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MIL-L-48063A(MI)
4.3.2 Examination.  The examinations listed in the following
subparagraphs shall be performed on inspection lots (see 4.3.1) of the
components or assemblies designated in the applicable paragraph headings.
Inspection for critical defects (and major defects, when so specified)
shall be 100 percent.  Sampling plans for major and minor defects shall
be in accordance with MIL-STD-105 except that continuous sampling plans
in accordance with MIL-STD-1235 may be used if approved by the Government.
Instead of applying the AQL's designated herein to the groups of major
and minor defects listed, the contractor may elect to apply AQL's to
individual defects using an AQL of 0.40 percent for each major defect
and an AQL of 0.65 percent for each minor defect. When this method
is elected, it shall be applied to all of the major and minor defects
listed in the applicable subparagraph of this section, except where 100
percent inspection is specified, and be documented as part of the
contractor's inspection system.  Equipment necessary for the
performance of the inspections listed shall be in accordance with 4.3.4.
4.3.2.1 Tube, Launcher (see dwg. 356AS144 covering a detail of dwg.
356AS100).
Defects
Method of Inspection
Categories
None defined.
Critical:
Major:
AQL 1.00 percent
Length overall . . . . . . . . . . . . . . . . . . . . . . . . . . . Gage
101.
102.
Inside diameter max.
(both ends) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Gage
Location of aft mounting
103.
hold for detent . . . . . . . . . . . . . . . . . . . . . . . . . . Gage
Location of forward mounting
104.
hole for rocket stop plate . . . . . . . . . . . Gage
Location of middle mounting
105.
hold for contact assembly . . . . . . . . . . . . Gage
Wall thickness . . . . . . . . . . . . . . . . . . Gage
106.
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