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ARINC 834A-1 Internet Protocol Based Aircraft Data Interface Function (ADIF)ARINC834A-1 (Current)7/2/2026
This standard defines the services, the transport layers, and the suggested security mechanisms to enable communication between aircraft systems and an Electronic Flight Bag (EFB). Herein is the definition of a set of protocols and services for the exchange of aircraft avionics data across aircraft networks. The purpose is to define a common set of services to be used to access specific avionics data that will enhance EFB applications. Supplement 1 introduces bi-directional communication between the EFB and FMS. It also enables mutual Transport Layer Security, incorporating client authentication.
Airlines Electronic Engineering Committee
Helicopter Engine-Rotor System CompatibilityARP704A (Current)7/2/2026
This SAE Aerospace Recommended Practice (ARP) recommends a methodology to be used for the design, analysis and test evaluation of modern helicopter gas turbine propulsion system stability and transient response characteristics. This methodology utilizes the computational power of modern digital computers to more thoroughly analyze, simulate and bench-test the helicopter engine/rotor system speed control loop over the flight envelope. This up-front work results in significantly less effort expended during flight test and delivers a more effective system into service. The methodology presented herein is recommended for modern digital electronic propulsion control systems and also for traditional analog and hydromechanical systems.
S-12 Powered Lift Propulsion Committee
Steel, Bars, Wire, and Forgings 10.5Mo - 6W - 3.75Cr - 2V (1.25 - 1.40C) Powder Metallurgy Product Hot Isostatically PressedAMS6558A (Current)5/16/2023
This specification covers a premium aircraft-quality, high-alloy steel gas-atomized and HIP-consolidated in the form of bars, wire, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings and Forging Stock, 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337), Aircraft QualityAMS6412R (Current)9/23/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Performance Rating of Lithium-Ion Battery ModuleJ1798/2_202412 (Current)12/5/2024
This document provides a recommended electrical performance testing guideline for LIBM, which makes up an xEV (Battery Electric Vehicles and Hybrid Electric Vehicles) battery pack system. This testing guideline may also be used for other applications, such as stationary, vessel, and aircraft. However, using the guideline for other applications should be determined by the users of this document. Users of this document may also be interested in conducting tests on battery cells and/or battery packs. To avoid conducting potentially redundant tests between cells, modules, and packs, this document does not specify which tests need to be conducted. Determination of which tests need to be conducted is at the user’s discretion and should be based on individual module applications. Rather than specifying which tests need to be conducted, this document describes how each test is to be conducted. This document provides a matrix of tests that can be selectively picked for the application
Battery Standards Testing Committee
Engine Rotation and Cylinder NumberingJ824_202206 (Current)6/29/2022
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry.
Engine Power Test Code Committee
Automatic Transmissions - Schematic DiagramsJ647_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
BOLT, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE, PD SHANK, CRES AMS5731 (UNS S66286), .1900-32 UNJF-3AAS3107B (Current)5/1/2026
E-25 General Standards for Aerospace and Propulsion Systems
Tubing, Carbon Steel (1025) (Aircraft Quality)AMST5066B (Current)7/1/2020
This specification covers carbon steel (1025) tubing of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
Steel, Welding Wire 1.75Mn - 0.78Cr - 2.8Ni - 0.85Mo - (0.09 - 0.12C) Vacuum Melted, Environment-Controlled PackagingAMS6469E (Current)10/26/2016
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock 1.05Cr - 0.55Ni - 1.0Mo - 0.11V (0.45 - 0.50C) (D6AC) Vacuum Consumable Electrode RemeltedAMS6431R (Current)3/9/2022
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
Aerospace Operator Self-Verification ProgramsARP9062A (Current)11/14/2006
Operator Self-Verification can apply to a variety of processes. The primary focus is on traditional manufacturing operations, but applications can be made wherever traditional inspection methods are employed. The practices recommended in this document are intended to identify the basic elements 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 overall efficiency and product quality to processes considered mature, as judged by the organization. Operator Self-Verification programs are not stand-alone processes, but augment existing quality management system standard requirements. The identified program elements are for voluntary organizational application, and are not intended for contractual flow-down unless otherwise
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Low Speed Thorax Impact Test Procedure for the HIII 50th Male DummyJ2779_202206 (Current)6/29/2022
Dummy Testing and Equipment Committee
TEE, FLARED TUBE, BULKHEAD UNIVERSAL ON SIDE, FOR SEAL RINGAS1253B (Current)10/19/2014
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel, Welding Wire 0.95Cr - 0.20V (0.28 - 0.33C) (SAE 6130)AMS6462K (Current)10/26/2016
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings, and Tubing 0.13 - 0.18C (SAE 1015)AMS5060K (Current)10/26/2016
This specification covers a low-carbon steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Steel, Maraging, Welding Wire 18Ni - 8.0Co - 4.9Mo - 0.40Ti - 0.10Al Vacuum Induction Melted, Environment Controlled PackagingAMS6501E (Current)6/3/2022
This specification covers a maraging steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Steel Strip (0.90 - 1.04C) (SAE 1095) Hard TemperAMS5122K (Current)10/20/2017
This specification covers a carbon steel in the form of strip.
AMS E Carbon and Low Alloy Steels Committee
Paste Adhesive for Core Restoration Part 1 - General RequirementsAMS2950/1 (Current)4/28/2026
This Technical Specification gives information about technical requirements and qualification procedures of adhesive paste with or without thickening agent for core restoration of aircraft components.
AMS CACRC Commercial Aircraft Composite Repair Committee
BOLT, MACHINE - HEXAGON HEAD, DRILLED 1 HOLE, PD SHANK, CRES AMS5731 (UNS S66286), .5625-18 UNJF-3AAS3113B (Current)5/1/2026
E-25 General Standards for Aerospace and Propulsion Systems
Low-Alloy Steel, Heat-Resistant, Bars, Forgings, Mechanical Tubing and Forging Stock 0.65Si - 1.25Cr - 0.50Mo - 0.25V (0.28 - 0.33C)AMS6302L (Current)3/20/2023
This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Tolerances Low-Alloy Steel Sheet, Strip, and PlateAMS2252E (Current)9/29/2021
This specification covers established inch/pound manufacturing tolerances applicable to low-alloy steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range.
AMS E Carbon and Low Alloy Steels Committee
NUT, SELF-LOCKING, DOUBLE HEXAGON, SOLID FILM LUBRICATED, COUNTERBORED, 160 KSI, 800 °F, UNS S66286AS3564F (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 4 - Purchasing Specification for Film AdhesiveAMS6885/4 (Current)5/7/2026
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
Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) Vacuum Consumable Electrode RemeltedAMS6414N (Current)3/1/2023
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
Steel, Bars, Forgings, and Tubing 1.6Si - 0.82Cr - 1.8Ni - 0.40Mo - 0.08V (0.38 - 0.43C) Consumable Electrode Vacuum RemeltedAMS6417K (Current)2/12/2021
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, Mechanical Tubing, Rings, and Stock for Forgings and Rings 1.0Cr - 7.5Ni - 4.5Co - 1.0Mo - 0.09V (0.29 - 0.34C) Consumable Electrode Vacuum Remelted, AnnealedAMS6526J (Current)3/2/2022
This specification covers a premium aircraft-quality, high-strength, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
AMS E Carbon and Low Alloy Steels Committee
Steel, Welding Wire 0.95Cr - 0.20V (0.28 - 0.33C) (SAE 6130) Vacuum Melted, Environment Controlled PackagingAMS6461L (Current)10/31/2016
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Chassis Dynamometer Simulation of Road Load Using Coastdown TechniquesJ2264_202301 (Current)1/13/2023
This procedure covers vehicle operation and electric dynamometer (dyno) load coefficient adjustment to simulate track road load within dynamometer inertia and road load simulation capabilities.
Light Duty Vehicle Performance and Economy Measure Committee
Recommended Green Racing ProtocolsJ2880_201406 (Current)6/4/2014
These Protocols can be used for all forms of motorsports; however, only certain combinations of Green Racing Elements will result in motorsport competitions that are recognized as Green Racing events. As new information, fuels and technologies emerge, addendums or new protocols will be developed. The SAE International (SAE) Motorsports Engineering Activity is also an invaluable source of reference materials and ongoing technical advice providing access to the constantly evolving set of best safety and operational practices for current and emerging technologies. This is especially true with regard to high voltage safety and the adoption of other advanced propulsion and fuel system technologies.
Green Racing Committee
J1979-DA, Digital Annex of E/E Diagnostic Test ModesJ1979DA_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
CABLE, POWER, ELECTRICAL, 600 VOLTS, PORTABLE, SINGLE CONDUCTOR, NON-OZONE RESISTANTAS5756/1C (Current)6/28/2023
AE-8D Wire and Cable Committee
573-7 Aircraft Integrated Data System Mark 2 (AIDS Mark 2)ARINC573-7 (Current)12/1/1974
This standard provides design guidance for the development and installation of an expandable Flight Data Acquisition and Recording System. The functions defined include flight data acquisition through suitable electrical interfaces, conversion of analog input signals into a standard serial data output and the capability for expansion to permit increased data handling capacity.
Airlines Electronic Engineering Committee
Shipping Caps, Torque Caps, and Body Plugs Ergonomic Design CriteriaUSCAR43 (Current)3/30/2015
This document describes the design and assembly force guidelines for conventional shipping caps, torque caps, and body plugs. All possible design and applications could not be anticipated in creating these guidelines. Where there are questions of adherence to this document, such as use of an “off-the-shelf” design, always consult the responsible Ergonomics Department.
USCAR
HOSE ASSEMBLY, POLYTETRAFLUORETHYLENE, PARA ARAMID REINFORCED, 275 °F, 4000 MAX PSI, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO STRAIGHTAS6013B (Current)4/17/2019
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
O-Ring Molded from AMS7276 Material, MetricMA3352A (Current)9/3/2019
A-6C2 Seals Committee
CONNECTOR, RECEPTACLE, ELECTRIC, SOLDER TYPE, JAM NUT MOUNTING, PUSH-PULL, COUPLING, SERIES 1 (CLASS E, P, J AND H)AS31341A (Current)5/19/2021
AE-8C1 Connectors Committee
Steel, Bars, Forgings, Rings, and Stock for Forging or Flash Welded Rings Aircraft Quality 0.95Cr - 0.20Mo (0.38 - 0.43C) (4140) AnnealedAMS6382S (Current)10/20/2023
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash-welded rings, and stock for forging or flash-welded rings.
AMS E Carbon and Low Alloy Steels Committee
Ship Systems and Equipment - Hydraulic System Design Criteria for Marine VehiclesJ1779_201305 (Current)5/30/2013
The marine environment differs greatly from other environments in which hydraulics are used. This Recommended Practice provides hydraulic design considerations and criteria for the marine environment and is applicable to commercial vessels, military ships, and submersible vehicles. This document may be used for manned and un-manned vehicles.
Ship Fluid Systems Committee
Titanium Alloy, Ti-6Al-4V, Hot Isostatically Pressed (Low Temperature, High Pressure), Produced by Laser Powder Bed FusionAMS7028 (Current)12/3/2024
This specification covers an alpha-beta Ti-6Al-4V alloy produced by laser powder bed fusion (L-PBF) additive manufacturing and subjected to hot isostatic press (HIP) operation. Typically, this material is used for complex-shaped aerospace products made to near net shape dimensions. These products have been used typically for parts requiring operating strength up to 750 °F (399 °C), but usage is not limited to such applications.
AMS AM Additive Manufacturing Metals
680 Aircraft Autonomous Distress Tracking (ADT)ARINC680 (Current)8/26/2019
This document describes the technical requirements, architectural options, and recommended interface standards to support an Autonomous Distress Tracking (ADT) System intended to meet global regulatory requirements for locating aircraft in distress situations and after an accident. This document is prepared in response to International Civil Aviation Organization (ICAO) and individual Civil Aviation Authorities (CAAs) initiatives.
Airlines Electronic Engineering Committee
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR AS81659 SERIES 2 CONNECTORS)AS39029/11D (Current)4/10/2024
AE-8C1 Connectors Committee
800P3-2 Cabin Connectors and Cables, Part 3, Specification of CablesARINC800P3-2 (Current)7/7/2025
This specification describes the general cable and wire characteristics recommended for use in cabin systems for commercial aircraft. Supplement 1 adds new definitions of 26 AWG 2-pair (Quad), 4-pair (Oct) data cables, and copper-fiber optic hybrid composite cables. Supplement 2 includes definitions of shielded twisted pair ethernet over single pair for data rates up to 1000Base-T1.
Airlines Electronic Engineering Committee
JAUS Transport ConsiderationsAIR5645A (Current)9/5/2014
This SAE Aerospace Information Report (AIR) discusses characteristics of data communications for the Joint Architecture for Unmanned Systems (JAUS). This document provides guidance on the aspects of transport media, unmanned systems and the characteristics of JAUS itself that are relevant to the definition of a JAUS transport specification.
AS-4JAUS Joint Architecture for Unmanned Systems Committee
Portable Measuring Devices/Systems for Maintenance Troubleshooting of Aircraft Cabin and Flight Deck Air Quality IssuesAS6923 (Current)12/13/2021
The purpose of this standard is to aid manufacturers in creating devices that will provide maintenance staff with objective, reliable data consistent with certain types of airborne contaminants (“sources”), captured either during an event or during maintenance troubleshooting on the ground, in both cases for post-flight interpretation on the ground.
AC-9M Cabin Air Measurement Committee
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), 140 KSI, .5000-20, UNJF-3AAS3172B (Current)9/18/2024
E-25 General Standards for Aerospace and Propulsion Systems
747-3 Flight Data RecorderARINC747-3 (Current)6/7/2011
This document provides design guidance for the development and installation of Flight Data Recorders (FDR) which may utilize solid state memory and which may employ some means of data compression. The Flight Data Recorder will be utilized with a Flight Data Acquisition Unit (FDAU) (ARINC Characteristic 573) or a Digital Flight Data Acquisition Unit (DFDAU) (ARINC Characteristic 717) to accommodate mandatory flight data recording and other flight data acquisition needs. The document provides guidance and information to ensure customer controlled interchangeability of equipment in a standard aircraft installation and in data retrieval. The system capability was expanded to accommodate a data bus speed of 1024 words per second.
Airlines Electronic Engineering Committee
628P8-1 Cabin Equipment Interfaces, Part 8, In-Flight Entertainment (IFE) Equipment Standard Availability Measurement GuidelinesARINC628P8-1 (Current)12/18/2009
Cabin equipment is required to operate with high standards of availability. This standard provides a standard methodology for measuring and calculating availability. Quantitative measurement guidelines are included.
Airlines Electronic Engineering Committee
Control of Water Carryover from the Environmental Control System and Condensation on the StructureAIR1204A (Current)10/3/2024
This Aerospace Information Report (AIR) outlines the design considerations and criteria for the control of water carryover from the environmental control system (ECS) with respect to causes and indicated corrective or preventative action. In addition, condensation on structure will be reviewed with possible preventative action described.
AC-9 Aircraft Environmental Systems Committee
792-2 Second-Generation Ku-Band and Ka-Band Satellite Communication SystemARINC792-2 (Current)8/25/2023
This standard sets forth the desired characteristics of a second-generation aviation Ku-band and Ka-band satellite communication (satcom) system intended for installation in all types of aircraft.
Airlines Electronic Engineering Committee
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