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MIL-M-63995 (AR)
4.5.2.4 Part modification.  Each mount shall be examined to
determine compliance with requirements specified in 3.3.3.  Any
evidence of parts being altered or hand-fitted durinq assemblv
beyond the provisions of 3.3.3,  shall be cause for rejection of
the mount.
4.5.2.5 Gas and accumulation system.  To determine
conformance to 3.3.4, the system shall be examind 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 meassured
with Government-approved gages.  Failure to comply with 3.3.5
shall be cause for rejection of the mount.
4.5.2.7 Pistons, rods and nuts or collars.  To determine
compliance with 3.3.6, the pistons, piston rods, and nuts or
collars of each mount shall-be inspected for permanent set or
damaged threads after being pull-stressed by Government approved
equipment.  Failure to comply with 3.3.6 shall be cause for
rejection of the mount.
4.5.2.8 Lubrication.  Inspection and tests for lubricants
shall be in accordance with MIL-G-10924.  Failure to comply with
3~1L-G-10924 shall be cause for rejection of the mount.
4.5.2.9 Gas.  Inspection and tests  for nitrogen shall be in
accordance with BB-N-411.  Failure to comply with BB-N-411 shall
be cause for rejection of the mount.
4.5.2.10 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
Incorrect or missing marking
c*
d.
Color of paint not as specified
Workmanship not as specified.
e.
4.5.2.11 Packaqinq and packing.  Examination of packaging and
packing shall be in accordance with Packaging Data Sheet P10891937
or P12253872 as applicable.
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