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MIL-M-70821 (AR)
4.5.2.4 Part modification.  Each mount shall be examined to
determine compliance with requirements specified in 3.3.3.  And
evidence of parts being altered or hand-fit during assembly beyond
the provisions of 3.3.3, shall be cause for rejection of the mount.
4.5.2.5 Air gas and accumulator system.  To determine
conformance to 3.3.4, the system shall be examined for
cleanliness, air and moisture.  Failure to comply with 3.3.4 shall
be cause for rejection of the mount.
4.5.2.6 Cylinder pressure.  To determine compliance with
3.3.5, the cylinders of each mount shall be pressurized in
accordance with drawing requirements and inspected for damage,
permanent deformation or leakage.  Pressures shall be measured
with Government-approved gages.  Failure to comply with 3.3.5
shall be cause for rejection of the mount.
4.5.2.7 Lubrication.  Inspection and tests for lubicants
shall be in accordance with MIL-G-10924.  Failure to comply with
MIL-G-10924 shall be cause for rejection of the mount.
4.5.2.8 Gas.  Inspection and tests for nitrogen shall be in
accordance with BB-N-441.  Failure to comply with BB-N-441 shall
be cause for rejection of the mount.
4.5.2.9 Visual examination.  Each mount shall be examined for
the following defects.  One or more defects shall be cause for
rejection of the mount.
Incorrect assembly or missing parts.
a.
b.
Discontinuity or absence of protective finish.
c , Incorrect or missing marking.
d.
Color of paint not as specified.
Workmanship not as specified.
e.
4.5.2.10 Packaging and packing.  Examination of packaging and
packing shall be in accordance with Packaging Data Sheet P1291086O
for M182.
4.6 Testinq.
4.6.1 "Mechanical gymnstication.  Each mount shall have a
mechanical gymnastication in accordance with test method 4.7.3 to
determine compliance with requirements specified in 3.4.1.
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