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|  MIL-T-60201C
203 Number of units contained incorrect
Visual
204 Marking missing, incorrect, or illegible
Visual
205 Tape incomplete
Visual
4.2.3 Inspection testing. The following tests shall be performed in accordance with 4.3.
4.2.3.1 Breakaway torque.
4.2.3.1.1 Retainer guide and sleeve. Each retainer guide and sleeve subassembly shall be
subjected to a breakaway torque. Failure of any subassembly to comply with the requirements of
column C, table I in 3.3 shall be cause for rejection of the subassembly.
4.2.3.1.2 Head and retainer guide. Each head and retainer guide subassembly shall be
subjected to a breakaway torque. Failure of any subassembly to comply with the requirements of
column C, table I in 3.3 shall be cause for rejection of the subassembly.
4.2.3.1.3 Head and body. Each head and body assembly shall be subjected to a breakaway torque.
Failure of any assembly to comply with the requirements of column C, table I in 3.3 shall be cause
for rejection of the assembly.
4.2.3.2 Residual magnetism. Each assembly shall be subjected to the test for excessive
residual magnetism as specified in 4.3.2. Failure of any unit to comply with 3.5 shall be cause
for rejection of the assembly.
4.2.3.3 Functional tests. The following tests shall be performed by the Government.
4.2.3.3.1 Ballistics. Twenty-one units shall be tested to determine compliance with 3.7.
The units shall be temperature conditioned as provided in table II and 4.3.4.2. Failure of any
unit to comply with 3.7.1 through 3.7.6 shall be cause for rejection of the lot.
TABLE II. Conditioning temperature.
Sample size
Method
Temperature ( F)
7
Load (see 3.7.1)
65 to 70
7
Load (see 3.7.1)
65 to 75
7
Load (see 3.7.1)
195 to 205
4.2.3.3.2 Retest. There shall be no retests.
4.2.3.3.3 Test failure. If a test failure is attributable to an assignable cause, excluding
the test thruster, the original test results shall be discarded and that test reconducted.
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