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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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