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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
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
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
High-Tension Ignition CableJ2031_202511 (Current)11/06/2025
The specifications contained in this SAE Standard pertain to high-tension ignition cable used in road vehicle engine ignition systems.
Ignition Standards Committee
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, STRAIGHT, SELF-LOCKING, SHIELD BAND TERMINATION (RFI/EMI), SHRINK BOOT ACCOMMODATION, CATEGORY 3B (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)AS85049/85D (Current)04/01/2025
AE-8C1 Connectors Committee
Flux, Aluminum Brazing for Torch or Furnace BrazingAMS3412F (Current)08/09/2021
This specification covers the requirements for an aluminum brazing flux in the form of powder or paste.
AMS B Finishes Processes and Fluids Committee
Cleaner for Aircraft Exterior Surfaces Water-Miscible, Pressure-Spraying TypeAMS1526C (Current)04/29/2020
This specification covers a water-miscible, low-foaming cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Tube Fittings, Aerospace Fluid Systems, Separable, for 24 Degree Cone, General Specification, Metric (ISO 7169)MA2005C (Current)06/10/2021
This document specifies performance and quality requirements for the qualification and manufacture of 24 degree cone fittings to ensure reliable performance in aircraft hydraulic systems. This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines. This document covers fittings of temperature types and pressure classes specified in MA2001.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL CABLE SEALING, STRAIGHT, STEP-DOWN, CATEGORY 1A (FOR MIL-DTL-22992 CONNECTORS, CLASSES C, J, AND R)AS85049/5D (Current)02/08/2025
AE-8C1 Connectors Committee
Aluminum Alloy Die Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution and Precipitation Heat TreatedAMS4141H (Current)04/28/2021
This specification covers an aluminum alloy in the form of die forgings up to 6 inches in thickness and forging stock of any size ordered to inch/pound units (see 8.8).
AMS D Nonferrous Alloys Committee
Steel Bars, Wire, Forgings and Forging Stock, Mechanical Tubing, Rings, and Extrusions, Corrosion-Resistant 11.8Cr - 2.5Ni - 1.8Mo - 0.33V (0.08 - 0.15C) Annealed, Vacuum Arc or Electroslag RemeltedAMS5719E (Current)05/18/2021
This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and extrusions 7.00 inches (177.8 mm) and under in nominal diameter or least distance between parallel sides, and stock of any size for forging, flash welded rings, or extruding (see 8.8).
AMS F Corrosion and Heat Resistant Alloys Committee
Copper-Beryllium Alloy, Bars and Rods 98Cu - 1.9Be Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (TH04, formerly HT)AMS4534E (Current)04/22/2021
This specification covers a copper-beryllium alloy in the form of bars and rods up to 3.000 inches (76.20 mm), inclusive, in nominal diameter or least distance between parallel sides (see 8.7).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Bars, Rods, and Wire 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T4) Cold Finished, Solution Heat Treated and Naturally AgedAMS4116K (Current)04/14/2021
This specification covers an aluminum alloy in the form of bars, rods, and wire.
AMS D Nonferrous Alloys Committee
Flight Test Procedures for Static Pressure Systems Installed in Subsonic Transport AircraftARP921B (Current)12/22/2020
This SAE Aerospace Recommended Practice (ARP) covers the test procedures and equipment for performing flight testing on pitot-static systems installed in subsonic transport type aircraft.
A-4 Aircraft Instruments Committee
Elastomer: Silicone Rubber (VMQ) Aircraft Piston Engine Oil Resistant Compression Set Resistant 65 - 75 Type A HardnessAMS3357H (Current)03/10/2021
This specification covers a silicone (VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7XXX specification.
AMS CE Elastomers Committee
Iron-Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 41Fe - 37.5Ni - 14Co - 4.8Cb (Nb) - 1.5Ti Vacuum Melted, Low ExpansionAMS5802E (Current)06/05/2017
This specification covers a corrosion and heat-resistant iron-nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Cleaner, Turbine Engine Gas Path Solvent Emulsion TypeAMS1548B (Current)06/01/2017
This specification covers a solvent-emulsion cleaner in the form of a solvent-base liquid concentrate
AMS J Aircraft Maintenance Chemicals and Materials Committee
Steel, Bars, Forgings, and Tubing 4.1Cr - 3.4Ni - 4.2Mo - 1.2V (0.11 - 0.15C) Premium Aircraft-Quality for Bearing Applications Double Vacuum MeltedAMS6278F (Current)09/09/2020
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings, and Tubing 1.45Cr (0.93-1.05C) (SAE 52100) Special Aircraft-Quality CleanlinessAMS6479E (Current)09/09/2020
This specification covers a special aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Steel, Corrosion Resistant, Sheet, Strip, and Plate 15Cr - 6.5Ni - 0.75Mo - 0.30Cb - 1.5Cu Consumable Electrode Melted, Solution Heat Treated Precipitation HardenableAMS5859F (Current)01/13/2021
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Phosphor Bronze, Sheet, Strip, and Plate 94.5Cu - 4.0Sn - 0.19P Spring Temper (H08)AMS4510J (Current)01/20/2021
This specification covers a copper alloy (phosphor bronze) in the form of sheet, strip, and plate.
AMS D Nonferrous Alloys Committee
Plating, Chromium Hard DepositAMS2406P (Current)12/30/2020
This specification covers the requirements for electrodeposited hard chromium plate.
AMS B Finishes Processes and Fluids Committee
Cleaner for Aircraft Exterior Surfaces Emulsion, Foam-On, Pressure-Spray TypeAMS1529D (Current)04/29/2020
This specification covers an emulsion-type, foam-on, pressure-spray cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Copper-Beryllium Alloy, Bars, Rods, Shapes, and Forgings 98Cu - 1.9Be Solution Heat Treated TB00 (A)AMS4650N (Current)04/11/2019
This specification covers a copper-beryllium alloy in the form of bars, rods, shapes, and forgings.
AMS D Nonferrous Alloys Committee
Performance Testing of Lubricant Filter Elements Utilized in Aircraft Power and Propulsion Lubrication SystemsAIR1666C (Current)11/12/2020
This SAE Aerospace Information Report (AIR) reviews performance testing parameters for non-cleanable (often referred to as disposable) filter elements utilized in aircraft power and propulsion lubrication systems, including gas turbine engines and auxiliary power units (APUs), propulsion and transmission gear boxes, and constant speed drives and integrated drive generators (IDGs). This document is confined to laboratory testing of filter element performance to qualify the filtration medium and filter element construction as opposed to qualification of the complete filter assembly. The testing discussed here is usually followed by laboratory and on-engine testing of the entire lube filter assembly (including filter element, housing, valving, etc.), which is outside the scope of this AIR.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Polyalkylene Glycol Heat Treat QuenchantAMS3025E (Current)01/18/2018
This specification covers two types of polyalkylene glycol in the form of a liquid.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T6151) Solution Heat Treated, Stress Relieved, and AgedAMS4306C (Current)01/12/2018
This specification covers an aluminum alloy in the form of plate.
AMS D Nonferrous Alloys Committee
Ductile (Nodular) Iron Castings, Sand 60000 psi (415 MPa) Tensile Strength Ferritize AnnealedAMS5315E (Current)08/04/2017
This specification covers a ductile (nodular) iron in the form of sand castings.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T51) Precipitation Heat TreatedAMS4210M (Current)04/22/2021
This specification covers an aluminum alloy in the form of castings.
AMS D Nonferrous Alloys Committee
Leaded Brass, Seamless Tubing 66.5Cu - 32.5Zn - 0.48Pb Light Annealed (O50)AMS4555L (Current)04/22/2021
This specification covers a copper alloy (leaded brass) in the form of seamless tubing.
AMS D Nonferrous Alloys Committee
Steel, Corrosion and Heat Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Multiple Melted, 1800 °F (982 °C) Solution Heat Treated, Welding Grade Precipitation HardenableAMS5858E (Current)04/27/2021
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Quality Assurance Sampling and Testing Carbon and Low-Alloy Steel ForgingsAMS2372H (Current)04/05/2019
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable specification requirements of carbon and low-alloy steel forgings.
AMS E Carbon and Low Alloy Steels Committee
Remover, Acid Activated, For Amine-Cured Epoxy Coating SystemsAMSR81903A (Current)05/06/2021
This specification covers the requirements for removers used on amine-cured epoxy coating systems (see 6.1).
AMS J Aircraft Maintenance Chemicals and Materials Committee
Leaded Phosphor Bronze Strip 88.5Cu - 4.0Sn - 4.0Pb - 3.0Zn - 0.26P Cold Rolled, Half Hard (H02)AMS4520M (Current)04/28/2021
This specification covers a copper alloy in the form of strip.
AMS D Nonferrous Alloys Committee
Steel, Corrosion and Heat Resistant, Welded Tubing 25Cr - 20Ni (310) Solution Heat TreatedAMS5577J (Current)04/15/2019
This specification covers a corrosion and heat resistant steel in the form of welded tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
Plating, LeadAMS2414G (Current)08/09/2021
This specification covers the requirements for electrodeposed lead on metal parts.
AMS B Finishes Processes and Fluids Committee
Compound, Corrosion-Inhibiting Water-Displacing, Soft Film, Aerosol CannedAMS3066C (Current)08/09/2021
This specification covers a solvent-dispersed, corrosion-inhibiting compound packaged in aerosol cans.
AMS B Finishes Processes and Fluids Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings, and Tubing 16Cr - 2.5Ni (SAE 51431)AMS5628F (Current)05/26/2015
This specification covers a heat-treatable, corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, and stock for forging or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
Manganese Bronze, Sand and Centrifugal Castings 63Cu - 24Zn - 6.2Al - 3.8Mn - 3.0Fe High Strength, As CastAMS4862F (Current)03/23/2016
This specification covers a manganese bronze alloy in the form of sand and centrifugal castings.
AMS D Nonferrous Alloys Committee
BOLT, MACHINE - SPLINE EXTENDED WASHER, FULL HEAD, PD SHANK, LONG THREAD, NICKEL ALLOY (UNS N07718) - METRICMA3476A (Current)11/12/2020
E-25 General Standards for Aerospace and Propulsion Systems
Compound, Corrosion-Preventive Hard Film, Hot ApplicationAMS3075F (Current)08/09/2021
This specification covers a stable, nonvolatile, petroleum-base compound in a form suitable for application by dipping at 170 to 210 °F (77 to 99 °C).
AMS B Finishes Processes and Fluids Committee
Minimum Performance Standard Stall Warning EquipmentAS8014A (Current)12/22/2020
This Aerospace Standard covers two basic Stall Warning Systems, one measures air flow and pressure distribution on the airfoil and the other measures the angle of airflow with respect to an arbitrary reference line. Each type of system includes, as a minimum, a sensor and the means for activating a device which warns the pilot of an impending stall.
A-4 Aircraft Instruments Committee
Aircraft Fuel System Pressure DefinitionsAIR1749A (Current)12/18/2020
The information in this document is limited to aircraft engine fuel feed, refueling, and transfer components (see 2.1). It is assumed that isothermal, liquid fluid conditions exist, herein referred to as fuel. Where applicable and allowable, it is understood that a referee fluid may be substituted for fuel.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Cobalt Alloy, High Temperature Brazing Filler Metal 50Co - 8.0Si - 19Cr - 17Ni - 4.0W - 0.80B 2050 to 2100 °F (1121 to 1149 °C) Solidus-Liquidus RangeAMS4783H (Current)07/07/2021
This specification covers a cobalt alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion and Heat-Resistant, Plate 54Ni - 22Cr - 12.5Co - 9.0Mo - 1.2Al AnnealedAMS5888D (Current)07/19/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of plate nominally 2.00 inches (50.8 mm) and under in thickness, inclusive.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Welding Wire 0.65Si - 1.25Cr - 0.50Mo - 0.30V (0.28 - 0.33C)AMS5035C (Current)12/23/2014
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy Bars, Rolled or Cold Finished 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T451) Solution Heat Treated and Stress Relieved by StretchingAMS4128E (Current)06/28/2021
This specification covers an aluminum alloy in the form of bars and rods 0.500 inch (12.7 mm) to 8.000 inches (203.2 mm) in nominal diameter or least difference between parallel sides and up to 50 square inches (322.6 square centimeters) in cross-sectional area (see 8.7).
AMS D Nonferrous Alloys Committee
Case Hardening of Titanium and Titanium AlloysAMS2775C (Current)10/22/2015
This specification covers the engineering requirements for producing a carbon-oxygen-nitrogen-bearing case on titanium and titanium alloys by means of a molten salt bath, and the properties of the case.
AMS B Finishes Processes and Fluids Committee
Electric Tachometer: Magnetic Drag (Indicator & Generator)AS404C (Current)02/16/2008
This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
A-4 Aircraft Instruments Committee
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