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Silicone (PVMQ) Rubber Extreme-Low-Temperature Resistant 65 - 75AMS3337G (Current)11/10/2025
This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Rubber, Fluorocarbon Elastomer (FKM) 70 to 80 Hardness, Low Temperature Sealing Tg -22 °F (-30 °C) For Elastomeric Shapes or Parts in Gas Turbine Engine Oil, Fuel and Hydraulic SystemsAMS3384A (Current)11/10/2025
This specification covers a high temperature, compression set and fluid resistant fluorocarbon (FKM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes for aeronautical and aerospace applications.
AMS CE Elastomers Committee
Dedicated Short Range Communications (DSRC) Performance Requirements for V2V Safety AwarenessJ2945/2_202511 (Current)11/10/2025
This SAE Document specifies DSRC interface requirements for V2V Safety Awareness applications, including detailed Systems Engineering documentation (needs and requirements mapped to appropriate message exchanges). These applications include: Emergency Vehicle Alert, Roadside Alert, and Safety Awareness Alerts for Objects and Adverse Road Conditions. This document extends the V2V Communications capabilities defined in J2945/1 to support these applications, and the National ITS Architecture. The purpose of this SAE Document is to enable interoperability for V2V Safety Awareness communications.
V2X Core Technical Committee
Time‐Sensitive Networking for Aerospace Onboard Ethernet CommunicationsIEEE/SAEAS6675 (Current)11/07/2025
This standard specifies profiles of IEEE 802.1 Time-Sensitive Networking (TSN) and IEEE 802.1 Security standards for aerospace onboard bridged IEEE 802.3 Ethernet networks. The profiles select features, options, configurations, defaults, protocols, and procedures of bridges, end stations, and Local Area Networks to build deterministic networks for aerospace onboard communications.
AS-1A Avionic Networks Committee
CONNECTOR ADAPTER, RFI SHIELDED, CABLE TO ELECTRIC CONNECTORAS81582/4B (Current)10/23/2025
AE-8C1 Connectors Committee
SHIELD TERMINATION, SOLDER STYLE, INSULATED, HEAT-SHRINKABLE, ENVIRONMENT RESISTANT WITH PREINSTALLED BRAID, NI PLATED, CLASS 1, ROHSAS83519/5B (Current)09/18/2025
AE-8C2 Terminating Devices and Tooling Committee
National Aerospace and Defense Contractors Accreditation Program Titanium 3Al-2.5V Alloy, Seamless Hydraulic Tubing Manufacturing RequirementsAS7112/6 (Current)01/09/2013
This Aerospace Standard (AS) is to be used as a supplement to SAE AS7112. In addition to the requirements specified in AS7112, the requirements specified herein shall apply to suppliers seeking Nadcap Fluid System accreditation for manufacturing titanium 3AI-2.5V alloy, seamless hydraulic tubing. The corresponding PRI Audit Criteria (AC) is to be applied to ensure the tubing is manufactured to the applicable specification(s) and standard(s).
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING END; ATTACHABLE, FLARELESS MALE, FLEXIBLE METAL HOSE - STRAIGHT, 45° ELBOW AND 90° ELBOW STYLESAS1016 (Current)04/01/1993
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLT, MACHINE - HEXAGON HEAD, DRILLED, 1 HOLE, PD SHANK, STEEL, UNS K14675, DIFFUSED NICKEL-CADMIUM PLATE, 195 KSI MIN, .1900-32 UNJF-3AAS9685D (Current)04/21/2023
E-25 General Standards for Aerospace and Propulsion Systems
Appendix A Electronic Display Symbology for EADI/PFDARP4102/7_APXA (Current)07/10/2007
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 28 000 kPa, HYDRAULIC AND PNEUMATICMA2140 (Current)01/26/2003
This specification defines the requirements for a PTFE lined, non-metallic, aramid reinforced assembly suitable for use to 135°C and 28 000 kPa aircraft and missile hydraulic and pneumatic systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Requirements for Oversight of Aerospace Quality Management System Registration/Certification ProgramsAS9104/2A (Current)06/13/2014
The requirements established in this document are applicable to the IAQG and associated sectors for managing oversight to established requirements contained in 9104-series standards (i.e., 9104/1, 9104/2, 9104/3). The requirements are applicable to IAQG working groups for oversight. NOTE: All required forms are depicted in Appendix A. These form exhibits are provided for reference only; the current versions of these forms are available on the IAQG website.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
STUD, STEPPED, 1.5 DIA ENGAGEMENT, CADMIUM PLATED, STEEL UNS G87400, .2500-20 UNS X .1900-32 UNF-3AAS150501C (Current)08/12/2014
E-25 General Standards for Aerospace and Propulsion Systems
DISPOSITION OF WHEELS WHICH HAVE BEEN OVERHEATEDAIR811A (Current)08/10/2011
A-5A Wheels, Brakes and Skid Controls Committee
SHORT-BAR FRACTURE TOUGHNESS OF METALLIC MATERIALS Determination ofARP1704 (Current)07/01/1981
This method covers the determination of the fracture toughness of metallic materials (KSR or KSB) by testing slotted short-rod or short-bar specimens.
AMS D Nonferrous Alloys Committee
BOLT, MACHINE-DOUBLE HEXAGON, EXTENDED WASHER HEAD, DRILLED, SILVER PLATED, NICKEL ALLOY (UNS N07001), .3125-24 UNJF-3AAS9716C (Current)04/01/2022
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, CLOSE TOLERANCE SHANK, AMS4967, .5625-18 UNJF-3AAS3162B (Current)12/29/2020
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS4967 (UNS R56400), 160 KSI, .5000-20 UNJF-3AAS3152B (Current)12/02/2019
E-25 General Standards for Aerospace and Propulsion Systems
CABLE, SAFETY, NICKEL ALLOY, CORROSION RESISTANT (UNS N06625)AS3655A (Current)11/01/2019
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, FULL SHANK, CORROSION AND HEAT RESISTANT STEEL, UNS S66286, 130 KSI MIN, .6250-18 UNJF-3AAS9496B (Current)11/02/2018
E-25 General Standards for Aerospace and Propulsion Systems
Design Recommendations for Spare Seals in Landing Gear Shock StrutsARP4912C (Current)03/27/2025
This SAE Aerospace Recommended Practice (ARP) provides recommendations on cavity design, the installation of elastomer type spare seals in these cavities, and information surrounding elastomer material properties after contact with typical shock absorber hydraulic fluid(s) or grease. This ARP is primarily concerned with the use of spare seals on shock absorbers where only a single dynamic seal is fitted and in contact with the slider/shock absorber piston at any one time. These shock absorbers typically have a spare (dynamic) seal gland located on the outer diameter of the lower seal carrier. This spare seal gland is intended to house a spare elastomer contact seal. Split Polytetrafluoroethylene (PTFE) backup rings can also be installed in the spare seal cavity. During operation, if the fitted dynamic shock absorber standard seal begins to fail/leak, then the aircraft can be jacked up, allowing the lower gland nut of the shock absorber to be dropped down. The current used dynamic seal
A-5B Gears, Struts and Couplings Committee
TOLERANCES, METRIC Aluminum Alloy Drawn TubingMAM2203 (Current)07/23/2002
This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.
AMS D Nonferrous Alloys Committee
Test Plan/Procedure for AS5643 IEEE-1394b Interface Requirements for Military and Aerospace Vehicle ApplicationsAS5657 (Current)04/25/2025
This document establishes test plans/procedures for the AS5643 Standard that by itself defines guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. This test specification defines procedures and criteria for testing device compliance with the AS5643 Standard.
AS-1A Avionic Networks Committee
PUMPS, HYDRAULIC, POWER DRIVEN, VARIABLE DELIVERY COMPOSITE OUTLINE DRAWINGSAIR45 (Current)09/30/2000
Outline drawings from all known pump manufacturers for the various size pumps listed in MIL-P-7740 were requested and those received have been combined to make up the various outline drawings. There has been prepared a composite outline drawing enclosing all of the individual outline drawings. Since the pump manufacturers' drawings will change over a period of time and complete detail is not shown, it is not possible to make a detailed mockup of any specific pump. These drawings are intended to provide information concerning the general space requirement for variable delivery pumps, and could be used to manufacture a composite mockup to indicate roughly the space required on a new engine design.
A-6C4 Power Sources Committee
Low Speed Thorax Impact Test Procedure for the HIII 50th Male DummyJ2779_202206 (Current)06/29/2022
Dummy Testing and Equipment Committee
Polishing Compound, Aircraft MetalAMS1650D (Current)05/06/2021
This specification covers a polishing compound for aircraft metals in the form of a liquid or paste.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Chloroprene (CR) Rubber Weather Resistant 65 - 75AMS3209M (Current)03/18/2014
This specification covers a chloroprene (CR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Steel, Mechanical Tubing 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337)AMS6413N (Current)12/18/2020
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
AMS E Carbon and Low Alloy Steels Committee
Ethylene Propylene (EPM) Rubber Phosphate Ester Resistant 55 - 65AMS3248D (Current)09/18/2020
This specification covers an ethylene propylene (EPM) rubber in the form of sheet, strip, tubing, molded shapes, and extrusions.
AMS CE Elastomers Committee
Tungsten Heavy Alloy Shapes, Sintered, High DensityAMS7725F (Current)11/12/2020
This specification covers four classes of tungsten heavy metal in the form of sintered and annealed shapes.
AMS G Titanium and Refractory Metals Committee
Titanium Alloy Bars, Wire, Forgings, and Rings 6Al - 4V, Extra Low Interstitial AnnealedAMS4930L (Current)10/09/2020
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or distance between parallel sides, and stock for forging or flash welded rings of any size.
AMS G Titanium and Refractory Metals Committee
Steel Castings, Investment 0.80Cr - 1.8Ni - 0.35Mo (0.28 - 0.36C) (SAE 4330 Modified) AnnealedAMS5328E (Current)08/04/2017
This specification covers a low-alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
Iron-Nickel-Cobalt Alloy, Bars and Forgings 53Fe - 29Ni - 17Co Low Expansion, Glass SealingAMS7727F (Current)04/06/2017
This specification covers an iron-nickel-cobalt alloy in the form of bars and forgings.
AMS F Corrosion and Heat Resistant Alloys Committee
Alloy Sheet and Strip, Sintered Wire Mesh, Corrosion and Heat Resistant 30Fe - 1.5Mn - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0(Cb +Ta) - 0.15N PorousAMS7724D (Current)04/06/2017
This specification covers a corrosion and heat resistant iron alloy sintered wire mesh in the form of sheet and strip.
AMS F Corrosion and Heat Resistant Alloys Committee
Perfluorocarbon (FFKM) Engine Oil, Fuel and Hydraulic Fluid Resistant 70 to 80 Hardness For High Temperature Seals in Engine Oil Systems, Fuel Systems and Hydraulic SystemsAMS7257E (Current)09/05/2014
This specification covers a Perfluorocarbon (FFKM) rubber in the form of molded rings, compression seals, o-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications.
AMS CE Elastomers Committee
Phosphate Treatment AntichafingAMS2481K (Current)01/08/2021
This specification covers the requirements for a manganese phosphate coating on ferrous alloys.
AMS B Finishes Processes and Fluids Committee
Metal Dimensional Change with TemperatureAIR809B (Current)03/30/2018
Data are related to the dimensional changes with respect to room temperature and provide accuracy sufficient for use with most aerospace systems. Two basic methods of solution are presented with examples for steady state conditions involving uniform and non-uniform temperature distributions. The answers to the example problems are carried to the fifth place for a comparison of the results between Methods I and II.
E-25 General Standards for Aerospace and Propulsion Systems
BUSHING, CABLE CLAMP TO CABLE, TELESCOPING FOR AS85049 CABLE CLAMPS CATEGORY 9AS85049/139C (Current)02/08/2025
AE-8C1 Connectors Committee
Carbon Fiber Tape and Sheet Epoxy Resin ImpregnatedAMS3894F (Current)09/14/2016
This specification and its supplementary detail specifications cover tape and sheet fabricated using carbon fibers impregnated with epoxy resin.
AMS P17 Polymer Matrix Composites Committee
Tape and Sheet, Adhesive, Rubber and Cork CompositionAMST6841A (Current)07/06/2016
This specification covers one type of tape and sheet for use in the installation of windshields, panels, and windows in cabins and cockpits of aircraft.
AMS P Polymeric Materials Committee
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, 45°, SELF LOCKING, SHIELD, BAND TERMINATION, (RFI/EMI), SHRINK SLEEVE ACCOMMODATION, CATEGORY 3B (FOR AS50151 CRIMP, AS95234, MIL-DTL 26482 SERIES 2, AS81703 SERIES 3 AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/83D (Current)04/01/2025
AE-8C1 Connectors Committee
Aluminum Alloy Die Forgings, and Rolled or Forged Rings 0.9Si - 0.62Mg - 0.25Cr (6151-T6) Solution and Precipitation Heat TreatedAMS4125L (Current)11/14/2014
This specification covers an aluminum alloy in the form of die forgings, rolled or forged rings, and stock for forgings and rings.
AMS D Nonferrous Alloys Committee
Steel Castings, Sand, Corrosion and Moderate Heat Resistant 13Cr Normalized and TemperedAMS5351G (Current)04/04/2017
This specification covers a corrosion and moderate heat resistant steel in the form of sand castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Graphite Coating, Thin Lubricating Film Impingement AppliedAMS2525E (Current)10/10/2019
This specification covers a coating consisting of finely-powdered graphite in a heat-resistant inorganic binder.
AMS B Finishes Processes and Fluids Committee
Copper Sheet, Strip, and Plate Oxygen-Free, Light Cold RolledAMS4501F (Current)04/04/2017
This specification covers one type of copper in the form of sheet, strip, and plate.
AMS D Nonferrous Alloys Committee
Core, Flexible Honeycomb, Aluminum Alloy, Treated for Sandwich Construction 5052, 350 Fahrenheit (177 Celsius)AMS4178G (Current)07/07/2021
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form.
AMS D Nonferrous Alloys Committee
Magnesium Alloy, Plate, Extra Flat 3.0Al – 1.0Zn – 0.20Mn (AZ31B-0) AnnealedAMS4382D (Current)11/08/2018
This specification covers a magnesium alloy in the form of plate.
AMS D Nonferrous Alloys Committee
Cleaner for Aircraft Exterior Surfaces Wipe-On, Wife-OffAMS1530C (Current)04/29/2020
This specification covers a cleaner in the form of a ready-to-use liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Bearings, Leaded Bronze 80Cu – 10Pb – 10Sn Steel BackAMS4827F (Current)04/19/2018
This specification covers bearings of a leaded bronze cast on one or both faces of a steel backing.
AMS D Nonferrous Alloys Committee
NUT, CASTELLATED, HEX - UNS S66286, SILVER PLATE, MJ THREAD, METRICMA3426B (Current)05/28/2021
E-25 General Standards for Aerospace and Propulsion Systems
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