MIL-C-8605B
TABLE III
Vibration Test
4.6.10 Burst Pressu re. The burst pressure test procedure shall be similar to the proof
pressure procedure, except that the pressure shall be 180 psi. There shall be no failure or
evidence of distortion of the cap as a result of this test.
4.6.11 Locking Torque. The cap shall be locked onto the adapter. Prior to locking the
height of the rocker arm shall be 0.150 inch or greater. After locking, the rocker arm shall
be flush with the cap top. Apply an 80 in.-lbs. torque to the cap in a counterclockwise
direction. The cap shall not unlock nor sustain damage.
4.6.12 Disassembly and Inspection. The cap shall be disassembled and inspected.
There shall be no evidence of excessive deterioration, wear or corrosion.
5.
PREPARATION
FOR
DELIVERY
5.1 Preservation and Interior Packaging. The cap shall be preserved, packaged, and
packed in accordance with MIL-STD-794.
5.2 Marking of Shipments. Interior packages and exterior shipping containers shall be
marked in accordance with MIL-STD-129.
6. NOTES
6.1 Intended Use. The caps covered by this specification are intended for use in
sealing aircraft hydrocarbon fuel-tank pressure servicing adapters.
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