MIL-DTL-5002E
SAE AMS2460
-
Plating, Chromium
SAE AMS2700
-
Passivation of Corrosion Resistant Steels. (DoD adopted)
SAE AMS7881
-
Tungsten Carbide-Cobalt Powder, Agglomerated and Sintered
SAE AMS7882
-
Tungsten Carbide-Cobalt Chrome Powder, Agglomerated and
Sintered
SAE AMS-C-8837
-
Coating, Cadmium (Vacuum Deposited). (DoD adopted)
SAE AMS-C-81562
-
Coatings, Cadmium, Tin-Cadmium and Zinc (Mechanically
Deposited). (DoD adopted)
SAE AMS-M-3171
-
Magnesium Alloy, Processes for Pretreatment and Prevention of
Corrosion on. (DoD adopted)
SAE AMS-P-81728
-
Plating, Tin-Lead (Electrodeposited). (DoD adopted)
SAE AMS-QQ-P-416
-
Plating, Cadmium (Electrodeposited). (DoD adopted)
(Copies of these documents are available from www.sae.org or SAE International, 400
Commonwealth Drive, Warrendale, PA 15096-0001.)
2.3 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a
conflict between the text of this document and the references cited herein, the text of this
document takes precedence. Nothing in this document, however, supersedes applicable laws and
regulations unless a specific exemption has been obtained.
3.
REQUIREMENTS
3.1 Materials and processes. Materials and processes shall conform to applicable
documents, as specified herein. Additional guidance may be found in the DoD Corrosion
Prevention and Control Planning Guidebook. Materials and processes not covered by applicable
specifications and any deviations from the requirements herein shall not be used unless approved
by the cognizant engineering organization (see 6.5).
3.2 Finishing requirements. Unless otherwise specified, all fabrication operations,
including thermal treatments and cleaning, shall have been completed prior to application of any
surface treatment, metallic coating, and/or non-metallic coating.
3.3 Surfaces. Parts, with the exception of those processed in accordance with
MIL-DTL-16232, shall conform to specified dimensions and surface roughness conditions after
final cleaning, surface treatment or coating. In the case of metals which may respond in a non-
uniform manner when metal removal is done with mechanical, chemical, electrochemical, or
electromechanical methods, inspection procedures shall be established and used to ensure each
part has a uniform surface, including freedom from pits and intergranular attack. Where etching
results, the degree found shall be demonstrated not to affect the serviceability of the parts.
3.4 Cleaning. Cleaning, prior to application of surface treatments and coatings, shall be as
specified herein. These methods shall be utilized in a manner which does not result in damage to
the metal, including freedom from pits, intergranular attack, and hydrogen embrittlement. When
specified in the contract or order, an appropriate hydrogen embrittlement relief test shall be
conducted. After cleaning, all parts shall be completely free of corrosion products, scale, paint,
4
For Parts Inquires call Parts Hangar, Inc (727) 493-0744
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business