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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
Exterior Lighting Recommendations for Urban Air Mobility and Electric Vertical Takeoff and Landing AircraftARP7216 (Current)4/10/2026
This document covers external lighting for Electric Vertical Takeoff and Landing (E-VTOL) and Urban Air Mobility (UAM) vehicles. It discusses lights that may be installed both to meet regulatory requirements as well as for customer comfort and aircraft recognition. It also discusses the differences between UAM vehicles and other aircraft and how those differences impact the lighting.
A-20B Exterior Lighting Committee
J1939 Digital AnnexJ1939DA_202601 (Current)4/10/2026
This document is intended to supplement the J1939 documents by offering the J1939 information in a form that can be sorted and searched for easier use.
Truck and Bus Control and Communications Network Committee
INSERT ARRANGEMENTS, ELECTRIC CONNECTOR, SHELL SIZE 12 (FOR AS81703 CONNECTORS)AS33700C (Current)4/9/2026
AE-8C1 Connectors Committee
Aluminum Alloy, Rolled or Forged Rings, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T651, 7075-T652), Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat TreatedAMS4310G (Current)4/9/2026
This specification covers an aluminum alloy in the form of rolled or forged rings up to 6 inches (152 mm), inclusive, in thickness (see 3.3.1.1.1) and an OD to wall thickness ratio of 10 or greater (see 8.5).
AMS D Nonferrous Alloys Committee
Magnesium Alloy, Investment Castings, 8.7Al - 0.70Zn - 0.22Mn (AZ91C-T6), Solution and Precipitation Heat TreatedAMS4452G (Current)4/9/2026
This specification covers a magnesium alloy in the form of investment castings (see 8.6).
AMS D Nonferrous Alloys Committee
Steel Bars, Forgings, and Tubing, Nitriding, 1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C), (32CrMoNiV5), Double Vacuum Melted, Premium Aircraft-Quality for Bearing ApplicationsAMS6498C (Current)4/9/2026
This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6496 and AMS6497 cover UNS K23280 with other quality levels.
AMS E Carbon and Low Alloy Steels Committee
Motorcycle and Motor Driven Cycle Electrical System Maintenance of Design VoltageJ392_202005 (Current)5/26/2020
This SAE Recommended Practice pertains to electrical systems of motorcycles both with and without batteries.
Motorcycle Technical Steering Committee
Cleaner, Carpet Shampoo TypeAMS1630D (Current)11/22/2024
This specification covers a shampoo type carpet cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Tungsten Carbide-Cobalt PowderAMS7879G (Current)9/18/2025
This specification covers tungsten carbide-cobalt in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
Titanium Alloy, Bars, Forgings, and Flash-Welded Rings, 5.0Al - 2.5V - 4.0Sn - 1.0Co - 0.8Fe, Solution Heat Treated and AgedAMS6904 (Current)12/4/2025
This specification covers a titanium alloy in the form of bars, forgings, and flash-welded rings up to 4.500 inches (114.30 mm), inclusive, in nominal diameter or least distance between parallel sides and stock of any size for forging and flash-welded rings (see 8.6).
AMS G Titanium and Refractory Metals Committee
Headlamp CleanersJ2111_202008 (Current)8/26/2020
This SAE Recommended Practice provides test procedures, performance requirements, and guidelines for cleaners intended for use on motor vehicles.
Road Illumination Devices Standards Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, MODULES, ELECTRONIC, FEEDBACK TYPE, SIZES 20-3, 20-4, 20-5 VERTICAL MOUNTING WITH INTEGRAL BRACKET, BLOCK MOUNTING, SERIES IAS81714/30A (Current)2/24/2018
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, MODULES, FEEDBACK TYPE, SIZES 20-6, 20-7, 20-8 HORIZONTAL MOUNTING WITH INTEGRAL BRACKET, SERIES IAS81714/31A (Current)2/24/2018
AE-8C2 Terminating Devices and Tooling Committee
INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE II, CLASS 2, COMPOSITION C, FOR UNWIRED CONTACTSAS81969/30B (Current)5/28/2024
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, BUSSING MODULES, FEED THRU TYPE, SIZE 20, SERIES IAS81714/7A (Current)7/13/2022
AE-8C2 Terminating Devices and Tooling Committee
CRIMPING TOOL AND ACCESSORIES, REMOTE CRIMP HEAD, HYDRAULIC, WIRE SIZE 8 TO 00 UN-INSULATED AND 8 THRU 2 INSULATED CRIMP BARRELSAS5259/4A (Current)8/22/2025
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, BUSSING MODULES, FEED THRU TYPE, SIZE 12, SERIES IAS81714/9A (Current)7/13/2022
AE-8C2 Terminating Devices and Tooling Committee
CRIMPING TOOL, TERMINAL, HAND, ACTUATED, WIRE TERMINATION, IN-SERVICE INSPECTION GAGE FOR AS22520/5, /37, /38, AND /44 CRIMP TOOLSAS22520/39B (Current)10/13/2023
AE-8C2 Terminating Devices and Tooling Committee
CRIMPING TOOLS, TYPE 1, TERMINAL, HAND, WIRE TERMINATINO FOR MINIATURE CO-AXIAL AND TRI-AXIAL INNER CONTACTSAS22520/46A (Current)1/13/2023
AE-8C2 Terminating Devices and Tooling Committee
TOOL, CONNECTOR ASSEMBLY, FOR MIL-C-5015 CONNECTORSAS34801A (Current)1/18/2018
AE-8C2 Terminating Devices and Tooling Committee
Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing ProcessAMS7005 (Current)8/6/2025
This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
AMS AM Additive Manufacturing Metals
TERMINAL JUNCTION SYSTEM, BRACKET, BLOCK MOUNTING, SERIES IAS81714/29A (Current)7/13/2022
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, GROUNDING MODULES, STUD AND FLANGE TYPE MOUNTING, SERIES IIAS81714/63E (Current)7/6/2022
AE-8C2 Terminating Devices and Tooling Committee
INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE II, CLASS 1, COMPOSITION AAS81969/20A (Current)5/28/2024
AE-8C2 Terminating Devices and Tooling Committee
INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE II, CLASS 1, COMPOSITION CAS81969/3B (Current)5/28/2024
AE-8C2 Terminating Devices and Tooling Committee
Shield Termination, Solder Style, Insulated, Heat-Shrinkable, Environment Resistant General Specification forAS83519D (Current)12/13/2021
This specification covers environment resistant, heat-shrinkable solder type shield terminations. They may be used on data-bus, RF, and shielded cables in applications. Operating temperature of each product are as indicated on detail specifications.
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, BUSSING MODULES, FEEDBACK TYPE, SIZE 12, SERIES IAS81714/4A (Current)7/13/2022
AE-8C2 Terminating Devices and Tooling Committee
SHIELD TERMINATION, SOLDER STYLE, INSULATED, HEAT-SHRINKABLE, ENVIRONMENT RESISTANT WITH PREINSTALLED BRAID, CLASS 1, NON-ROHSAS83519/3B (Current)7/11/2025
AE-8C2 Terminating Devices and Tooling Committee
CRIMPING TOOL AND ACCESSORIES, INSPECTION GAGES, FOR AS5259 DIESAS5259/6C (Current)10/20/2025
AE-8C2 Terminating Devices and Tooling Committee
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, MODULES, ELECTRONIC, FEEDBACK TYPE, SIZE 16, SERIES IAS81714/19A (Current)2/24/2018
AE-8C2 Terminating Devices and Tooling Committee
CRIMPING TOOL, TERMINAL, HAND ACTUATED, WIRE TERMINATION, TYPE II, FOR FLAG SHAPE LUG TERMINAL SIZES 22-10AS22520/47 (Current)8/9/2024
AE-8C2 Terminating Devices and Tooling Committee
Steel, Maraging, Investment Castings 18.5Ni - 9.0Co - 5.0Mo - 0.70Ti - 0.12Al Vacuum Melted Homogenized, Overaged, and Solution Heat TreatedAMS5337E (Current)6/5/2022
This specification covers an alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Castings, Sand, 4cu 2ni 1.5mg 0.2cr, Solution Treated and OveragedAMS4220E (Current)11/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of November 1995.
AMS D Nonferrous Alloys Committee
Cloth, Nylon, MetallizedAMS3848B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Cord, Coreless, Para-Aramid Intermediate Modulus 4000 Lb (17,790 N), 75 Ft Per Lb (50 M/Kg)AMS3814/16A (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS P Polymeric Materials Committee
Aluminum Alloy, Sheet 4.4mg-0.70mn-0.15cr (5083-H323)AMS4057E (Current)2/1/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS D Nonferrous Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu Solution and Precipitation Heat Treated (H1075)AMS5659/H1075 (Current)9/14/2022
This specification covers a corrosion-resistant steel product 12 inches (305 mm) and under in nominal diameter, thickness or for hexagons, least distance between parallel sides, and having a maximum cross-sectional area of 144 square inches (930 cm2) in the solution and precipitation heat treated (H1075) condition.
AMS F Corrosion and Heat Resistant Alloys Committee
Copper-Beryllium Alloy, Bars and Rods, 98Cu - 1.9Be, Solution and Precipitation Heat Treated (TF00, formerly AT)AMS4533F (Current)1/27/2026
This specification covers a copper-beryllium alloy in the form of bars and rods (see 8.5).
AMS D Nonferrous Alloys 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
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
Copper-Nickel-Tin Alloy Plate, 77Cu - 15Ni - 8Sn, Solution Annealed and Spinodal Hardened (TX02, formerly TX00)AMS4595A (Current)11/13/2025
This specification covers a copper-nickel-tin alloy in the form of plate over 0.188 to 4.50 inches (4.77 to 114.3 mm) in nominal thickness (see 8.8).
AMS D Nonferrous Alloys Committee
Interior Decorative Clear Coating for Metal SurfacesAMS7200 (Current)2/10/2020
This specification establishes requirements for an interior decorative clear coating for wear protection of metal substrates.
AMS G8 Aerospace Organic Coatings Committee
Aluminum Alloy, 7075, Plate and Sheet (Improved Exfoliation Resistant)AMSQQA250/24C (Current)5/21/2021
This specification covers the specific requirements for aluminum alloy 7075 plate and sheet for applications requiring improved exfoliation resistance.
AMS D Nonferrous Alloys Committee
Nickel-Iron Alloy, Corrosion- and Heat-Resistant, Bars Forgings and Forging Stock, 12.5Cr - 42.5Ni - 6.0Mo - 2.7Ti - 0.015B - 34Fe (Incoloy® 901), Consumable Electrode Remelted or Vacuum Induction Melted, Solution, Stabilization, and Precipitation Heat TreatedAMS5660N (Current)11/13/2025
This specification covers a corrosion- and heat-resistant nickel-iron alloy in the form of bars and forgings 5 inches (127 mm) and under in nominal diameter or least distance between parallel sides and forging stock of any size.
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Plate 1.0mg 0.60si 0.28cu 0.25crAMS4053B (Current)3/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of March 1995. By this action, subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications.
AMS D Nonferrous Alloys 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
Titanium Alloy Bars, Wire, Forgings, and Rings, 6Al - 4V, Extra Low Interstitial, AnnealedAMS4930M (Current)11/13/2025
This specification covers a titanium alloy in the form of wire, forgings, flash-welded rings 4.000 inches (101.60 mm), inclusive, and under in nominal diameter or distance between parallel sides, bars up through 10.000 inches (254 mm), inclusive, and under in nominal diameter with a maximum cross-sectional area for bars over 4.000 to 10.000 inches (101.60 to 254 mm) in diameter of 79 square inches (509.7 cm2), and stock for forging or flash-welded rings of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 4 - Purchasing Specification for Film AdhesiveAMS6885/4 (Current)2/22/2021
This Purchasing Specification, AMS6885/4, specifies the batch release and delivery requirements for film adhesive used for repair. This specification is applicable only when the film adhesive is used as part of the repair system defined in AMS6885 and AMS6885/1. This specification also defines the procedure and requirements for storage life extension of materials purchased against this specification. It is only applicable for materials qualified against AMS6885 (refer to PRI-QPL-AMS6885), and shall be carried out within the responsibility of the purchaser and under control of its Quality organisation.
AMS CACRC Commercial Aircraft Composite Repair Committee
Silicone Compound, NATO Code Number S-736AMS8660A (Current)8/22/2025
This specification covers one type of a non-melting, heat-stable silicone compound, for use in high tension electrical connections, ignition systems, and electronics equipment, for application to unpainted mating threaded or non-threaded surfaces, and as a lubricant for components fabricated from elastomers. This compound is effective in the temperature range from -54 °C (-65 °F) to +204 °C (400 °F) for extended periods. This compound is identified by NATO symbol S-736 (see 6.5).
AMS M Aerospace Greases Committee
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