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CONNECTOR, RECEPTACLE, ELECTRIC THRU BULKHEAD, WALL MOUNTING FLANGE, SERIES I (CLASS E)AS31391A (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, 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
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
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
Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For (Supplement 1)AS85421SUP1A (Current)7/7/2026
This supplement forms a part of SAE Aerospace Specification AS85421. It shall be used to identify fitting standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Measurement of Exhaust Sound Levels of Stationary SnowmobilesJ2567_202607 (Current)7/6/2026
This SAE Standard establishes the test procedure, environment, and instrumentation for determining the sound levels of snowmobiles in the stationary test mode. This test method is intended to provide an accurate measurement of exhaust and other engine noise and may be used to evaluate new and in-use snowmobiles to determine compliance with noise control regulations. Sound level measurements obtained with this test method are not intended as an engineering determination of overall machine noise. For this purpose, the use of SAE J192 is recommended.
Snowmobile Technical Committee
Un-Shielded Balanced Single Twisted Pair Ethernet CableJ3117_202307 (Current)7/10/2023
This document covers un-shielded balanced single twisted pair data cable intended for use in surface vehicle cables for 100 Mbps Ethernet applications. The tests in this document are intended to qualify cables for normal operation in an automotive environment while maintaining the necessary electrical properties for reliable data transmission.
Cable Standards Committee
Steering Ball Studs and Socket AssembliesJ491_201210 (Current)10/15/2012
This SAE Recommended Practice has been established for the purpose of providing design criteria and suggested dimensional proportions which may be used for ball studs and ball stud socket assemblies as used on steering systems or control mechanisms of passenger vehicles, trucks and off-road equipment. The recommended practice does not cover all applications. It is intended to provide assistance in obtaining functional satisfaction and interchangeability. The inclusion of dimensional data in this report is not intended to imply that all the products described are stock production sizes. Consumers are requested to consult with manufacturers concerning stock production parts.
Materials, Processes and Parts Council
Use of Terms Yield Strength and Yield PointJ450_201710 (Current)10/10/2017
The purpose of this SAE Recommended Practice is to describe the terms yield strength and yield point. Included are definitions for both terms and recommendations for their use and application.
Metals Technical Committee
COUPLING, FEMALE, 12 INCH AIR DUCTAS7365/2A (Current)6/11/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Unshielded High Voltage Primary CableJ1654_202107 (Current)7/1/2021
This SAE Standard covers unshielded cable, 22 gauge and larger, intended for use at a nominal system voltage up to 600 V or 1000 V (ACrms or DC). It is intended for use in surface vehicle electrical systems.
Cable Standards Committee
CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, ENVIRONMENT RESISTANT, REMOVABLE CRIMP CONTACTS, PLUG (SERIES A)AS29600/12B (Current)1/27/2026
AE-8C1 Connectors Committee
HFC-134a (R-134a) Recovery/Recycle/Recharging Equipment for Mobile Air-Conditioning SystemsJ2788_202602 (Current)2/12/2026
The purpose of this SAE Standard is to establish the specific minimum equipment performance requirements for recovery and recycling of HFC-134a that has been directly removed from, and is intended for reuse in, mobile air-conditioning (A/C) systems. It also is intended to establish requirements for equipment used to recharge HFC-134a to an accuracy level that meets Section 9 of this document and SAE J2099. The requirements apply to the following types of service equipment and their specific applications: a. Recovery/recycling equipment b. Recovery/recycling - refrigerant charging c. Refrigerant recharging equipment only
Interior Climate Control Service Committee
CLAMP, CENTER MOUNT, BARE METAL, ALUMINUM, METRICMA2152/1 (Current)4/27/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
TS95AR-10 Amendment Record for Technical Specification No. TS95TS95AR-10 (Current)2/19/2020
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
NUT, SELF-LOCKING, PLATE, TWO LUG, LOW HEIGHT, UNS S66286, CLASS: 125 KSI/800 °FAS3478E (Current)6/12/2026
E-25 General Standards for Aerospace and Propulsion Systems
Composite Electrical ConnectorsAIR4567C (Current)1/27/2026
This SAE Aerospace Information Report (AIR) establishes guidelines for evaluating composite electrical connectors and accessories.
AE-8C1 Connectors Committee
Wire, Steel, High Carbon, Round, Type IIIAMSQQW428/2B (Current)8/1/2017
AMS E Carbon and Low Alloy Steels Committee
Lessons Learned from Developing, Implementing, and Operating a Health Management System for Propulsion and Drive Train SystemsAIR1871C (Current)1/19/2017
SAE Aerospace Information Report AIR1871 provides valuable insight into lessons learned in the development, implementation, and operation of various health monitoring systems for propulsion engines and drive train systems. This document provides an overview of the lessons learned for ground-based systems, oil debris monitoring systems, lubrication systems, and Health and Usage Monitoring Systems (HUMS) for military and commercial programs. For each case study, this document presents a brief technical description, the design requirements, accomplishments, lessons learned, and future recommendations. The lessons learned presented in this document represent a fragment of the knowledge gained through experience when developing and implementing a propulsion health management system. Previous versions of this document contain additional lessons learned during the 1980’s and 1990’s that may be of additional value to the reader. This document will be maintained as technology progresses so that
E-32 Aerospace Propulsion Systems Health Management
Aerospace - General Requirements for Hydraulic Fuse - Quantity MeasuringAS5466 (Current)6/24/2024
This specification establishes the design, performance, and test requirements for hydraulic quantity measuring fuses intended to be used for hydraulic circuit protection.
A-6C5 Components Committee
Test Facility Shakedown and CommissioningAIR6364 (Current)11/29/2017
The paper discusses in general terms the activities required to be undertaken or demonstrated during the establishment of the facility such as: the assessment checks prior to forwarding to the end users site for embodiment into the facility system the establishment of the facility such as trial installations of hardware, functionality checking of lifting transportation and access systems, centerline pull checks, pressure testing of fuel and air start systems, flushing of wet systems and electrical continuity checking. the commissioning of the facility such as instrumentation calibrations, engine starts, engine running, assessment of command and control system, assessment of DAS system, aerodynamic and acoustic surveys. The paper will concentrate on the main engineering engine related aspects of the facility and will not necessarily contain information on the construction validation activities such as HVAC, electrical, facility fire system, waste water etc. Risk analysis may be
EG-1E Gas Turbine Test Facilities and Equipment
A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education Introduction to Aerospace Fiber Optics Hands-on CompetenciesARP5602/2 (Current)10/23/2025
This document establishes training guidelines applicable to fiber optic safety training, technical training and fiber awareness for individuals involved in the manufacturing, installation, support, integration and testing of fiber optic systems. Applicable personnel include: Managers Engineers Technicians Logisticians Trainers/Instructors Third Party Maintenance Agencies Quality Assurance Shipping Receiving Production Purchasing
AS-3 Fiber Optics and Applied Photonics Committee
Silver Alloy, Brazing Filler Metal 35Ag - 26Cu - 21Zn - 18Cd 1125 to 1295 °F (607 to 702 °C) Solidus-Liquidus RangeAMS4768J (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
AS6021 Aerospace Fiber Optic Cable Assembly Drawing SpecificationAS6021A (Current)12/29/2020
This SAE Aerospace Standard (AS) defines the items that shall be considered when creating a fiber optic cable assembly specification and source control drawing intended for installation on aerospace platforms.
AS-3 Fiber Optics and Applied Photonics Committee
E/E Diagnostic Test Modes: OBDonUDSJ1979-2_202604 (Current)4/21/2026
SAE J1979-2 describes the communication between the vehicle’s OBD systems and test equipment required by OBD regulations. OBD regulations require passenger cars and light-, medium-, and heavy-duty trucks to support a minimum set of diagnostic information to external (off-board) “generic” test equipment.
Vehicle E E System Diagnostic Standards Committee
Fuel Pump Thermal Safety DesignARP594F (Current)10/18/2022
The requirements presented in this document address the key considerations for thermal safety in aircraft fuel pump design. Document sections focus on understanding safety relative to an electrically motor driven fuel pump assembly acting as an ignition source for explosive fuel vapors within the airplane tank.
AE-5B Aircraft and Engine Fuel and Lubricant Sys Components
Heat Treatment, Carbon, Low-Alloy and Specialty SteelsAMS2760A (Current)1/1/1987
This specification covers the procedure for through-hardening and related heat treatments of carbon, low-alloy, and specialty steel parts to produce specified mechanical properties within the capability of each respective steel. Heat treating processes such as induction hardening, flame hardening, carburizing, nitriding, austempering, and martempering are recognized processes but are not covered by this specification.
AMS E Carbon and Low Alloy Steels Committee
CLAMP, LOOP TYPE, CUSHIONED SUPPORT, METRICAS14241 (Current)11/4/2014
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
850 System Level Guidance for Data Loading LRU Target SystemsARINC850 (Current)1/12/2024
This document provides LRU Target System manufacturers, airframe manufacturers, and others with principles, concepts, and guidance for the design of data loading targets and complex data loading target systems. The mechanisms described in this paper apply to federated LRUs and complex platforms, such as airborne servers and data loading of IMA systems. The document guides data loading system design for Target Systems: How to avoid common pitfalls during the system/software design architectural design phase Specific considerations to actively decide on in early conceptual design phases Increase of useability and robustness for the end-user and maintainer of data loading targets This document focuses on reaching common design objectives for Target System data loading systems and circumventing repeatedly occurring issues rooted in system design. Commonly desired design objectives include: Architectural choices – Simplify the upload process of LRU Target Systems of the same type Reducing
Airlines Electronic Engineering Committee
Determination of Brake Fluid TemperatureJ291_201304 (Current)4/9/2013
This code provides a test procedure for obtaining and determining extremely high brake fluid temperature encountered in the brake system of a vehicle that is equipped with disc brakes. Vehicles in normal operation may or may not produce brake fluid temperatures that are obtained in this procedure.
Road Test Procedures Standards Committee
Cooling System Nonmetallic Caps and Filler Necks - Threaded ConstructionJ3096_202604 (Current)4/1/2026
This SAE Recommended Practice was developed primarily for passenger car and truck applications but may be used in marine, industrial, and similar applications. It addresses nonmetallic caps and both metallic and nonmetallic filler necks.
Cooling Systems Standards Committee
PWM HVAC Blower Controller and BLDC Motor Controller Efficiency AssessmentJ3109_202306 (Current)6/13/2023
The intention of this standard is to establish a framework to measure the efficiency of PWM HVAC Blower Controllers and Brushless DC Motor Controllers and define a usage based overall efficiency. This result can then be used by vehicle OEMs to demonstrate compliance towards requirements or benchmarks established by regulatory agencies.
Interior Climate Control MAC Supplier Committee
COVER FOR USE WITH MS90362 EXTERNAL POWER RECEPTACLEAS35051A (Current)12/3/2021
AE-8C1 Connectors Committee
DIMENSIONAL STANDARD FOR CYLINDRICAL HYDRAULIC COUPLERS FOR AGRICULTURAL TRACTORSJ1036_199304 (Current)3/3/2001
This SAE Standard specifies the essential interface dimensions, the installation dimensions, and the operating requirements for hydraulic couplers employed to transmit hydraulic power from agricultural tractors to agricultural implements and farmstead equipment as defined in SAE J1150.
Agricultural Tractor Standards Committee (ATSC)
Dynamic Ozone Test Procedure--Hydraulic Brake HoseJ1914_198803 (Current)6/1/1988
The purpose of this recommended practice is to evaluate in the laboratory the effect of flexing on a brake hose when exposed to a high ozone concentration environment. This recommended practice is intended for all vehicle hydraulic brake hoses. It is an accelerated test which subjects the hose to dynamic ozone exposure.
Automotive Brake and Steering Hose Standards Comm
Steel, Bars, Wire, and Forgings 9V - 5.25Cr - 1.3Mo (1.80 - 1.95C) Powder Metallurgy Product Hot Isostatically PressedAMS6557A (Current)5/16/2023
This specification covers a premium aircraft-quality, high-alloy tool steel gas-atomized and HIP consolidated in the form of bars, wire, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
NUT, SELF-LOCKING, PLATE, ONE LUG, REDUCED RIVET SPACING, LOW HEIGHT, UNS S66286, CLASS: 125 KSI/800 °FAS3480E (Current)6/12/2026
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Corrosion-Resistant, Wire, 18Cr - 9.0Ni (302), Spring TemperAMS5688N (Current)6/1/2026
This specification covers a corrosion-resistant steel in the form of wire.
AMS F Corrosion and Heat Resistant Alloys Committee
FITTING, BULKHEAD END - THREADED COUPLING, RIGID, SELF-BONDING, DESIGN STANDARDAS5948A (Current)5/15/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING END, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING MALE AND FEMALE DESIGN STANDARDAS5836 (Current)1/9/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CLAMP, LOOP TYPE, CUSHIONED SUPPORTAS5874 (Current)4/23/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
COUPLING BODY, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDINGAS5835 (Current)1/9/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
INSERT - THIN WALL, SHORT AND LONG HOLE PREPARATION FORAS3508A (Current)1/31/2026
E-25 General Standards for Aerospace and Propulsion Systems
Adhesive, Film Form Metallic Structural Sandwich ConstructionAMSA25463 (Current)10/4/2022
This specification covers the requirements for adhesives in film form for bonding metal facings to metal cores and to metal components of sandwich panels which are intended for use in primary and secondary structural airframe parts that may be exposed to temperatures up to 500°F (260°C).
AMS P17 Polymer Matrix Composites Committee
Titanium Alloy, Investment Castings 6Al - 4V Hot Isostatically PressedAMS4962B (Current)12/6/2016
This specification covers a premium grade titanium alloy in the form of investment castings.
AMS G Titanium and Refractory Metals Committee
Determination of Cost Benefits from Implementing a Blockchain SolutionARP6984 (Current)8/19/2021
This SAE Aerospace Recommended Practice (ARP) provides insights on how to perform a Cost Benefit Analysis (CBA) to determine the Return on Investment (ROI) that would result from implementing a blockchain solution to a new or an existing business process. The word “blockchain” refers to a method of documenting when data transactions occur using a distributed ledger with desired immutable qualities. The scope of the current document is on enterprise blockchain which gives the benefit of standardized cryptography, legal enforceability and regulatory compliance. The document analyzes the complexity involved with this technology, lists some of the different approaches that can be used for conducting a CBA, and differentiates its analysis depending on whether the application uses a public or a private distributed network. This document is intended for people who do not have a deep technical understanding or familiarity with blockchain solutions to qualify and quantify its economic benefits
G-31 Digital Transactions for Aerospace
Failure Mode and Effects Analysis (FMEA) Includes Criticality Analysis and Design, Supportability, Software, and Process FMEASAE1025 (Current)1/1/2026
FMEA is a systematic approach aimed at identifying and mitigating potential risks in the design, manufacture, and maintenance of a product. Implementing FMEA provides a range of benefits, such as: Preventing potential failures early in the life cycle. Identifying risk - establishing clear linkages ensures that no potential failure mode is overlooked across the life cycle of the product. Improving product safety, reliability, performance, and supportability. Enhancing collaboration - the framework fosters cross-functional communication, enabling design, manufacturing, and maintenance teams to work in harmony. Achieving effectiveness - by integrating analyses and plans, organizations can streamline workflows and reduce redundancies. Reducing costs associated with product failures. Enhancing customer satisfaction through consistent quality and reliability. Improving product quality - comprehensive linkage reduces errors and ensures a robust design and manufacturing process. Providing the
G-41 Reliability
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