednogreaterthan10feetperminutepastthecompassforitsentirelength,rotated90degrees 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 Packing and marking. Packing and marking shall be Level A or B, as specified by the contractingactivity(see6.2). LevelAshallbeinaccordancewithDrawings8797633and8797634. Level B shall be in accordance with Drawings 8797633 and 9235819.
5.2 Air Force packaging. Air Force packaging shall be in accordance with TP0 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. Thethruster assemblyisused inconjunctionwithother propellant actuated devices in Aircrew Emergency Escape 8ystems.
6.2 Acquisition requirements. Acquisition documents must specify the following:
a. Title, number, and date of this specification
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