MIL-T-46591B
4.3.4.3 Final lock test. The test shall be performed in accordance with 3.7.5.1. The thruster fired under load condition shall be separated from the testing setup in their "as fired" condition and installed in a tensile testing machine to determine compliance with the requirements.
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 8858440 and 8858441. Level B shall be in accordance with Drawings 8858441 and 9217560.
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 00-607-0314.
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 revision letter 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. Production test activity and lot size (see 4.1 and 4.2.1)
d. Directions for shipping radiographs of entire production lot along with ballistic sample to the activity conducting production lot acceptance tests (see 4.3.3)
e. Level of packing and marking (see 5.1)
f. That the safety precaution requirements of the ``Contractor's Safety Manual for Ammunition, Explosives, and Related Dangerous Material,'' DOD 4145.26M are applicable. NOTE: When this specification is used as part of the description of work to be accomplished by a Government activity, the safety precaution requirements of ``Ammunition and Explosives Ashore,'' OP 5 are applicable.
6.3 Load firing. The expected performance of the thruster, under conditions simulating those existing in aircraft, is obtained when the thruster satisfactorily meets the conditions of the "load" firing.
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