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MIL-L-48063A(MI)
103. Depth of locking indents
(four places) . . . . . . . . . . . . . . . . . . . Gage
104. Length from forward end of
fairing to aft edge of indent max . . . . . Gage
105. Location of fairing clip lock
pin to indent . . . . . . . . . . . . . . . . Gage
106. Missing parts or improper
assembly . . . . . . . . . . . . . . . . . Visual
Minor:
AQL 1.50 percent
201.
Width of locking indents
(four places ) . . . . . . . . . . . . . . . . . . . . . Gage
202. Markings missing or illegible . . . . . . . . . . . Visual
203.
Evidence of poor workmanship
(see 3.7) . . . . . . . . . . . . . . . . . . . . . Visual
4.3.2.13 Launcher, Pocket, aircraft, LAU 68B/A (see dwg.
356AS164 covering a detail of dwg. 356AS1OO).
Method of Inspection
Defects
Categories
Critical:
None defined.
AQL 1.00 percent
Major:
101. Gaps or voids in skin weld . . . . . . . . . Visual
102. Gaps or voids in retaining
ring weld . . . . . . . . . . . . . . . . . . . . . . . . . . Visual
103.
Retaining ring missing,
damaged, or improperly assembled . . . . . . . . Visual
104.
Suspension lugs missing, damaged,
or improperly assembled . . . . . . . . . . Visual
105. Electrical receptacles missing,
damaged or improperly assembled . . . . . . . . . Visual
Intervalometer missing, damaged,
106.
or improperly assembled . . . . . . . . . . . .Visual
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