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SAE - SAE J452 - GENERAL INFORMATION - CHEMICAL COMPOSITIONS, MECHANICAL AND PHYSICAL PROPERTIES OF SAE ALUMINUM CASTING ALLOYS Organization: SAE
Date: 2003-12-01
Description: The SAE Standards for aluminum casting alloys cover a wide range of castings for general and special use, but do not include all the alloys in commercial use.
FORD ESB-M2A119-A - ALUMINUM ALLOY - SHEET, (SAE AA5182) Organization: FORD
Date: 1983-10-31
Description: SCOPE The material defined by this specification is a wrought aluminum sheet alloy (SAE AA 5182).
FORD ESB-M2A118-A - ALUMINUM ALLOY - SHEET, (SAE AA2036) Organization: FORD
Date: 1983-10-31
Description: SCOPE The material defined by this specification is a stampable, heat treatable aluminum sheet alloy (SAE AA 2036).
SAE - SAE J457 - CHEMICAL COMPOSITIONS, MECHANICAL PROPERTY LIMITS, AND DIMENSIONAL TOLERANCES OF SAE WROUGHT ALUMINUM ALLOYS Organization: SAE
Date: 1991-02-01
Description: 1. Scope--This SAE Standard for wrought aluminum alloys provides sources of chemical and mechanical property data for a considerable range of alloys with varying properties, structures, and applications.
FORD ESB-M2A125-A - ALUMINUM, EXTRUSION AND SHEET ALLOY (SAE AA 7129-T6) ***TO BE USED WITH FORD WSS-M99P1111-A*** Organization: FORD
Date: 2010-02-15
Description: The material defined by this specification can be either an extruded or sheet product, heat treatable aluminum alloy, SAE AA 7129.
NASA - NACA-TN-2324 - FATIGUE STRENGTHS OF AIRCRAFT MATERIALS AXIAL LOAD-FATIGUE TESTS ON UNNOTCHED SHEET SPECIMENS OF 24S-T3 AND 75S-T6 ALUMINUM ALLOYS AND OF SAE 4130 STEEL Organization: NASA
Date: 1951-01-01
Description: This report presents information on the axial-load fatigue behavior of unnotched specimens of each of three sheet materials: 24S-T3 and 75S-T6 aluminum alloys and normalized SAE 4130 steel. The experimental investigation of these materials included the following items: 1.
NASA - NACA-TN-3866 - FATIGUE TESTS ON NOTCHED AND UNNOTCHED SHEET SPECIMENS OF 2024-T3 AND 7075-T6 ALUMINUM ALLOYS AND OF SAE 4130 STEEL WITH SPECIAL CONSIDERATION OF LIFE RANGE FROM 2 TO 10,000 CYCLES Organization: NASA
Date: 1956-12-01
Description: Fatigue tests were performed on notched and unnotched sheet specimens made of 2024-T3 and 7075-T6 aluminum alloys and of SAE 4130 steel. The steel was tested in two conditions: normalized and heat-treated to a tensile strength of 180 ksi.
SAE - SAE AMS5047 - STEEL, SHEET AND STRIP 0.08 - 0.13C, ALUMINUM KILLED (SAE 1010) DEEP FORMING GRADE - UNS G10100 Organization: SAE
Date: 2017-02-01
Description: Form  This specification covers an aluminum-killed carbon steel in the form of sheet and strip.
NPFC - QQ-A-591 - ALUMINUM ALLOY DIE CASTINGS **USE ASTM B85, ASTM B 26, ASTM B 108, SAE AMS 4290, SAE AMS 4291,SAE J452, SAEJ453** Organization: NPFC
NPFC - QQ-A-200/2 - ALUMINUM ALLOY 2014, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED *** CNCL S/S BY SAE AMS-QQ-A-200/2, ASTM B241, ASTM B221 *** Organization: NPFC
NPFC - QQ-A-200/3 - ALUMINUM ALLOY 2024, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED *** CNCL S/S BY SAE AMS-QQ-A-200/3, ASTM B241, ASTM B221 *** Organization: NPFC
NPFC - QQ-A-200/5 - ALUMINUM ALLOY 5086, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED *** CNCL S/S BY SAE AMS-QQ-A-200/5, ASTM B241, ASTM B222 *** Organization: NPFC
NPFC - QQ-A-200/6 - ALUMINUM ALLOY 5454, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED *** CNCL S/S BY SAE AMS-QQ-A-200/6, ASTM B241, ASTM B221 *** Organization: NPFC
NPFC - QQ-A-200/9 - ALUMINUM ALLOY 6063, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED *** CNCL S/S BY SAE AMS-QQ-A-200/9, ASTM B241, ASTM B221 *** Organization: NPFC
NPFC - QQ-A-200/1 - ALUMINUM ALLOY 3003, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED *** CNCL S/S BY SAE AMS-QQ-A-200/1, ASTM B241, AND ASTM B221 *** Organization: NPFC
NPFC - QQ-A-200/4 - ALUMINUM ALLOY 5083, BAR, ROD, SHAPES, STRUCTURAL SHAPES, TUBE ANDWIRE, EXTRUDED *** CNCL S/S BY SAE AMS-QQ-A-200/4, ASTM B241, ASTM B221 *** Organization: NPFC
SAE - SAE AS1990 - ALUMINUM ALLOY TEMPERS Organization: SAE
Date: 2016-01-01
Description: The purpose of this SAE Aerospace Standard (AS) is to provide a description of the temper nomenclature system for aluminum alloys used in the aerospace industry by combining information from different sources for the benefit of the user.
SAE - SAE AMS03-25 - SULFURIC ACID ANODIZING OF ALUMINUM AND ALUMINUM ALLOYS Organization: SAE
Date: 2015-05-01
Description: This SAE Standard specifies the properties of sulphuric acid anodizing of aluminum and aluminum alloys.
SAE - SAE ARP1675 - STRUCTURAL WELDBONDING OF ALUMINUM STRUCTURES Organization: SAE
Date: 1990-10-01
Description: This SAE Aerospace Recommended Practice describes the aluminum weldbonding process for fabrication of secondary aircraft structural assemblies possessing excellent strength, fatigue life, and environmental durability.
NASA-LLIS-1423 - LESSONS LEARNED – ELEMENTS OF THE ELECTROLESS NICKEL PLATING PROCESS (SAE-AMS-C-26074) Organization: NASA
Date: 2004-04-13
Description: Abstract: During assembly of the Fluids and Combustion Facility by Northrop Grumman Information Technology at the Glenn Research Center, it was found that numerous aluminum components that were Electroless Nickel Plated to SAE-AMS-C-26074, Class 4, Grade A, by a specific supplier's subcontractor experienced peeling and flaking.

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