MIL-PRF-87100A(USAF)
2.2 Government documents
2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a
part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents will
be those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and
supplement thereto, cited in the solicitation (see 6.2).
SPECIFICATIONS
FEDERAL
A-A-51057
Steel, Straight
QQ-A-250/4
Aluminum Alloy 2024, Plate and Sheet
DEPARTMENT OF DEFENSE
MIL-S-13282
Silver and Silver Alloys
FEDERAL
FED-STD-313
Material Safety Data Sheets, Preparation and Submission of
FED-STD-791
Lubricants, Liquid Fuels, and Related Products; Methods of Testing
MILITARY
MIL-STD-290
Packaging of Petroleum and Related Products
TECHNICAL ORDERS
TO 33A6-7-24-11
Operations and Maintenance Instructions for Fluid Analysis
Spectrometer, Type A/E35U-3A
(Unless otherwise indicated, copies of the above specifications, standards, and handbooks are available from the
Defense Automated Printing Service, 700 Robbins Avenue, Bldg 4D, Philadelphia PA 19111-5094.)
2.2.2 Other Government documents, drawings, and publications. The following other Government documents,
drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified
the issues are those cited in the solicitation.
CODE OF FEDERAL REGULATIONS (CFR)
DEPARTMENT OF LABOR
29 CFR 1910.1200
Occupational Safety and Health Standards Hazard Communications
(Application for copies should be addressed to the Superintendent of Documents, Government Printing Office,
Washington DC 20402.)
2.3 Non-government publications. The following documents form a part of this document to the extent specified
herein. Unless otherwise specified, the issues of the documents which are DOD adopted are those listed in the issue
of the DoDISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the
DoDISS are the issues of the documents cited in the solicitation (see 6.2).
SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)
AEROSPACE MATERIAL SPECIFICATIONS (AMS)
AMS 4908
Titanium Alloy Sheet and Strip - 8Mn Annealed, 110,000 psi (760 MPa)
Yield Strength (DoD adopted)
AMS 5544
Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 57Ni -19.5Cr -
13.5Co - 4.2Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B, Consumable Electrode
or Vacuum Induction Melted, Annealed (DoD adopted)
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