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Missile Hydraulic Pumps and Their Power SourcesAIR560D (Current)
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
Aluminum Alloy Castings, 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti (A206.0-T4), Solution Heat Treated and Naturally AgedAMS4236E (Current)3/25/2026
This specification covers an aluminum alloy in the form of sand, investment, permanent mold, and composite mold castings with nominal wall thicknesses of up to 1.0 inch (25.4 mm), inclusive (see 8.8).
AMS D Nonferrous Alloys Committee
Sheet, Polychlorotrifluoroethylene (PCTFE), Molded, UnplasticizedAMS3646E (Current)3/25/2026
This specification covers a 100% homopolymer of polychlorotrifluoroethylene (PCTFE) in the form of molded sheet 0.250 inch (6.35 mm) and under in nominal thickness.
AMS P Polymeric Materials Committee
Aluminum Alloy, Welding Wire, 7.0Si - 0.52Mg (357)AMS4246G (Current)3/25/2026
This specification covers an aluminum alloy in the form of welding wire.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Rolled or Cold-Finished, Bars, Rods, and Wire, and Flash-Welded Rings, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061; -T6, -T651)AMS4117M (Current)3/25/2026
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire and of flash-welded rings and stock for flash-welded rings.
AMS D Nonferrous Alloys Committee
RIVET - TUBULAR, COUNTERSUNK, AS7228AS3228B (Current)3/24/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, TEE HEAD – CHAMFERED, AMS5708 (UNS N07001), 165 KSI MIN UTS, .1900-32UNJF-3AAS3232C (Current)3/24/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .4375-20 UNJF-3AAS3118B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .2500-28 UNJF-3A X .1900-32 UNJF-3AAS3139C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .3125-24 UNJF-3A X .2500-28 UNJF-3AAS3140C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .375-24 UNJF-3AAS3117B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, CRES (UNS S66286), .5000-20 UNJF-3AAS3119B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, UNS S66286, .5625-18 UNJF-3AAS3120B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .3750-24 UNJF-3A X .3125-24 UNJF-3AAS3141C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
Engine Rotation and Cylinder NumberingJ824_202206 (Current)6/29/2022
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry.
Engine Power Test Code Committee
Cotter Pins, Steel 18cr 10.5ni 0.40ti, Corrosion and Heat Resistant SteelAMS7211G (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
PLASTIC ROD AND BAR, POLYIMIDE Unfilled, MoldedAMS3644/1 (Current)9/1/1994
This specification covers an unfilled polyimide plastic in the form of molded rod and bar.
AMS P Polymeric Materials Committee
Urea Compound, PowderAMS1731B (Current)3/1/1994
This specification has been designated as "SUPERSEDED" by the Aerospace Materials Division, SAE, as of May 17, 1993. The requirements of this specification are embodied in the latest issue of AMS 1431.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Primer, Adhesive, Corrosion-Inhibiting -55 to +95°C (-67 to +203°F)AMS3106A (Current)12/1/1994
AMS CE Elastomers Committee
Gaskets, Type Xx Engine Accessory Drive Corrosion Resistant Steelscreen Reinforced Controlled PerforAMS7283C (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Bolts and Screws Steel, Low Alloy Heat Resistant 195,000 Psi Hardened & Tempered, Roll ThreadedAMS7459E (Current)10/1/1993
AMS E Carbon and Low Alloy Steels Committee
Bolts and Screws Roll ThreadedAMS7473F (Current)10/1/1993
AMS E Carbon and Low Alloy Steels Committee
Rods, Sheets, and Molded Shapes, Polychlorotrifluoroethylene (PCTFE), UnplasticizedAMS3650E (Current)3/16/2026
This specification covers a 100% homopolymer of polychlorotrifluoroethylene (PCTFE) in the form of rods, sheets, and molded shapes.
AMS P Polymeric Materials Committee
Plating, Chromium, Hard DepositAMS2406R (Current)12/3/2025
This specification covers the requirements for electrodeposited hard chromium plate.
AMS B Finishes Processes and Fluids Committee
Bolts and Screws, Corrosion and Heat Resistant, Nickel Alloy, Upset Headed, Heat Treated, Roll Threaded, 2050°F (1120°C) Solution, 1650°F (900°C) Precipitation Heat TreatedAMS7469D (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy 6061, Plate and SheetAMSQQA250/11A (Current)7/15/2008
This specification covers the specific requirements for 6061 aluminum alloy plate and sheet.
AMS D Nonferrous Alloys Committee
Tolerances, Metric, Copper and Copper Alloy WireMAM2224D (Current)1/16/2008
This specification covers established metric manufacturing tolerances applicable to copper and copper alloy wire ordered to metric (SI) dimensions. These tolerances apply to all conditions, unless otherwise noted.
AMS D Nonferrous Alloys Committee
Coating Material, Fluorocarbon (FKM) Elastomeric, Anti-Static Topcoating, WhiteAMS3138/5C (Current)4/14/2009
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3138D. Cancelled specifications are available from SAE.
AMS G8 Aerospace Organic Coatings Committee
Quality Assurance, Sampling and Testing, Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded RingsMAM2355E (Current)1/3/2008
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of wrought aluminum alloy and wrought magnesium alloy mill products, except forging stock, including rolled, forged, and flash welded rings, specified in metric (SI) units. Definitions of rings, as applicable to this specification, are presented in 8.3 (Definitions).
AMS D Nonferrous Alloys Committee
Coating Material, Fluorocarbon (FKM) Elastomeric, Anti-Static Topcoating, Color MatchedAMS3138/6C (Current)4/14/2009
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3138D. Cancelled specifications are available from SAE.
AMS G8 Aerospace Organic Coatings Committee
Steel Bars, Forgings, Tubing, and Rings 1.3Mn - 1.5Si - 0.30Cr - 1.8Ni - 0.40Mo (0.23 - 0.28C)AMS6418H (Current)9/1/2000
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging and flash welded rings.
AMS E Carbon and Low Alloy Steels Committee
Steel, Corrosion and Heat Resistant, Covered Welding Electrodes 25cr 20niAMS5695G (Current)6/1/2000
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes.
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Particulate Reinforced Extrusions 6092/Sic/25p - T6p Solution Heat Treated, Quenched, and Precipitation Heat TreatedAMS4265A (Current)7/1/2000
This specification covers particulate reinforced aluminum metal matrix composites in the form of extruded shapes. These extrusions have been used typically for structural applications requiring moderate static strength and high elastic modulus, but usage is not limited to such applications.
AMS D Nonferrous Alloys Committee
Stepping Surface Test Method for Heavy VehiclesJ3351_202602 (Current)2/12/2026
Define the test equipment and test procedures for measuring slip resistance for stepping, walking, and standing surfaces commonly used on heavy vehicles.
Truck and Bus Human Factors Committee
Test Standard for Vulcanized Rubber and Thermoplastic Elastomer Determination of Compressive Stress Relaxation (CSR) ResponseJ2979_202603 (Current)3/13/2026
The scope of this document is to define a test method for performing the Compression Stress Relaxation (CSR) Test with the Automotive Standard (ASD) or HP CSR Jig using the appropriate test fixtures, configurations, and procedures. This standard defines the equipment needed, guidelines for running the test, and the format for generating the results and analyzing the data.
Committee on Automotive Rubber Specs
Air Brake Actuator Test Procedure, Truck-Tractor, Bus, and TrailersJ1469_202603 (Current)3/13/2026
This SAE Recommended Practice provides procedures and methods for testing service, spring applied parking, and combination brake actuators with respect to durability, function, and environmental performance. A minimum of six test units designated A, B, C, D, E, and F are to be used to perform all tests per 1.1 and 1.2.
Truck and Bus Brake Actuator Committee
Considerations and Guidelines to Extract Knowledge from Long-Term Archival DataAIR8479 (Current)2/24/2026
The scope of this document is to provide considerations, guidelines, and best practices for extracting knowledge from long-term archival data. The document is intended to cover the data generated across all life cycle stages of an aircraft starting from concept to disposal. This document does not standardize the process, nor does it allow regulatory authorities to recognize the document as an acceptable means of compliance. It is only a guideline document to discover, capture, store, retrieve, process, and consume knowledge.
G-31 Digital Transactions for Aerospace
HOSE ASSEMBLY, LINED SILICONE, 125 PSI, FLARELESS, POTABLE WATER, 45° TO 45°AS4472D (Current)2/23/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, LINED SILICONE, 125 PSI, FLARELESS, POTABLE WATER, 90° TO 90°AS4474D (Current)2/23/2026
SCOPE IS UNAVAILABLE.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Billets and Preforms, 6al 4v, Premium Quality, Powder-Metallurgy ProductAMS4996B (Current)7/23/2002
This specification covers a premium-quality, titanium alloy powder-metallurgy product in the form of billets and preforms for forgings.
AMS G Titanium and Refractory Metals Committee
Bars and Forgings, 14cr 4.0mo (1.00-1.10c)AMS5619A (Current)7/1/2000
Primarily for parts requiring resistance to both corrosion and wear with hardness retained during exposure to temperatures up to 600 F (316 C).
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy, 5.4al 1.4cr 1.3fe 1.25mo Annealed 135,000 Psi YieldAMS4929 (Current)12/16/2002
AMS G Titanium and Refractory Metals Committee
Steel Tubing, Seamless, 0.50cr 0.55ni 0.20mo (0.28 0.33c)AMS6535H (Current)7/1/2001
Primarily for use where welding and moderate tensile properties are required. May be used where minimum tensile strength up to 180,000 psi (1240 MPa) is required for wall thicknesses up to 0.125 in. (3 mm) and proportionately lower strength is required in heavier thicknesses. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of 19 April 1988. It is recommended, therefore, that this specification not be specified for new designs.
AMS E Carbon and Low Alloy Steels Committee
Castings, Alloy-Investment, 61ni 16cr 8.5co 1.8mo 2.6w 0.8cb 3.4ti 1.8ta 3.4al 0.010b 0.06zr (0.03-0.08c), Vacuum Melted, Vacuum Cast, as CastAMS5409A (Current)8/21/2002
This specification covers a corrosion and heat resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
ALUMINUM ALLOY WELDING WIRE 7.0Si - 0.30Mg (A356.0)AMS4188/4 (Current)12/16/2002
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
AMS D Nonferrous Alloys Committee
Aqueous Cleaners for Cleaning Prior to Application of Sealing CompoundsAMS3168 (Current)11/19/2001
This specification covers liquid aqueous cleaners.
AMS G9 Aerospace Sealing Committee
Centrifugal Steel Castings Chromium Molybdenum 38-45AMS5345 (Current)12/16/2002
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Welding WireAMS4188A (Current)5/1/1995
Primarily for use as filler metal for gas-metal-arc and gas-tungsten-arc welding, including repair welding, of aluminum alloy castings. Where casting service conditions require good corrosion resistance, maximum strength, and homogeneity, filler metal should be of the same alloy as the casting.
AMS D Nonferrous Alloys Committee
EPOXY PRIMER PLATING ElectrodepositionAMS2443 (Current)10/1/1995
This specification covers the engineering requirements for electrodeposition of AMS 3109 epoxy primer on aluminum alloy surfaces and the properties of the deposit.
AMS P Polymeric Materials Committee
STUDS, CORROSION AND HEAT RESISTANT STEEL Heat Treated, Roll ThreadedAMS7481B (Current)5/1/1995
AMS F Corrosion and Heat Resistant Alloys Committee
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