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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
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
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), .2500-28 UNJF-3AAS3307B (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, 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
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
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
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
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
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
Silicone Rubber Sponge Closed Cell, MediumAMS3195H (Current)6/14/2019
This specification covers a silicone rubber sponge in the form of sheet, strip, extrusions, and molded shapes.
AMS CE Elastomers Committee
Carbon Fiber Tape and Sheet Epoxy Resin Impregnated G 110000 (758) Tensile, 27000000 (186) Modulus, 80 (176)AMS3894/5C (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
Plating, Brush, Zinc-Nickel Low Hydrogen EmbrittlementAMS2451/9C (Current)5/24/2023
This specification covers the requirements for brush plating of zinc-nickel by electrodeposition.
AMS B Finishes Processes and Fluids Committee
Tolerances, Aluminum And Aluminum Alloy Bar, Rod, Wire, And Forging Stock Rolled Or Cold-FinishedAMS2201M (Current)9/1/1994
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of September 1994. The requirements of this specification are embodied in the latest issue of ANSI H35.2, Dimensional Tolerances for Aluminum Mill Products.
AMS D Nonferrous Alloys 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
Bolts and Screws Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Roll Threaded, Fatigue ResistantAMS7466B (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys 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
Bolts and Screws Roll ThreadedAMS7473F (Current)10/1/1993
AMS E Carbon and Low Alloy Steels 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
Alloy Bars and Forgings, Corrosion and Heat Resistant, 38fe 13.2cr 38ni 5.5mo 0.85cb 2.5ti 1.6al 0.009b, Consumable Electrode Melted, Solution Heat Treated, Precipitation HardenableAMS5633D (Current)7/1/1993
This specification has been "CANCELLED" by the Aerospace Materials, Division, SAE, as of July 1, 1993.
AMS F Corrosion and Heat Resistant Alloys Committee
Graphite Fiber Tape and Sheet, Epoxy Resin Impregnated, G 150,000 (1034) Tensile, 15,000,000 (103) Modulus, 350 (177)AMS3894/6B (Current)12/1/1994
This specification covers one type of epoxy-resin-impregnated graphite fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
Retaining Rings, Steel Corrosion Resistant, Spiral WoundAMS7330B (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Rings, Sealing, Tubular Metal, Corrosion and Heat Resistant SteelAMS7325F (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Glass Non-Woven Fiber Tape and Flat Sheet Epoxy Resin Impregnated, For Hand and Machine Layup GL-I-36 - 150 (302)AMS3906/5C (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
Alcohol, Denatured EthylAMS3002H (Current)3/24/2014
This specification covers a denatured ethyl alcohol in the form of a liquid.
AMS B Finishes Processes and Fluids Committee
Solvent, Petroleum AromaticAMS3165F (Current)2/9/2016
This specification covers a petroleum-base liquid solvent.
AMS B Finishes Processes and Fluids 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
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
Tolerances Carbon and Alloy Steel TubingAMS2253F (Current)2/24/2018
This specification covers established inch/pound manufacturing tolerances applicable to carbon and alloy tubing ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range.
AMS E Carbon and Low Alloy Steels Committee
Silicone Rubber Sponge Closed Cell, Medium, Extreme Low TemperatureAMS3193F (Current)6/14/2019
This specification covers a silicone rubber sponge in the form of sheet, strip, extrusions, and molded shapes.
AMS CE Elastomers Committee
Yarn, Organic Fiber (Para-Aramid) Intermediate Modulus 3000 Denier (3300 Dtex), 0.9% FinishAMS3904/9B (Current)8/1/2016
This specification covers one type of organic (para-aramid) 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
POLYTETRAFLUOROETHYLENEAMS3651D (Current)12/1/1994
AMS P Polymeric Materials Committee
POTTING COMPOUND, EPOXY, FLEXIBLE Durometer 75 - 85AMS3750 (Current)12/1/1994
AMS P Polymeric Materials Committee
Bolts and Screws, Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Heat Treated, Roll Threaded, 1950°F Solution Heat Treatment (AMS 5708)AMS7471G (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Test Slabs, Fluorosilicone (FVMQ) 55 - 65AMS3217/5C (Current)7/19/2013
This specification covers a standard fluorosilicone (FVMQ) rubber stock in the form of molded test slabs.
AMS CE Elastomers Committee
Webbing, Low Modulus Aramid 1-23/32 (44) Wide, 5500 (24,465) Breaking Strength Double Plain Weave with BinderAMS3798/4C (Current)4/14/2015
This specification covers one width and one breaking strength of low-modulus aramid webbing.
AMS P Polymeric Materials Committee
Webbing, Textile, Tubular, Para-Aramid Intermediate Modulus 0.50 ounce per linear yard (20 g/linear m)AMS3782/4B (Current)9/11/2013
This specification covers one weight and type of para-aramid webbing.
AMS P Polymeric Materials Committee
Webbing, Nylon/Polyester, Aircraft Arresting Center Pick 130,000 Pounds (578 kN)AMS3796/3B (Current)6/9/2016
This specification covers one type of nylon/polyester in the form of webbing.
AMS P Polymeric Materials Committee
Aluminum Alloy, 2017, Bar, Rod, and Wire, Rolled, Drawn, or Cold FinishedAMSQQA225/5A (Current)11/6/2018
This specification covers the specific requirements for 2017 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing.
AMS D Nonferrous Alloys Committee
Cloth, Parachute, Meta-Aramid, Low Modulus 7.0 (237) Weight, Plain WeaveAMS3801/4C (Current)10/11/2016
This specification covers one weight and one weave of low-modulus meta-aramid cloth.
AMS P Polymeric Materials Committee
Tape and Webbing, Textile, Para-Aramid Intermediate Modulus 1-1/2 Inches (37.5 mm), 0.12 to 0.47 Ounces per Yard (3.7 to 14.6 g/m)AMS3793/7B (Current)9/11/2013
This specification covers three classes of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
Webbing, Low Modulus Aramid 3/4 (19) Wide, 600 (2669) Breaking Strength Herringbone TwillAMS3798/3C (Current)4/14/2015
This specification covers one width and one breaking strength of low-modulus aramid webbing.
AMS P Polymeric Materials Committee
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