MIL-S-6451E
3.11 Identification of product. A nameplate permanently and legibly marked
in accordance with MIL-STD-130 shall be securely attached to each section
(upper and lower) of the shield. The following special marking shall be
included:
FOR USE ON TYPE
AIRCRAFT (OR MISSILES).
3.12 Workmanship. The shields, including all parts and accessories, shall
be constructed and finished in a thoroughly workmanlike manner. Particular
attention shall be given to strength of welds, neatness and thoroughness of
painting, riveting, machine-screw assemblies, molding, forming, fit, function,
et cetera. Parts, assemblies and end items shall be free of defects such as,
but not limited to, burrs, cracks or crazing, fatigue, loose components, and
rough or sharp edges.
3.12.1 Dimensional tolerances. Dimensions and tolerances not specified
shall be as close as is consistent with the best shop practices. Where dimen-
sions and tolerances may affect the interchangeability, operation, or perform-
ance of the shield, they shall be held or limited accordingly.
3.12.2 Class 1 shields shall be fabricated by drawing or bending and welding,
except where ease of servicing of the shields requires that a removable panel
construction be used or where the applicable stresses dictate the use of
strong aluminum alloy that does not provide a good weld; for such parts,
riveting or bolting may be used.
3.12.3 Molding, forming, pressing, et cetera, of class 2 shields shall be
accomplished with the use of accurate molds, presses, and forms. Shields
shall be fabricated for ease of installation and removal and to provide a
press fit in the required orifice.
3.12.4 Screw assemblies. Assembly screws and bolts shall be tight; restraint
items such as lock washers, lock nuts, safety wiring, cotter pins, epoxy, et
cetera, shall be used as necessary.
3.12.5 Riveting. Riveting operations shall be performed to insure that the
rivets are tight and satisfactorily headed.
3.12.6 Cleaning. The shields shall be thoroughly cleaned of loose, spattered,
or excess weld, metal chips, or other foreign material after final assembly.
Burrs and sharp edges, as well as resin flash that may crumble, shall be
removed.
4. QUALITY ASSURANCE PROVISIONS
4.1 Responsibility for inspection. Unless otherwise specified in the contract,
the contractor is responsible for the performance of all inspection requirements
as specified herein. Except as otherwise specified in the contract, the con-
tractor may use his own or any other facilities suitable for the performance
of the inspection requirements specified herein, unless disapproved by the
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