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Items (221,567)

J3226_202607 (Current)

7/10/2026

This document defines the test procedures and performance limits of steady state and transient voltage characteristics for 12 V, 24 V, or 48 V electrical power generating systems used in commercial ground vehicles.

Truck and Bus Electrical Systems Committee

CONNECTOR, RECEPTACLE, ELECTRIC, DUMMY STOWAGE, WALL MOUNTING FLANGE, PUSH-PULL COUPLING (SERIES 1 AND 2 CONNECTORS)

AS31351B (Current)

7/9/2026

AE-8C1 Connectors Committee

CONNECTOR, RECEPTACLE, ELECTRIC, SOLDER TYPE, WALL MTG. FLANGE, PUSH-PULL COUPLING, SERIES 1 (CLASS E, P, AND J)

AS31301B (Current)

7/9/2026

AE-8C1 Connectors Committee

CONNECTOR, RECEPTACLE, ELECTRIC, BOX MOUNTING FLANGE, PUSH-PULL COUPLING, SERIES 1 (CLASS E AND H)

AS31321B (Current)

7/9/2026

AE-8C1 Connectors Committee

CONNECTOR, RECEPTACLE, ELECTRIC, SOLDER TYPE, JAM NUT MOUNTING, PUSH-PULL, COUPLING, SERIES 1 (CLASS E, P, J AND H)

AS31341B (Current)

7/9/2026

AE-8C1 Connectors Committee

CONNECTOR, RECEPTACLE, ELECTRIC THRU BULKHEAD, WALL MOUNTING FLANGE, SERIES I (CLASS E)

AS31391A (Current)

7/9/2026

AE-8C1 Connectors Committee

CONNECTOR, PLUG, ELECTRIC, SOLDER TYPE LANYARD, PUSH-PULL COUPLING, SERIES 1 (CLASS E, P, AND J)

AS31381B (Current)

7/8/2026

AE-8C1 Connectors Committee

Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock, 0.50Cr - 0.12Mo (0.89 - 1.01C)

AMS6476G (Current)

7/8/2026

This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging or tubing stock.

AMS E Carbon and Low Alloy Steels Committee

J1979-DA, Digital Annex of E/E Diagnostic Test Modes

J1979DA_202510 (Current)10/20/2025

The SAE J1979 document set includes the communication between the vehicle's On-Board Diagnostic (OBD) systems and test equipment implemented across vehicles within the scope of regulated emissions and propulsion related OBD. The SAE J1979 Digital Annex supplements the J1979 base documents primarily by maintaining a global registry of regulated emissions and propulsion related data identifiers.

Vehicle E E System Diagnostic Standards Committee

FITTING ASSEMBLY, TEE, AXIALLY SWAGED ON THE RUN, INTERNAL PORT END ON THE SIDE, HYDRAULIC, UP TO 1500 PSI

AS6446A (Current)

3/1/2024

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

SCREW, MACHINE - HEXAGON HEAD, PD SHANK, TITANIUM AMS4967 (UNS R56400), .1380-40 UNJF-3A

AS9631A (Current)

3/4/2019

E-25 General Standards for Aerospace and Propulsion Systems

WIRE, THERMOCOUPLE, FP/POLYIMIDE/FP INSULATED, NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, NORMAL WEIGHT, 260 °C

AS5419/7A (Current)

12/7/2018

AE-8D Wire and Cable Committee

Silicone (VMQ) Rubber Sheet, Glass Cloth Reinforced

AMS3315G (Current)

2/9/2012

This specification covers silicone (VMQ) rubber sheet reinforced with glass cloth.

AMS P Polymeric Materials Committee

Shims, Molded, Filled Resin Compound and Sheet Prepeg

AMSS83474B (Current)

7/6/2016

This specification covers the requirements for filled, resinous thermosetting compound and sheet pre-preg to fabricate shims for use during assembly of aircraft and marine components and parts.

AMS P Polymeric Materials Committee

Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution Heat Treated

AMS5399D (Current)

11/3/2023

This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.

AMS F Corrosion and Heat Resistant Alloys Committee

Aluminum and Aluminum Alloy, Bar, Rod, Wire, or Special Shapes; Rolled, Drawn, or Cold Finished; General Specification For

AMSQQA225C (Current)

1/4/2018

This specification covers the general requirements for aluminum and aluminum alloy bar, rod, wire, or special shapes; rolled, drawn, or cold finished. Specific requirements for these products are covered by the applicable detail specification (See 6.3).

AMS D Nonferrous Alloys Committee

Coatings, Cadmium, Tin-Cadmium and Zinc (Mechanically Deposited)

AMSC81562A (Current)

1/18/2018

This specification covers the requirements for three types and three classes of mechanically deposited cadmium, tin-cadmium or zinc coatings on metallic surfaces by impacting (peen plating).

AMS B Finishes Processes and Fluids Committee

Design and Operating Requirements of the Onboard Aircraft Refueling System and Associated Ground Refueling Equipment Interface

AS5751 (Current)

10/2/2023

This SAE Aerospace Specification (AS) is applicable to all aircraft. This AS defines the minimum design and operating requirements for the aircraft refueling interface. These requirements establish the minimum criteria for the aircraft design that provides practical standardized refueling system requirements, provides minimum standardized criteria for the operation and performance of any aircraft refueling equipment, and establishes an integrated minimum performance for aircraft refueling operations. This standardization provides the minimum design criteria to assure full compatibility between the aircraft refueling system connection point(s), aircraft operating characteristics, and the design and operation of ground based aircraft refueling equipment in all steady state and dynamic refueling and defueling conditions. The criteria that shall be used to test the operation and performance of the aircraft refueling system and equipment are also specified. Compliance to this AS shall be

AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee

Steel Bars and Forgings 3.5Cr - 7.5Ni - 16.3Co - 1.75Mo - 0.2W - (0.09 - 0.13C) Double Vacuum Melted, Normalized, Annealed

AMS6509B (Current)

9/30/2022

This specification covers a premium aircraft-quality alloy steel in the form of bars and forgings 199 square inches (1284 cm2) and under in cross section, and forging stock of any size.

AMS E Carbon and Low Alloy Steels Committee

Gamma Titanium-Aluminide Powder for Additive Manufacturing Ti - 48Al - 2Nb - 2Cr

AMS7023 (Current)

6/1/2021

This specification covers a heat-resistant gamma titanium aluminide alloy in the form of pre-alloyed powder.

AMS AM Additive Manufacturing Metals

SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN, .1900-32 UNF-3A

AS115801C (Current)

11/11/2020

E-25 General Standards for Aerospace and Propulsion Systems

Aerospace Operator Self-Verification Programs

ARP9162A (Current)3/28/2017

The focus of Operator Self-Verification is on traditional manufacturing operations, and applications can be made wherever traditional inspection is employed. The practices recommended in this document are intended to identify the basic elements and provide a “guideline” for structuring Operator Self-Verification programs within the aerospace industry; applicable to producers of commercial and military aircraft and weapons platforms, space vehicles, and all related hardware, software, electronics, engines and composite components. Operator Self-Verification programs are applied to improve the overall efficiency and product quality of processes considered mature, as judged by the implementing organization. Operator Self-Verification programs are not stand-alone processes, but augment existing quality management systems. The identified program elements are for voluntary implementation by the organization, and are not intended for contractual flow-down unless otherwise stipulated through

G-14 Americas Aerospace Quality Standards Committee (AAQSC)

Guide to the Application and Use of Engine Coolant Pump Face Seals

J1245_200210 (Current)10/25/2002

SAE IC Powertrain Steering Committee

AS70003 Ring, Tube, Welding (Metric & Inch Tube Series)

AS70003-1 (Current)8/11/2017

No Scope available.

Engine and Airframe Technical Standards Committee (TSC)

Plating, Tin-Lead (Electrodeposited)

AMSP81728C (Current)

5/24/2023

This specification covers the requirements for electrodeposited tin-lead plating intended for use as a coating for corrosion protection and as a base for soldering.

AMS B Finishes Processes and Fluids Committee

Maintenance of Ground Support Equipment

AIR4286 (Current)

2/12/2026

The following are suggested policies, procedures, and practices required to maintain mobile and fixed ground support equipment at airport passenger and cargo terminals. The principal purpose for ground support equipment maintenance is to provide the owner/user with safe, serviceable equipment, in good appearance, at minimal cost, and with minimum downtime. Maintenance programs initiated on ground support equipment must also conform to regulations controlling airport operations. This document has been divided into three sections corresponding to the three stages of equipment life; acquisition, maintenance, and disposal.

AGE-3 Aircraft Ground Support Equipment Committee

Requirements for Oversight of Aerospace Quality Management System Registration/Certification Programs

AS9104/2A (Current)

6/13/2014

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)

Sealing Compound, Polysulfide For Aircraft Windshields and Canopies, For Use up to 250 °F (121 °C)

AMS3333B (Current)

1/17/2012

This specification covers types and classes of polysulfide sealing compound supplied as a two-component system suitable for application by brush, or by extrusion gun, spatula brush, or roller.

AMS G9 Aerospace Sealing Committee

Insulation Blanket, Thermal-Acoustical

AMSI7171A (Current)

9/23/2011

This specification covers the requirements of composite blankets suitable for acoustical and thermal insulation of the walls of aircraft compartments within the temperature range of -65°F to +175°F (-54°C to +80°C).

AMS CE Elastomers Committee

BOLT, MACHINE, DOUBLE HEX, EXTENDED WASHER HEAD, CLOSE TOL. SHANK, UNS N07718, 185 KSI MIN, .1900-32 UNJF-3A (STRESS RUPTURE RESISTANT)

AS3417C (Current)

8/19/2022

E-25 General Standards for Aerospace and Propulsion Systems

Steel Carburizing and Nitriding, Processes for

AMSS6090B (Current)

5/15/2006

This specification presents requirements for the carburizing and nitriding of carbon and alloy steels to produce the mechanical properties specified by drawings, detail metal specifications, or other applicable specifications (see 6.3).

AMS E Carbon and Low Alloy Steels Committee

CABLE, ELECTRIC, FILTER LINE, SMALL DIAMETER COMPONENT WIRE, TIN-COATED COPPER CONDUCTOR, RADIO FREQUENCY, ABSORPTIVE, 150 °C, 600-VOLT

AS85485/9B (Current)

7/15/2021

AE-8D Wire and Cable Committee

Automatic Transmissions - Schematic Diagrams

J647_202512 (Current)

12/1/2025

The following schematic diagrams reflect various methods of illustrating automotive transmission arrangements. These have been developed to facilitate a clear understanding of the functional interrelations of the gearing, clutches, hydrodynamic drive unit, and other transmission components. Two variations of transmission diagrams are used: in neutral (clutches not applied) and in gear. For illustrative purposes, some typical transmissions are shown.

Automatic Transmission and Transaxle Committee

INSTALLATION, JOINT, 40° V-BAND COUPLING AND NARROW SHEET METAL FLANGES

AS1960/5A (Current)

12/5/2024

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Steel, Nitriding, Bars, Forgings, Mechanical Tubing, and Stock for Forging, 1.6Cr - 0.35Mo - 1.13Al (0.38 - 0.43C) (135 Mod), Premium Aircraft Quality, Consumable Electrode Vacuum Remelted

AMS6471K (Current)

12/26/2023

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

Titanium Alloy, Investment Castings 6Al - 4V 130 UTS, 120 YS, 6% EL Hot Isostatically Pressed Anneal Optional or When Specified

AMS4985E (Current)

11/21/2018

This specification covers a titanium alloy in the form of investment castings.

AMS G Titanium and Refractory Metals Committee

Acceptance Criteria for Nuts - Magnetic Particle, Fluorescent Penetrant, and Visible Penetrant Examination

AS5447A (Current)

4/1/2024

This standard establishes the acceptance criteria for surface discontinuities as revealed by magnetic particle or liquid penetrant examination of nuts.

E-25 General Standards for Aerospace and Propulsion Systems

Performance, Nut, Self-Locking, Castellated, Prevailing Torque, UNJ 16 Pitch Thread Form

AS4958B (Current)

1/16/2024

This document covers all metal, castellated, self-locking nuts made from alloy steel of the types identified under the Unified Numbering System as UNS G41300 and UNS G43400.

E-25 General Standards for Aerospace and Propulsion Systems

Aerospace Vehicle Wiring, Lessons Learned

AIR6808A (Current)

3/4/2024

This AIR is limited to the requirements of AS50881 and examines these requirements, providing rationale behind them. AS50881 is only applicable to the aircraft EWIS. Pods and other devices that can be attached to an aircraft are considered as part of the aircraft equipment design. Its scope does not include wiring inside of airborne electronic equipment but does apply to wiring externally attached to such equipment. The AS50881 scope does not include attached devices but does include the interface between the pod/equipment and aircraft wiring. Section 3.3.5 addresses components such as antennas and other similar equipment that were once supplied as Government Furnished Aeronautical/Aerospace Equipment (GFAE).

AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install

HOSE ASSEMBLY, RUBBER, FLARELESS, FIELD ATTACHABLE FITTING, 45° TO 45°

AS1866A (Current)

9/17/2024

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

WIRE, THERMOCOUPLE, FLUOROPOLYMER INSULATED, EXTRUDED TFE NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, 260 °C

AS5419/5A (Current)

12/7/2018

AE-8D Wire and Cable Committee

Terms, Definitions, and Acronyms Counterfeit Materiel or Electrical, Electronic, and Electromechanical Parts

AIR6273 (Current)

7/30/2019

The SAE Aerospace Information Report (AIR) provides standardized terms, definitions, and acronyms that may be used in the G-19 and G-21 documents, unless otherwise specified in those documents. The SAE International series of documents that address the mitigation of suspect and counterfeit parts will reference this document in their respective Applicable Documents sections. This AIR is for use by organizations that procure and/or use materiel or EEE parts. The terms and definitions of this AIR are intended to be used in conjunction with other G-19 and G-21 standards.

G-19 Counterfeit Electronic Parts Committee

SCREW, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE, PD SHANK, CRES AMS5731(UNS S66286), .1640-36 UNJF-3A

AS3106B (Current)

4/30/2026

E-25 General Standards for Aerospace and Propulsion Systems

Validation Methods For MIL-STD-1760D Mission Stores

AS42701 (Current)

9/29/2014

This document establishes techniques for validating that a mission store complies with the interface requirements contained in MIL-STD-1760 Revision D.

AS-1B Aircraft Store Integration Committee