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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, 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
Propeller Control Clearance - Single Acting System Single Rotation Propeller Shaft Reciprocating EnginesARP237B (Current)2/5/2013
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Bars, Forgings, Mechanical Tubing and Forging Stock, 0.50Cr - 0.55Ni - 0.20Mo (0.18 - 0.23C) (SAE 8620), Premium Aircraft Quality, Vacuum Arc or Electroslag RemeltedAMS6277K (Current)9/25/2025
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
Impulse Testing of Hydraulic Hose, Tubing and Fitting AssembliesMA2002B (Current)11/12/2013
This standard establishes the requirements and the procedures for impulse testing of hose assemblies, tubing, and fittings for use in aerospace metric hydraulic systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
R-1234yf [HFO-1234yf] Refrigerant Electronic Leak Detectors, Minimum Performance CriteriaJ2913_202501 (Current)1/21/2025
This SAE Standard provides testing and functional requirements to meet specified minimum performance criteria for electronic probe-type leak detectors. The equipment specified here will identify smaller refrigerant leaks when servicing motor vehicle air conditioning systems, including those engineered with improved sealing and smaller refrigerant charges to address environmental concerns and increase system efficiency. This document does not address any safety issues concerning the equipment design or use beyond that of sampling a flammable refrigerant, save those described in 3.1 and 3.2 of this document. All requirements of this standard shall be verified in SAE J2911.
Interior Climate Control Service Committee
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSS LINKED MODIFIED ETFE, LIGHTWEIGHT, SILVER COATED, EXTRA HIGH STRENGTH COPPER ALLOY, 200 °C, 600 VOLT, ROHSAS22759/55A (Current)8/10/2021
AE-8D Wire and Cable Committee
CABLE, LOW INDUCTANCE, 270 VOLT DCAS5756/7B (Current)7/15/2021
AE-8D Wire and Cable Committee
Air Cargo Unit Load Devices – Load Distribution ModelAS36101A (Current)9/7/2011
This SAE Aerospace Standard (AS) defines an industry agreed reference model for load distribution on air cargo unit load device (ULD) bases, to reflect maximum allowable center of gravity (CG) eccentricity and ensure the maximum allowable area load is not exceeded.
AGE-2 Air Cargo
Propeller Clearance EnvelopeARP166B (Current)2/5/2013
E-25 General Standards for Aerospace and Propulsion Systems
Direct Delivery Authorization Guidance for Aerospace CompaniesAS9107 (Current)6/12/2026
Limited to the commercial aerospace industry where a request is made for a PO to have Direct Delivery Authorization (DDA), which includes an Appropriate Arrangement (AA) between the PO and the Design Organization (DO). In this process, the DO is responsible for ensuring the continuous updating of approved design data to the PO, whilst the PO is responsible for assurance that the manufactured article conforms to approved design data. The PO is responsible to provide airworthiness release documentation.
SAE Committee
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General RequirementsAMS6885/1 (Current)6/10/2026
AMS6885/1 gives information about the technical requirements and qualification procedure for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The repair system includes an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
Supportive Information Report for the Fuel Economy Measurement Test (Engineering Type) for Trucks and BusesJ1420_199712 (Current)12/2/1997
This information report is a companion document to SAE Recommended Practice J1376, Fuel Economy Measurement Test (Engineering Type) for Trucks and Buses. It provides background information and explanations to better understand the measurement procedure and its use. It also provides references and data which were developed by the SAE/DOT Program in support of the particular limitations or parameters selected for the various items in the test procedure. The format used in this document is similar to the recommended practice so that corresponding topics can be found under the same headings.
Truck and Bus Aerodynamics and Fuel Economy Committee
NUT, SELF-LOCKING, EXTENDED DOUBLE HEXAGON, REDUCED FLANGE, DRY FILM LUBE, UNS S66286, CLASS: 160 KSI/800 °FAS3486E (Current)6/12/2026
E-25 General Standards for Aerospace and Propulsion Systems
STRAIGHT THREAD TUBE FITTING BOSS O-RING MOLDED FROM AMS-P-83461 ACRLONITRILE BUTADIENE (NBR) RUBBERAS83461/2D (Current)6/10/2021
A-6C2 Seals Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE METAL BRAID, MEDIUM PRESSURE, FLARED, 45° TO 90°AS644B (Current)7/12/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Recommended Testing Methods for Physical Protection of Wiring HarnessesJ2192_202606 (Current)6/18/2026
This SAE Recommended Practice describes the recommended methods for testing flexible harness coverings for use on ground vehicle electrical distribution systems. It shall apply to all tapes, extruded tube, and textile tube.
Harness Covering Standards Committee
1992 Visual Simulation for General Flight Simulator/Trainer AttachmentAIR771 (Current)6/1/1992
G-10G Realistic Training Committee
Inertia Dynamometer Brake Squeal Noise Test Procedure for Vehicles with Regenerative SystemsJ3211_202512 (Current)12/1/2025
The SAE J3211 procedure applies to squeal evaluation for foundation brakes using single-ended inertia dynamometers for friction couples used on vehicles with regenerative braking systems. This document applies to squeal noise occurrences for on-road passenger cars and light trucks with a gross vehicle weight rating of 4536 kg or below and with at least one rechargeable energy storage system as a source for propulsion. The procedure incorporates aspects related to (a) minimum inertia dynamometer capabilities, (b) fixture requirements and setup, and (c) test sequences with emphasis on brake temperatures, brake pressure profiles, and strategies to represent brake blending. For this document, squeal occurs when the peak noise level is at least 70 dB(A) between 1.25 and 16 kHz for tests using full suspension corners or complete axle assemblies, or between 2 and 16 kHz for brakes not using an entire suspension corner. Test facilities intending to use this document, building on their
Brake NVH Standards Committee
TITANIUM ALLOY SHEET AND STRIP 4Al - 3Mo - 1V Solution and Precipitation TreatedAMS4913A (Current)10/1/1991
AMS G Titanium and Refractory Metals Committee
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR MIL-DTL-83527, CONNECTOR)AS39029/93D (Current)1/28/2026
AE-8C1 Connectors Committee
AS48900-999 BOLT, DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, .3125-24 UNJF-3AAS48900-4 (Current)12/1/2025
Scope is unavailable.
Engine and Airframe Technical Standards Committee (TSC)
Aluminum Alloy Powder 10.0Si - 0.35MgAMS7018 (Current)5/11/2020
This specification covers an aluminum alloy in the form of pre-alloyed powder.
AMS AM Additive Manufacturing Metals
RING, RETAINING, EXTERNAL, INTERLOCKINGAS90708C (Current)3/20/2023
E-25 General Standards for Aerospace and Propulsion Systems
COUPLING, V-RETAINER, DOUBLE LATCH, TYPE II LOW PROFILEAS1895/20H (Current)6/18/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Coupling Assembly, V-Retainer, High Pressure, High Temperature, Pneumatic TubeAS1895G (Current)6/17/2026
This SAE Aerospace Standard establishes the requirements for a V-retainer coupling, flanges, and seal suitable for joining high-pressure and high-temperature ducting in aircraft bleed air systems. The rigid coupling joint assembly, hereafter referred to as “the joint,” shall operate within the temperature range of -65 to +1200 °F.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CONNECTOR, RECEPTACLE, SQUARE FLANGE, REVERSE BAYONET COUPLING, BOX MOUNT, FRONT, NO ACCESSORY THREADAS95234/2A (Current)11/15/2023
AE-8C1 Connectors Committee
TAPE, NYLON, LOOPAMS3784A (Current)1/1/1993
AMS P Polymeric Materials Committee
Fiberboard, SolidAMS3560A (Current)4/1/1984
AMS P Polymeric Materials Committee
Plastic Tubing, Electrical Insulation, Resin Bonded-Polyethylene Terephthalate, Heat Shrinkable 1.3 to 1 Shrink RatioAMS3589 (Current)10/1/1984
AMS P Polymeric Materials Committee
Heavy Vehicle Event Data Recorder (HVEDR) - Data and TriggersJ2728-1_202006 (Current)6/9/2020
This document provides a list of data elements and event triggers for recording of event data relevant to crash investigations for heavy vehicles. The list of data elements includes recommended source(s) and formatting.
Truck and Bus Event Data Recorder Committee
Tachometer Generator EnvelopesAIR82 (Current)1/6/1976
A-4 Aircraft Instruments Committee
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR AS81659 SERIES 2 CONNECTORS)AS39029/11D (Current)4/10/2024
AE-8C1 Connectors Committee
Hydraulic Tube FittingsJ514_202411 (Current)11/22/2024
This SAE Standard covers complete general and dimensional specifications for 37 degree flared and flareless types of hydraulic tube fittings and O-ring plugs. Also included are pipe fittings and adapter unions for use in conjunction with these tube fittings. These fittings are intended for general application in hydraulic systems on industrial equipment and commercial products. These fittings are capable of providing leakproof, full flow connections in hydraulic systems operating at working pressures as specified in Table 1 for respective sections. Since many factors influence the pressure at which a hydraulic system will or will not perform satisfactorily, the values shown in SAE J1065 should not be construed as a guaranteed minimum. For any application, it is recommended that sufficient testing be conducted and reviewed by both the user and fitting manufacturer to assure that performance levels will be safe and satisfactory.
Hydraulic Tube Fittings Committee
Human Interface Criteria for Flight Deck Surface Operations DisplaysARP5898A (Current)12/22/2020
Following a number of high-visibility collisions between aircraft on the airport surface, overall taxi operations have been brought under greater scrutiny. In addition, observation of taxi operations and the results of associated research programs have revealed that the efficiency of taxi operations could be significantly improved with available technologies and by applying a human centered design approach. Surface operations displays have been tested in prototype form and a number of manufacturers are moving toward product definition. This document provides guidance on the design of elements, which may be part of surface operations displays whose objectives would be to enhance safety and to improve overall efficiency of aircraft operations on the airport surface. Such efficiency increases should be realized not only in day-to-day operations, but should also be manifested in training for surface operations. This document sets forth functional and design recommendations concerning the
G-10EAB Executive Advisory Group
Perfluoroether ElastomerAMS7254B (Current)5/7/2014
This specification covers a perfluoroether elastomer in the form of molded rings.
AMS CE Elastomers Committee
Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Short Application Life, Durometer 35 - 55AMS3364D (Current)1/17/2012
This specification covers a silicone rubber in the form of a two-component liquid compound.
AMS G9 Aerospace Sealing Committee
ELBOW ASSEMBLY, 45°, RETAINED NUT, SHORT FLARELESSAS4667B (Current)6/26/2017
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel Bars, Corrosion and Heat Resistant 20cr 9ni 1.6mo 1.4w 0.6tiAMS5729 (Current)1/1/1987
AMS F Corrosion and Heat Resistant Alloys Committee
Test and Test Procedures for SAE 100R Series Hydraulic Hose and Hose AssembliesJ343_202310 (Current)10/5/2023
This SAE Standard gives methods for testing and evaluating performance of the SAE 100R series of hydraulic hose and hose assemblies (hose and attached end fittings) used in hydraulic fluid power systems. Specific tests and performance criteria for evaluating hose assemblies used in hydraulic service are in accordance with the requirements for hose in the respective specifications of SAE J517. This document further establishes a uniform means of testing and evaluating performance of hydraulic hose assemblies.
Hydraulic Hose and Hose Fittings Committee
Keyless Ignition Control DesignJ2948_201101 (Current)1/13/2011
This SAE Recommended Practice establishes guidelines for the operation of automotive keyless ignition systems with the goal of helping to minimize user instigated errors. For the purpose of this Recommended Practice, user instigated errors may include: the inability to start and stop the vehicle propulsion system, exiting the vehicle with the automatic transmission in a non-parking gear, exiting the vehicle while the vehicle propulsion system is enabled, exiting the vehicle while the vehicle propulsion system is disabled, but the accessory or electrical systems are active. To help minimize these errors, this Recommended Practice contains design recommendations pertaining to uniform labeling, operating logic, indication of vehicle ignition/control status, and physical control characteristics of keyless ignition systems. This Recommended Practice applies to keyless ignition controls permanently mounted in passenger cars, MPVs, and trucks 10 000 GVWR and under. It does not apply to remote
Controls and Displays Standards Committee
Ship Systems and Equipment - Hydraulic Systems - Filter Selection ParametersJ2333_201305 (Current)5/31/2013
This SAE Recommended Practice identifies and examines the various parameters which must be considered in selecting hydraulic system filters, their locations within the system and the dirt capacity of the filter elements.
Ship Fluid Systems Committee
Phosphor Bronze, Sheet, Strip, and Plate, 94.5Cu - 4.0Sn - 0.19P, Spring Temper (H08)AMS4510K (Current)6/15/2026
This specification covers a copper alloy (phosphor bronze) in the form of sheet, strip, and plate (see 8.6).
AMS D Nonferrous Alloys Committee
HUB, FLANGED - SPLINE TYPE WOOD PROPELLER - #10, #20ARP381B (Current)2/5/2013
E-25 General Standards for Aerospace and Propulsion Systems
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