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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
Test Procedures for Shear Strength of Automotive Brake Pads and Brake Lining AssembliesJ840_202603 (Current)3/31/2026
This SAE Recommended Practice covers equipment capabilities and the test procedure to quantify and qualify the shear strength between the friction material and backing plate or brake shoe for automotive applications. This SAE Recommended Practice is applicable to: bonded drum brake linings; integrally molded disc brake pads; disc brake pads and backing plate assemblies using mechanical retention systems (MRS); coupons from drum brake shoes or disc brake pad assemblies. The test and its results are also useful for short, semi-quantitative verification of the bonding and molding process. This Recommended Practice is applicable during product and process development, product verification and quality control. This Recommended Practice does not replicate or predict actual vehicle performance or part durability.
Brake Linings Standards Committee
FITTINGS, INSTALLATION OF FLARELESS TUBE, STRAIGHT-THREADED CONNECTORSAS33566A (Current)3/30/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLT, MACHINE - HEXAGON HEAD, PD SHANK, NICKEL ALLOY (UNS N07001), .1900-32 UNJF-3AAS3303B (Current)3/30/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, RING LOCKED, CORROSION AND HEAT RESISTANT STEEL (UNS S66286), .3125-18 UNJC X .3125-24 UNJFAS3321F (Current)3/30/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, PD SHANK, NICKEL ALLOY (UNS N07001), .2500-28 UNJF-3AAS3307B (Current)3/30/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, TEE HEAD – CHAMFERED, PD SHANK NICKEL ALLOY (UNS N07001),165 KSI MIN UTS .3750-24 UNJF-3AAS3235D (Current)3/30/2026
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
IVHM Design GuidelinesARP6407 (Current)7/29/2019
This Aerospace Recommended Practice (ARP) provides guidance for the design of an integrated vehicle health management (IVHM) capability that will extend the vehicle’s inherent design to enable health management of the platform and its components. This guidance is technology-independent; the principles are generally applicable to the majority of potential IVHM design scenarios, including “clean sheet” system design, where IVHM is considered as a primary design consideration, and the retrofit design, where existing systems are modified and leveraged with the IVHM capability. In either case, this ARP provides guidance for designing the IVHM capability from the feasibility assessment to the conceptual design analysis and to the development design phases, with considerations given to trade studies, metrics, and life cycle impacts.
HM-1 Integrated Vehicle Health Management Committee
Software Life Cycle Processes – Implementation ConsiderationsIEEEEIA12207_2 (Current)6/16/2016
This guide provides implementation consideration guidance for the normative clauses of IEEE/EIA 12207.0. The guidance is based on software industry experience with the life cycle processes presented in IEEE/EIA 12207.0.
Systems Management Council
Aerospace Series - Quality Management Systems Statistical Product Acceptance RequirementsAS9138 (Current)1/20/2018
This standard establishes requirements when implementing statistical product acceptance methods to meet defined risk requirements. This standard also establishes the minimum content required to be covered in an organization’s documented procedures that govern their application of statistical product acceptance methods. These general requirements and documented procedures apply the requirements of the 9100/9110/9120 quality management system standards, in addition to establishing requirements for retrievability, safety/critical characteristics, and quality parameters that protect the customer.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Test Cell Mass Fuel Flow Measurement Using Coriolis Flow MetersAIR6202 (Current)6/14/2017
The scope of this information report applies to the steady state measurement of direct mass fuel flow in gas turbine engine test cells. A measurement accuracy, and hence uncertainty of between ±0.1 to ±0.2% of value is believed to be achievable for liquid flow applications with some meter models/installations. Whilst capable of general transient measurement in 50 to 100 Hz region, this type of fuel meter is not capable of rapid transient measurement (in 100 to 250 Hz region). It is also not currently considered suitable for "in flight" fuel flow measurement.
EG-1E Gas Turbine Test Facilities and Equipment
Integrated Project Processes for Engineering a SystemSAE1001 (Current)10/9/2018
This standard is applicable to the engineering or the reengineering of: a Commercial or non-commercial systems, or portions thereof; b Any system, small or large, simple or complex, software-intensive or not, precedented or unprecedented; c Systems made up of hardware, software, firmware, personnel, facilities, data, materials, services, techniques, or processes (or combinations thereof); d A new system or a legacy system, or portions thereof. The requirements of this standard, or a designated subset, are intended to be applied by projects establishing policies and procedures for project implementation of the adopted process and process elements of this standard. The requirements of this standard may be tailored as follows: a Processes – Processes may be tailored to be applicable for a given type of project or system. For example, the System Utilization Processes typically don’t apply for conceptual or prototype systems in the same manner as for full-volume production systems. b
G-47 Systems Engineering
Tape, Adhesive, Pressure-Sensitive Thermal Radiation Resistant, Aluminum Foil/Glass ClothAMS3779/1B (Current)7/12/2016
This specification covers thermal radiation resistant material in the form of tape with pressure-sensitive adhesive.
AMS P Polymeric Materials Committee
Roving, Organic Fiber (Para-Aramid) Intermediate Modulus 4500 Denier (5000 Dtex), 0.9% FinishAMS3904/12B (Current)8/1/2016
This specification covers one type of organic (para-aramid) fiber in the form of roving. The product shall be formed as a number of ends, tows, or strands collected into a parallel bundle with little or no twist.
AMS P17 Polymer Matrix Composites Committee
Webbing, Textile, Tubular, Para-Aramid Intermediate Modulus 0.30 ounce per linear yard (12 g/linear m)AMS3782/2B (Current)9/10/2013
This specification covers one weight and type of para-aramid webbing.
AMS P Polymeric Materials Committee
Yarn, Organic Fiber (Para-Aramid), High Modulus 1420 (1580 d tex) Denier, 1.2% FinishAMS3901/11C (Current)7/31/2014
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
AMS P17 Polymer Matrix Composites Committee
Delegated Product Release Verification Training RequirementsAS13001A (Current)9/5/2017
This standard establishes the common requirements for training of DPRV personnel for use at all levels of the aerospace engine supply chain. This standard shall apply when an organization elects to delegate product release verification by contractual flow down to its suppliers (reference 9100 and 9110 standards) and to perform product acceptance on its behalf. It is intended that organizations specify their DPRV requirements through the application of AS9117. While the delegating organization will use the AS13001 standard as the baseline for establishing DPRV process and product training, it may include additional contractual training requirements to meet its specific needs. The DPRV training material was primarily developed for aerospace engine supply chain requirements. However, this standard may also be used in other aerospace industry sectors where a DPRV process requiring specific training can be of benefit.
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
Thread, Para-Aramid Intermediate Modulus 950 yards per pound (1915 m/kg), 150 pounds force (667 N) Breaking StrengthAMS3787/6B (Current)6/14/2016
This specification covers one weight and strength of para-aramid thread.
AMS P Polymeric Materials Committee
Aluminum Alloy 5083, Bar, Rod, Shapes, Tube, and Wire, ExtrudedAMSQQA200/4C (Current)11/20/2017
This specification covers the specific requirements for aluminum alloy 5083 bar, rod, shapes, tube, and wire produced by extrusion.
AMS D Nonferrous Alloys Committee
Plating, Brush, SilverAMS2451/13A (Current)5/24/2022
This specification covers the engineering requirements and process for brush plating of silver by electrodeposition. It shall be used, in conjunction with AMS2451, for silver deposits.
AMS B Finishes Processes and Fluids Committee
Carbon Fiber Tape and Sheet Epoxy Resin Impregnated G 150000 (1034) Tensile, 19000000 (131) Modulus, 80 (176)AMS3894/3C (Current)9/14/2016
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
Glass Non-Woven Fiber Tape and Flat Sheet Epoxy Resin Impregnated, For Hand and Machine Layup GL-III-33 - 95 (203)AMS3906/7C (Current)10/13/2016
This specification covers one type of epoxy-resin-impregnated, non-woven, glass fiber in the form of tape for hand or machine layup and of flat sheet.
AMS P17 Polymer Matrix Composites Committee
Copper-Beryllium Alloy Wire 98Cu - 1.9Be Solution Heat TreatedAMS4725F (Current)1/2/2018
This specification covers one type of copper-beryllium alloy in the form of wire.
AMS D Nonferrous Alloys Committee
Identification Bars, Wire, Mechanical Tubing, and Extrusions, Carbon and Alloy Steels and Corrosion and Heat-Resistant Steels and AlloysAMS2806D (Current)12/20/2018
This specification covers procedures for identifying bars, wire, mechanical tubing, and extrusions of carbon and alloy steels and corrosion and heat-resistant steels and alloys.
AMS B Finishes Processes and Fluids Committee
Cloth, Upholstery, Flame Resistant Novoloid/Aramid, Waffle Type WeaveAMS3856/1B (Current)6/24/2016
This specification covers one weight and one weave of novoloid/aramid cloth.
AMS P Polymeric Materials Committee
Webbing, Low Modulus Aramid 1 (25) Wide, 9000 (40,034) Breaking Strength Special WeaveAMS3798/12C (Current)4/14/2015
This specification covers one width and one breaking strength of low-modulus aramid webbing.
AMS P Polymeric Materials Committee
Test Slabs, Acrylonitrile Butadiene (NBR-L) Low Acrylonitrile, 65 - 75AMS3217/2D (Current)3/4/2020
This specification covers a standard acrylonitrile butadiene (NBR-L) rubber stock with low acrylonitrile content in the form of molded test slabs.
AMS CE Elastomers Committee
Webbing, Tubular, Low Modulus Aramid 1 (25) Wide, 4000 (17 793) Breaking StrengthAMS3799/3D (Current)7/31/2018
This specification covers one width and one breaking strength of low modulus aramid tubular webbing.
AMS P Polymeric Materials Committee
Glass Non-Woven Fiber Tape and Flat Sheet Epoxy Resin Impregnated, For Hand and Machine Layup GL-III-26 - 150 (302)AMS3906/4C (Current)10/12/2016
This specification covers one type of epoxy-resin-impregnated, non-woven, glass fiber in the form of tape for hand or machine layup and of flat sheet.
AMS P17 Polymer Matrix Composites Committee
Interleaf Carrier Material, Composite Tape Differentially Coated Paper, Unperforated 0.0035 inch (0.081 mm)AMS3898/6A (Current)4/13/2022
This specification covers a paper, coated on both sides and with different release characteristics on each side (i.e., differentially coated), supplied in the form of rolls of sheeting or reels of unperforated tape of the width specified.
AMS P17 Polymer Matrix Composites Committee
Cloth, Parachute, Meta-Aramid, Low Modulus 4.7 (159) Weight, TwillAMS3801/1C (Current)10/10/2016
This specification covers one weight and one weave of low-modulus meta-aramid cloth.
AMS P Polymeric Materials Committee
Carbon Fiber Tape and Sheet Polysulfone Resin Impregnated C PS 172 (1170) Tensile, 16 (110) Modulus, 120 (248)AMS3899/1C (Current)10/12/2016
This specification covers one type of thermoplastic, polysulfone resin-impregnated carbon fibers in the form of tape or sheet.
AMS P17 Polymer Matrix Composites Committee
Cloth, Parachute, Meta-Aramid, Low Modulus 12.0(407) Weight, Special WeaveAMS3801/3C (Current)10/11/2016
This specification covers one weight and one weave of low-modulus meta-aramid cloth.
AMS P Polymeric Materials Committee
Type 1 Virgin Polytetrafluoroethylene (PTFE) Moldings and ExtrusionsAMS3678/1C (Current)2/29/2016
This specification covers an unfilled grade of virgin polytetrafluoroethylene (PTFE) resin in the form of extruded or molded rods or tubes which are sintered after molding or, in the case of extrusions, sintered during the extrusion process.
AMS P Polymeric Materials Committee
Webbing, Tubular, Low Modulus Aramid 9/16 (14) Wide, 1400 (6228) Breaking StrengthAMS3799/1D (Current)7/31/2018
This specification covers one width and one breaking strength of low modulus aramid tubular webbing.
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
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
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
CONNECTORS, RECEPTACLE, ELECTRIC, JAM NUT MOUNTING, FRONT RELEASE, CRIMP CONTACT, AN TYPEAS34041C (Current)3/25/2026
AE-8C1 Connectors Committee
Chassis Dynamometer Test Procedure - Heavy-Duty Road VehiclesJ2177_202603 (Current)3/25/2026
This SAE Recommended Practice has been adopted by SAE to specify: a. A standard procedure for chassis dynamometer testing of heavy-duty road vehicles for the purpose of determining power delivered through the drive tires. b. A method of correcting observed power to reference test conditions. c. A method of analyzing the test data to determine if the test results are within expected power ranges.
Engine Power Test Code Committee
STUD - STRAIGHT, DRILLED, .2500-20UNS X .2500-28UNF-3AAS128363B (Current)3/20/2026
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
Battery Industrial, Lead-Acid Type, for Use in Electric Powered Ground Support EquipmentARP1817B (Current)3/25/2026
This SAE Aerospace Recommended Practice (ARP) describes an industrial battery, lead-acid type, for use in electric powered ground support equipment.
AGE-3 Aircraft Ground Support Equipment Committee
Steel Cleanliness, Premium Aircraft-Quality, Magnetic Particle Inspection ProcedureAMS2300N (Current)3/25/2026
This specification covers steel cleanliness requirements for premium aircraft-quality ferromagnetic steels, including hardenable, corrosion-resistant steels, by magnetic particle inspection methods. This specification contains sampling, sample preparation, inspection procedures, and cleanliness rating criteria (see 8.2).
AMS E Carbon and Low Alloy Steels Committee
Copper-Zinc Alloy, Laminated Sheet, 70Cu - 30Zn, Surface BondedAMS4508K (Current)3/25/2026
This specification covers a copper-zinc alloy (brass) in the form of laminated sheet with nominal thickness 0.006 to 0.125 inch (0.15 to 3.18 mm) (see 8.5).
AMS D Nonferrous Alloys Committee
Titanium Alloy Bars and Forging Stock, 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo, Duplex AnnealedAMS6905D (Current)2/18/2026
This specification covers a titanium alloy in the form of bars up through 3.000 inches (76.20 mm), inclusive, in diameter or least distance between parallel sides with a maximum cross-sectional area of 10 square inches (64.5 cm2) and forging stock of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
SEALING COMPOUND, LOW ADHESION, CORROSION INHIBITING 9,000 to 14,000 Poises (900 to 1400 Pa·s), 2 Hour Application Time (B-2)AMS3267/4A (Current)4/1/1992
This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system.
AMS G9 Aerospace Sealing Committee
Alloy Powder, Corrosion and Heat Resistant, 59.5ni 12cr 10co 3.0mo 6.0w 3.0ti 1.5ta 4.5al 0.015b 0.10zr (0.30-0.35c), as FabricatedAMS5855B (Current)1/1/1993
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of August, 1992.
AMS F Corrosion and Heat Resistant Alloys Committee
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