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Voltage Regulation and LimitsJ3226_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, 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, 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, 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, BOX MOUNTING FLANGE, PUSH-PULL COUPLING, SERIES 1 (CLASS E AND H)AS31321B (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
NUT - HEX, PORT FITTING CONNECTOR, AMS5639, MJ THREAD, METRICMA2521A (Current)9/1/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Silver Alloy, Brazing Filler Metal 45Ag - 24Cd - 16Zn - 15Cu 1125 to 1145 °F (607 to 618 °C) Solidus-Liquidus RangeAMS4769G (Current)12/8/2015
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips, and a viscous mixture (paste) of powder in a suitable binder.
AMS D Nonferrous Alloys Committee
Aluminum Alloy Sheet and Plate, Alclad 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (Alclad 6061; -T6 Sheet, -T651 Plate)AMS4023F (Current)10/15/2015
This specification covers an aluminum alloy in the form of sheet and plate.
AMS D Nonferrous Alloys Committee
NUT – SELF-LOCKING, CLINCH, SERRATED SHANK, 400 °C, DRY FILM COATED, UNS S66286, MJ THREAD, METRICMA3274A (Current)6/3/2019
E-25 General Standards for Aerospace and Propulsion Systems
Cobalt-Nickel Alloy, Corrosion and Heat-Resistant, Bars 19Cr - 36Co - 25Ni - 7.0Mo - 0.50Cb (Nb) - 2.9Ti - 0.20Al - 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated for Work StrengtheningAMS5841G (Current)2/3/2022
This specification covers a high strength, corrosion and heat-resistant cobalt-nickel-chromium alloy in the form of bars (see 8.4).
AMS F Corrosion and Heat Resistant Alloys Committee
NUT, SELF-LOCKING, DOUBLE HEXAGON REDUCED FLANGE, SOLID FILM LUBE COUNTERBORED 180 KSI, 1400 °F, UNS N07001AS3616A (Current)2/12/2024
E-25 General Standards for Aerospace and Propulsion Systems
Ethylene Propylene (EPDM) Rubber Hydrazine-Base-Fluid Resistant 75 - 85AMS3249D (Current)9/23/2011
This specification covers an ethylene propylene (EPDM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes other than O-rings.
AMS CE Elastomers Committee
COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS, ENVELOPE DIMENSIONS DESIGN STANDARDAS1711C (Current)6/26/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Thermoelectric Circuits and the Performance of Several Aircraft Engine ThermocouplesAIR65A (Current)5/7/2026
E-32 Aerospace Propulsion Systems Health Management
PORT - RING LOCKED FLUID CONNECTION TYPE STANDARD DIMENSIONS FORAS1300F (Current)3/5/2019
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35000 kPa), 400 °F (204 °C), Aircraft Hydraulic SystemsAS5960C (Current)4/11/2019
This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35000 kPa) aircraft hydraulic systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fuse, Current Limiter Type, AircraftAS5372A (Current)3/27/2023
This specification covers the requirements for current limiter type fuses for use in aircraft primary electrical power systems conforming to MIL-STD-704. These limiters are suitable for use in AS53731 fuse holders for operation at −54 to 125 °C.
AE-7P Protective and Control Devices
Sheet, Polyether Urethane (EU) Elastomer Foam Shock AbsorbingAMS3568B (Current)8/25/2011
This specification and its supplementary detail specifications cover a chemically or mechanically expanded polyether urethane (EU) elastomeric foam material in the form of ready-to-use sheet.
AMS P Polymeric Materials Committee
FITTING ASSEMBLY, TEE, AXIALLY SWAGED ON THE RUN, FEMALE FLARELESS ON THE BRANCH, HYDRAULIC, 3000 PSIAS5806B (Current)5/5/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic SystemsARP4925B (Current)10/9/2014
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a commercial transport rotorcraft hydraulic system, including the applicable airworthiness regulations that affect the hydraulic system. This ARP also provides information and guidelines on the many factors that arise in the design process to provide cost effectiveness, reliability, maintainability and accepted design and installation practices.
A-6A1 Commercial Aircraft Committee
Minimum Performance Standard for Parts 23, 27, and 29 Aircraft Wheels, Brakes, and Wheel and Brake AssembliesAS5714A (Current)9/8/2022
This SAE Aerospace Standard (AS) prescribes the Minimum Performance Standards (MPS) for wheel, brake, and wheel and brake assemblies to be used on aircraft certificated under 14 CFR Parts 23, 27, and 29. Compliance with this specification is not considered approval for installation on any aircraft.
A-5A Wheels, Brakes and Skid Controls Committee
Handbook of Hydraulic Metric CalculationsAIR1657C (Current)5/18/2021
This SAE Aerospace Information Report (AIR) provides details of how to perform hydraulic system calculations using equations that incorporate the metric International System of Units (SI).
A-6 Aerospace Actuation, Control and Fluid Power Systems
Elastomer: Silicone, Rubber (MQ/VMQ) General Purpose 65 – 75 Durometer Type ‘A’ HardnessAMS3304J (Current)4/5/2019
This specification covers a silicone (MQ/VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, AMS7268 should be used.
AMS CE Elastomers Committee
Steel, Welding Wire, 0.50Cr - 0.55Ni - 0.20Mo (0.18 - 0.23C) (SAE 8620), Vacuum Melted, Environment Controlled PackagingAMS6375F (Current)3/4/2026
This specification covers a low-alloy steel in the form of welding wire. Type 2 - copper coated wire was removed from this document (see 8.4).
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy 7178, Plate and SheetAMSQQA250/14B (Current)2/14/2014
This specification covers the specific requirements for 7178 aluminum alloy plate and sheet material; the general requirements are covered in AMS-QQ-A-250.
AMS D Nonferrous Alloys Committee
Steel Wire, Copper Clad, Round 99Fe - 0.32Mn AnnealedAMS7732D (Current)11/15/2012
This specification covers a low-carbon steel in the form of round wire clad with electrolytic copper.
AMS E Carbon and Low Alloy Steels Committee
RING, RETAINING SPIRAL, INTERNAL, HEAVY DUTY, CRES (UNS S30200)AS3215B (Current)5/10/2023
E-25 General Standards for Aerospace and Propulsion Systems
Canister, Lithium Hydroxide, Screened Ends, Friction Type CoversAS210041 (Current)2/13/2002
This specification covers canisters for shipment and storage of lithium hydroxide (LiOH), to be used in receptacle for CO2 absorbent (see MIL-R-24159).
Aerospace Council
Stand, Shipboard, Helicopter MaintenanceAS85376 (Current)11/6/2017
This specification covers a helicopter maintenance stand used by personnel aboard aviation capable ships.
AGE-2 Air Cargo
Guidelines for Specifying Linear and Rotary Variable Differential TransformersARP5554 (Current)4/1/2024
This SAE Aerospace Recommended Practice (ARP) provides guidelines for specifying Linear Variable Differential Transformers (LVDTs) and Rotary Variable Differential Transformers (RVDTs). Information on the application, operation, design, and construction of LVDTs and RVDTs is also provided.
A-6B1 Hydraulic Servo Actuation Committee
COUPLING, MALE, 12 INCH AIR DUCTAS7365/3A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
COOLING DATA FOR TURBINE ENGINES IN HELICOPTERSARP996A (Current)3/27/2025
A tested method of data presentation and use is described herein. The method shown is a useful guide, to be used with care and to be improved with use.
S-12 Powered Lift Propulsion Committee
In-Service Fiber Optic Inspection, Evaluation and Cleaning, Best Practices, Physical Contact TerminiARP6283 (Current)10/7/2024
This document provides recommended best practice methods and processes for the in-service inspection, evaluation and cleaning of all physical contact (PC) fiber optic interconnect components (termini, alignment sleeves and connectors), test equipment and test leads for maintainers qualified to the approved aerospace fiber optic training courses developed in accordance with ARP5602 or ARINC807. This document also provides a decision-making disposition flowchart to determine whether the fiber optic components are acceptable for operation. For definitions of individual component parts refer to ARP5061.
AS-3 Fiber Optics and Applied Photonics Committee
Titanium 6 - Aluminum 4 - Vanadium Powder for Additive Manufacturing, Extra Low Interstitial (ELI)AMS7017 (Current)4/7/2022
This specification covers a titanium alloy in the form of pre-alloyed powder.
AMS AM Additive Manufacturing Metals
Iron, Electrical, Bar and Strip Cold Finished, AnnealedAMS7713C (Current)1/13/2016
This specification covers electrical iron in the form of bar and strip.
AMS E Carbon and Low Alloy Steels Committee
Balancing Machines – Description and Evaluation Vertical, Single-Plane, Non-Rotating Type for Gas Turbine RotorsARP6217 (Current)8/13/2025
Characteristics of vertical non-rotating balancing machines are described which make such machines suitable for balancing rigid unbladed gas turbine rotors or rotors with fixed, integral blades.
EG-1A Balancing Committee
FITTING ASSEMBLY, STRAIGHT, EXTENDED BULKHEAD SHANK, FLARELESS, AXIALLY SWAGED, HYDRAULIC, 5080 PSIAS6106B (Current)5/5/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
PIN, STRAIGHT, HEADLESS, AMS5688, LOCKAS9105A (Current)1/9/2015
E-25 General Standards for Aerospace and Propulsion Systems
Commercial Aircraft Hydraulic System SizingARP6277 (Current)1/26/2021
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guidelines for determining the hydraulic flow demands for all phases of commercial flight including details of sizing of associated hydraulic components such as hydraulic pumps, hydraulic accumulators, hydraulic reservoirs, hydraulic filters, and hydraulic tubing.
A-6A1 Commercial Aircraft Committee
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)AMSS6758B (Current)11/30/2017
This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
Copper-Beryllium Alloy (Copper Alloy Numbers C17500 and C17510), StripAS81021B (Current)5/20/2026
This specification covers the requirements for the acquisition of two alloys of copper-beryllium alloy strip, having higher electrical conductivity than copper-beryllium alloy strip normally used (see 6.1). All sizes of strip are covered by this specification.
AMS D Nonferrous Alloys Committee
INSERT - CRES HELICAL COIL FINE THREAD, STRAIGHT, STUD LOCKING, 3 DIA NOM LENGTHAS3083A (Current)4/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
CLAMP, RECTANGULAR LOOP, CUSHIONED, WITH WEDGE, HIGH TEMPERATURE, STAINLESS STEEL, METRICMA2155/5 (Current)4/27/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Landing Gear ServicingARP5908A (Current)3/28/2025
The present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber (also known as dual stage and two stage) shock struts. This document should be considered as landing gear industry recommended practice but in no way is meant to supersede the shock strut OEM’s published procedures.
A-5B Gears, Struts and Couplings Committee
WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYMIDE INSULATED, SMOOTH SURFACE, LIGHT WEIGHT, SILVER-COATED HIGH STRENGTH OR ULTRA HIGH STRENGTH COPPER ALLOY, 200 °C, 600 VOLTS ROHSAS22759/181A (Current)12/18/2019
AE-8D Wire and Cable Committee
WIRE, THERMOCOUPLE, FP/POLYIMIDE/FP INSULATED, NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, LIGHT WEIGHT, 260 °CAS5419/6A (Current)12/7/2018
AE-8D Wire and Cable Committee
STEEL WIRE, CORROSION RESISTANT 17Cr - 7.1Ni - 1.1Al Precipitation Hardenable, Spring TemperAMS5673D (Current)7/1/1982
AMS F Corrosion and Heat Resistant Alloys Committee
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