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Aircraft Electrical Voltage Level DefinitionsAIR7502A (Current)
The scope of this report will document the various voltage levels and provide a rational for each level as discussed and agreed to in the AE-7 committee.
AE-7C Systems
Pyrotechnic Actuator for Fast Action Electrical Protection in HVDC Aerospace ApplicationAIR7258 (Current)
The scope of this report is to establish applicable definitions and terms prior to considering the application domain and use cases in HVDC applications. The report describes the specificities of the pyrotechnic actuator for use within a power-switching device with performances and main characteristics to consider for aerospace application.
AE-10 High Voltage Committee
Titanium Alloy Sheet, Strip, and Plate, 8Al - 1V - 1Mo, Single AnnealedAMS4915P (Current)12/19/2025
This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive (see 8.6).
AMS G Titanium and Refractory Metals Committee
Aircraft Position LightsAS271B (Current)12/19/2025
This specification covers three types of aircraft position lights. Type I - Forward Position Light (red wing tip light) Type II - Forward Position Light (green wing tip light) Type m - Rear Position Light (white tail light)
A-20B Exterior Lighting Committee
Qualified Hoses for Marine ApplicationsJ1942/1_202512 (Current)12/19/2025
The following list consists of hose data provided as of December 2025 and is for convenience in determining acceptability of nonmetallic flexible hose assemblies intended for usage under 46 CFR Part 56.60-25. Where the maximum allowable working pressure (MAWP) or type of fitting is not specified, use the manufacturer’s recommended MAWP or type of fitting. This list has been compiled by SAE staff from information provided by the manufacturers whose product listings appear in this document. Manufacturers wishing to list their products in this document shall: a. Successfully test their hose to the requirements of SAE J1942, Table 1. b. Submit a letter of certification to the SAE J1942 test requirements for each specific type of hose tested (see sample table, Table 1) along with the test results. All sizes should be included in the same letter, which must also include all of the information necessary to make an SAE J1942-1 listing. c. SAE will review the letter and may, at their discretion
Hydraulic Hose and Hose Fittings Committee
Gas Turbine Engine Test Facility Vibration MeasurementARP6068A (Current)12/19/2025
The test procedure per the applicable Engine Manual does require a vibration check for the low/intermediate and high speed rotor systems. Release of an engine with high vibrations can result in: On-wing vibration complaints, with subsequent troubleshooting Rotor system failures Premature engine removals Limits are provided for transient conditions and steady state data points. Troubleshooting recommendations are limited to verification of the proper signal input and tracking. This practice provides recommendations for: Correct cable and transmitter installation and connections Calibration Recorded data interpretation and data analysis
EG-1E Gas Turbine Test Facilities and Equipment
Color-Coded Incandescent Flange Base T-1 and T-1 3/4 Lamps for Voltage IdentificationAS4156D (Current)12/19/2025
This document specifies that black is the only color that can be used for the insulator at the bottom of the base of T-1 and T-1 ¾ Flanged Base lamps.
A-20A Crew Station Lighting
Connectors, Plug, Electric, 45° Assembly, Crimp Contact, AN TypeAS34091B (Current)12/19/2025
Scope is unavailable.
AE-8C1 Connectors Committee
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems (Supplement 1)AS1975SUP1A (Current)12/19/2025
This supplement forms a part of AS1975, Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems and shall be used to identify hose assembly standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, BUSSING MODULES, FEEDBACK TYPE, SIZE 22D, SERIES IAS81714/17C (Current)12/19/2025
AE-8C2 Terminating Devices and Tooling Committee
Automotive Gear Lubricants for Commercial and Military UseJ2360_202512 (Current)12/19/2025
The gear lubricants covered by this standard exceed American Petroleum Institute (API) Service Classification API GL-5 and are intended for automotive units with the primary drive hypoid gears, operating under conditions of high-speed/shock load and low-speed/high-torque. These lubricants may be appropriate for other gear applications where the position of the shafts relative to each other and the type of gear flank contact involve a large percentage of sliding contact. Such applications typically require extreme pressure (EP) additives to prevent the adhesion and subsequent tearing away of material from the loaded gear flanks. These lubricants are not appropriate for the lubrication of worm gears. The information contained within is intended for the demonstration of compliance with the requirements of this standard and for listing on the Qualified Products List (QPL) administered by the Lubricant Review Institute (LRI). A complete listing of qualification submission requirements and
Fuels and Lubricants TC 3 Driveline and Chassis Lubrication
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate, 59Ni - 22Cr - 2Mo - 14W - 0.35Al - 0.03La (Alloy No. 230®), Solution Heat TreatedAMS5878F (Current)12/19/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate 0.015 to 1.5 inches (0.38 to 38 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Fuel Consumption Test Procedure - Type IIJ1321_202512 (Current)12/19/2025
This document describes a rigorous-engineering fuel-consumption test procedure that utilizes industry accepted data collection and statistical analysis methods to determine the change in fuel consumption for trucks and buses with gross vehicle weight rating (GVWR) of more than 10000 pounds, equipped with internal combustion engines using diesel, gasoline, or their liquid substitutes. The test procedure may be conducted on a test track or on a public road under controlled conditions and supported by extensive data collection and data analysis constraints. The on-road test procedure is offered as a lower cost alternative to on-track testing, but the user is cautioned that on-road test may result in lower resolution (or precision) data due to a lack of control over the test environment. Test results that do not rigorously follow the method described herein are not intended for public use and dissemination and shall not be represented as an SAE J1321-Type II test result. This document
Truck and Bus Aerodynamics and Fuel Economy Committee
Titanium Alloy Bars, Forgings, and Flash Welded Rings 5Al-2.5V-4Sn-1Co-0.8Fe Solution Heat Treated and AgedAMS6904 (Current)12/19/2025
Titanium alloy specification for bars, forgings, and flash welded rings.
AMS G Titanium and Refractory Metals Committee
Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate, Ti-6Al-4V, Stress RelievedAMS7004A (Current)12/19/2025
This specification covers preforms fabricated up through 22.0 inches (560 mm), inclusive, in deposition width thickness (see 2.4) using a wire-fed plasma arc directed energy deposition (PA-DED) additive-manufacturing process on a Ti-6Al-4V substrate that are subjected to post-deposition stress-relief heat treatment. If required by the cognizant engineering organization (CEO), preforms may require subsequent machining to meet requirements for their intended final part application.
AMS AM Additive Manufacturing Metals
CONNECTORS, RECEPTACLE, ELECTRIC, WALL MOUNTING, FRONT RELEASE, CRIMP CONTACT, AN TYPE – WITH ACCESSORY THREADSAS34121D (Current)12/18/2025
SCOPE IS UNAVAILABLE.
AE-8C1 Connectors Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate, 65Ni - 15.8Cr - 15.2Mo - 0.30Al - 0.05La (HASTELLOY® S), Consumable Electrode Remelted, Solution Heat TreatedAMS5873H (Current)12/16/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Phosphate Treatment, AntichafingAMS2481L (Current)12/12/2025
This specification covers the requirements for a manganese phosphate coating on ferrous alloys.
AMS B Finishes Processes and Fluids Committee
CLAMP, LOOP TYPE, CUSHIONED SUPPORTAS21919D (Current)12/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Comparative Performance Data for Extra-High Strength Copper Alloy ConductorsAIR7145 (Current)12/11/2025
This AIR is limited to the testing of an extra-high strength copper alloy and benchmark conductors utilizing the test protocol of AS6324. All samples are 19 strand unilay conductors per AS29606 at 24 or 26 AWG, either nickel or silver coated. At 24 AWG, extra-high strength copper alloy is compared to high strength copper alloy conductors. At 26 AWG, extra-high strength copper alloy is compared to high strength copper alloy and ultrahigh strength copper alloy conductors.
AE-8D Wire and Cable Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Rings, Extrusions, and Stock for Forgings and Rings, 61Ni - 20.5Cr - 8.5Mo - 3.4Cb(Nb) - 1.3Ti - 5.0Fe (Alloy 716), Consumable Electrode or Vacuum Induction Melted, Solution Heat TreatedAMS5854D (Current)10/16/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, wire, forgings, flash-welded rings, and extrusions 4 inches (102 mm) and under in nominal diameter or least distance between parallel sides and stock for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Flat Wire, 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V (A286), 1800 °F (982 °C) Solution Treated, Cold Drawn or Cold Rolled and Aged, Consumable Electrode RemeltedAMS5810C (Current)10/02/2025
This specification covers a corrosion- and heat-resistant steel in the form of flat wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel-Copper Alloy Wire and Ribbon, Corrosion-Resistant, 67Ni - 31Cu (Monel® 400), AnnealedAMS4731E (Current)10/02/2025
This specification covers a corrosion-resistant nickel-copper alloy in the form of wire and ribbon.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire, 19Cr - 12.5Ni - 2.5Mo (316L)AMS5696F (Current)10/15/2025
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Welding Wire 2.0Cr - 10Ni - 14Co - 1.0Mo - (0.13 - 0.17C) Vacuum Melted, Environment Controlled PackagingAMS6533D (Current)10/23/2025
This specification covers a premium aircraft-quality alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, REPOSITIONABLE TO STRAIGHT, 45° AND 90°, ENVIRONMENTAL, CABLE SEALING, SHIELD TERMINATION, CATEGORY 1A, (FOR MIL-DTL-83723 SERIES III, AS50151 CRIMP, AS81703 SERIES 3, MIL-DTL-26482 SERIES 2, AND AS95234 CONNECTORS)AS85049/150B (Current)12/17/2025
SCOPE IS UNAVAILABLE.
AE-8C1 Connectors Committee
Magnesium Alloy Castings, Sand, 6.0Al - 3.0Zn (AZ63-T6), Solution and Precipitation Heat TreatedAMS4424M (Current)10/23/2025
This specification covers a magnesium alloy in the form of sand castings (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Investment Castings, 7.0Si - 0.32Mg (356.0-T6), Solution and Precipitation Heat TreatedAMS4260H (Current)10/03/2025
This specification covers an aluminum alloy in the form of castings (see 8.6).
AMS D Nonferrous Alloys Committee
Steel, Corrosion-Resistant, Laminated, Sheet, Surface Bonded (SAE 302)AMS5500H (Current)10/03/2025
This specification covers a corrosion-resistant steel in the form of laminated sheet.
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy, Sheet, Strip, and Plate, 5Al - 2.5Sn, AnnealedAMS4910T (Current)10/20/2025
This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive, in thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 0.92Cr - 0.75Ni - 0.52Mo - 0.003B - 0.04V (98BV40), Aircraft QualityAMS6423K (Current)10/23/2025
This specification covers an 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, Mechanical Tubing and Forging Stock, 0.80Cr - 0.85Ni - 0.20Mo - 0.003B - 0.04V (0.38 - 0.43C) (98BV40 Mod), Aircraft QualityAMS6422M (Current)10/20/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Bolts and Screws, Steel, UNS S66286 Tensile Strength 130 ksi, Procurement SpecificationAS7477K (Current)12/17/2025
This document covers bolts and screws made from a corrosion- and heat-resistant, precipitation-hardenable, iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
E-25 General Standards for Aerospace and Propulsion Systems
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet and Strip, 52.5Ni - 19Cr - 3.0Mo - 5.0Cb (Nb) - 0.90Ti - 0.50Al - 18Fe (Inconel® 718SPF), Vacuum Induction and Consumable Electrode Remelted, Solution Heat Treated, Precipitation HardenableAMS5950E (Current)10/15/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet and strip 0.080 inch (2.03 mm) and under in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy Bars, Wire, Forgings, Flash-Welded Rings, and Drawn Shapes, 6Al - 4V AnnealedAMS4928X (Current)10/20/2025
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, and drawn shapes up through 10.000 inches (254.00 mm), inclusive, in diameter or least distance between parallel sides and stock of any size for forgings or flash-welded rings. Bar over 6.000 inches (152.40 mm) in nominal thickness has a maximum cross-sectional area of 288 square inches (1858 cm2). Forgings and flash-welded rings with nominal thicknesses over 6.000 inches (152.40 mm) have a maximum cross-sectional area of 79 square inches (509 cm2) (see 8.6).
AMS G Titanium and Refractory Metals Committee
Steel, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate, 13Cr - 2.0Ni - 3.0W (Greek Ascoloy), AnnealedAMS5508H (Current)10/15/2025
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
Titanium Alloy Bars and Forging Stock, 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo, Duplex AnnealedAMS6907D (Current)10/02/2025
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides and 32 square inches (206.46 cm2) maximum cross-sectional area and stock for forging of any size (see 8.7).
AMS G Titanium and Refractory Metals Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock, 5.8Mn - 17Cr - 5.8Ni - 2.0Cu - 0.26S (203 EZ), Free Machining, Solution Heat TreatedAMS5762H (Current)10/03/2025
This specification covers a free-machining, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400 °F, Lightweight, Hydraulic and Pneumatic (Supplement 1)AS1339SUP1A (Current)12/18/2025
This supplement forms a part of the Aerospace Standard AS1339, Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 3000 psi, 400°F, Lightweight, Hydraulic and Pneumatic, and shall be used to identify hose assembly standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Iron Alloy, Corrosion- and Heat-Resistant, Welding Wire, 31Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N (N-155), AnnealedAMS5794G (Current)10/03/2025
This specification covers a corrosion- and heat-resistant iron alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 1.2Cr - 3.2Ni - 0.12Mo (0.11 - 0.17C) (9315), Aircraft QualityAMS6263P (Current)10/23/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Copper Nickel Tin Alloy, Bars and Rods, 77Cu - 15Ni - 8Sn, Solution Annealed and Spinodal Hardened (TX02, formerly TX00)AMS4596C (Current)10/20/2025
This specification covers a copper-nickel-tin alloy in the form of bars and rods up to 8.500 inches (216 mm), inclusive, in nominal thickness. When tube is ordered to AMS4596, it shall be supplied to AMS4598 (see 8.8).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-O, Sheet and Plate), Annealed; or when specified, “As Fabricated” (2024-F)AMS4461C (Current)10/16/2025
This specification covers an aluminum alloy in the form of sheet and plate 0.008 to 1.000 inch (0.203 to 25.4 mm) thick, supplied in the annealed (O) temper (see 8.5). When specified, product shall be supplied in the “as fabricated” (F) temper (see 8.5).
AMS D Nonferrous Alloys Committee
Steel Bars, Forgings, Mechanical Tubing, and Forging Stock, 1.5Cr - 3.5Ni (0.07 - 0.13 C) (3310), Aircraft QualityAMS6250P (Current)10/23/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Tin Bronze Castings, Sand and Centrifugal, 87.5Cu - 10Sn - 2Zn, As CastAMS4845K (Current)10/23/2025
This specification covers a tin bronze in the form of sand and centrifugal castings (see 8.5).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Bars, Rods, and Wire, Rolled or Cold Finished, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-F), As Fabricated, or When Specified, Annealed (7075-O)AMS4186F (Current)10/02/2025
This specification covers an aluminum alloy in the form of bars, rods, and wire, in the sizes shown in 3.3.3, in the “as-fabricated (F) temper.” When specified, product shall be supplied in the annealed (O) condition (see 8.6).
AMS D Nonferrous Alloys Committee
Trimmable Horizontal Stabilizer Actuator Structural Load Path Integrity Monitoring PrinciplesAIR6226A (Current)12/17/2025
This SAE Aerospace Information Report (AIR) supplies information on trimmable horizontal stabilizer actuator structural load path integrity. It describes the different methods for detecting rupture or disconnection of load paths. It also describes the monitoring principle to compare existing solutions as a reference for its implementation in new aircraft programs.
A-6B3 Electro-Mechanical Actuation Committee
CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, SHIELDED (FOR MIL-C-81511 SERIES 3 CONNECTORS)AS39029/20C (Current)12/12/2025
AE-8C1 Connectors Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE CRES BRAID REINFORCED, 400 °F, 5080 PSI FLARELESS, 90° ELBOW TO 90° ELBOWAS5966C (Current)12/17/2025
SCOPE IS UNAVAILABLE.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Graphite Coating, Thin Lubricating Film, Impingement AppliedAMS2525F (Current)12/18/2025
This specification covers a coating consisting of finely powdered graphite in a heat-resistant inorganic binder applied to parts.
AMS B Finishes Processes and Fluids Committee
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