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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 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
BOSS - PLUG/PIN, EXPANSION TYPE HOLE PREPARATIONAIR3276A (Current)2/19/2026
E-25 General Standards for Aerospace and Propulsion Systems
Aluminum Alloy 2219, Plate and SheetAMSQQA250/30A (Current)12/12/2013
This specification covers the specific requirements for 2219 aluminum alloy plate and sheet.
AMS D Nonferrous Alloys Committee
Unmanned Systems (UxS) Control Segment (UCS) Architecture: EA Version of UCS ICD ModelAIR6515A (Current)2/23/2024
This User Guide describes the content of the Enterprise Architect (EA) version of the UCS Architectural Model and how to use this model within the EA modeling tool environment. The purpose of the EA version of the UCS Architectural Interface Control Document (ICD) model is to provide a working model for Enterprise Architect tool users and to serve as the source model for the Rational Software Architect (RSA) and Rhapsody models (AIR6516 and AIR6517). The AIR6515 EA Model has been validated to contain the same content as the AS6518 model for: all UCS ICD interfaces all UCS ICD messages all UCS ICD data directly or indirectly referenced by ICD messages and interfaces the Domain Participant, Information, Service, and Non-Functional Properties Models
AS-4UCS Unmanned Systems Control Segment Architecture
ARP4754B Clarification NoticeAIR4757 (Current)6/11/2026
The purpose of this AIR is to provide additional information on some areas of ARP4754B/ED-79B that may need additional clarification in order to be put into practice. This document should be used in conjunction with ARP4754B/ED-79B. The contents are recommendations and should not be construed to be regulatory requirements. This document may be revised with additional information as ARP4754B/ED-79B is put into practice.
S-18 Aircraft and Sys Dev and Safety Assessment Committee
Tolerances Carbon and Alloy Steel TubingAMS2253F (Current)2/24/2018
This specification covers established inch/pound manufacturing tolerances applicable to carbon and alloy tubing 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
Fused Filament Fabrication, Material forAMS7101A (Current)7/8/2022
This specification establishes the minimum requirements for fused filament fabrication (FFF) feedstock.
AMS AM Additive Manufacturing Non-Metallic
Steel Bars, Forgings, and Tubing, Nitriding 1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C) Electroslag Remelted or Consumable Electrode Vacuum Remelted Premium Aircraft-Quality for Bearing ApplicationsAMS6497B (Current)11/28/2018
This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6496 and AMS6498 cover UNS K23280 with other quality levels.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T6151) Solution Heat Treated, Stress Relieved, and AgedAMS4306C (Current)1/12/2018
This specification covers an aluminum alloy in the form of plate.
AMS D Nonferrous Alloys Committee
Polytetrafluoroethylene Film General Purpose GradeAMS3662D (Current)5/13/2015
This specification covers one grade of polytetrafluoroethylene resin in the form of film.
AMS P Polymeric Materials Committee
Rubber: Acrylonitrile-Butadiene (NBR) Fuel-Resistant 60 - 70 Type A HardnessAMSP5315C (Current)8/5/2022
This specification covers an acrylonitrile-butadiene (NBR) rubber in the form of molded rings, molded compression seals, molded O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications.
AMS CE Elastomers Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings Ni - 18Cr - 2.8Mo - 5.5Cb(Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W Consumable Electrode Remelted or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat TreatedAMS5442B (Current)8/4/2022
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and flash welded rings up to 5.0 inches (127mm) in least nominal cross-sectional dimension having a cross-sectional area not greater than 50 in2 (323 cm2), and stock of any size for forging or flash welded rings (see 8.5).
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Welding Wire 0.88Cr - 1.8Ni - 1.6Co - 0.42Mo - 0.08V (0.28 - 0.33C) (SAE 4330V) Vacuum Melted, Environment Controlled PackagingAMS6473B (Current)9/1/2006
This specification covers a low-alloy steel in the form of welding wire. This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of September, 2006. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
AMS E Carbon and Low Alloy Steels Committee
Microspheres, Hollow GlassAMS3751C (Current)1/16/2012
This specification covers hollow glass microspheres.
AMS P Polymeric Materials Committee
Silicone (PVMQ) Rubber Extreme-Low-Temperature Resistant 55 - 65AMS3336E (Current)11/7/2011
This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Flux, Aluminum Brazing for Torch or Furnace BrazingAMS3412F (Current)8/9/2021
This specification covers the requirements for an aluminum brazing flux in the form of powder or paste.
AMS B Finishes Processes and Fluids Committee
LIGHT, DESK, AIRCRAFTAS7768/1B (Current)11/9/2020
A-20C Interior Lighting
WIRE, ELECTRIC, CROSSLINKED POLYALKENE INSULATED, SILVER-COATED HIGH STRENGTH COPPER ALLOY, MEDIUM WEIGHT, 600 VOLT, 150 °CAS81044/10A (Current)7/29/2022
AE-8D Wire and Cable Committee
FITTING ASSEMBLY, CROSS, AXIALLY SWAGED, HYDRAULIC, 5080 PSIAS5973B (Current)6/2/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
GASKET, METAL C-RING, FACE SEAL, INTERNAL PRESSURE, UNS N07750, SILVER PLATED, METRICMA2536A (Current)9/19/2018
E-25 General Standards for Aerospace and Propulsion Systems
Regional Aircraft Towbarless Tow Vehicle - Test RequirementsARP5911A (Current)3/30/2022
The present Aerospace Recommended Practice specifies for airplane operator and tow vehicle manufacturers the basic testing requirements for towbarless tow vehicles to be used on the nose gear of conventional tricycle type landing gears of commercial civil transport aircraft with maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as “regional aircraft”. Its purpose is to achieve testing results, or equivalent computer modeling, demonstrating that the loads induced by the tow vehicle will not exceed the design loads of the airplane’s nose landing gear and associated structure, reduce the certified safe life limit of the nose landing gear, or otherwise compromise the airplane’s structural integrity and airworthiness certification.
AGE-3 Aircraft Ground Support Equipment Committee
CABLE ASSEMBLY, EXTERNAL ELECTRIC POWER, AIRCRAFT 28 VOLT DC, OPERATING POWERAS90347C (Current)9/11/2023
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
Fluid for Automotive Electrified DrivetrainsJ3200_202210 (Current)10/13/2022
This SAE Information Report details the important new performance properties and suggested test methods for lubricants used in e-Mobility drivetrain components. The lubricants under discussion are those used in electrified drivetrains, mainly electric-transmissions and axles (e-transmissions and e-axles). The scope is limited to those geared systems in which an electric motor (e-motor) is immersed in the powertrain lubricant or comes in contact with the powertrain lubricant. Though the report focuses on new lubricant attributes, some information on conventional lubricant attributes is included. The information presented here will be helpful in understanding the similarities and differences between conventional (i.e., internal combustion engine (ICE)) and e-Mobility powertrain systems.
Fuels and Lubricants TC 3 Driveline and Chassis Lubrication
RING, LOCK, SERRATEDAS51990C (Current)2/10/2020
E-25 General Standards for Aerospace and Propulsion Systems
Procedure for the Calculation of Non-Volatile Particulate Matter Sampling and Measurement System Losses and System Loss Correction FactorsARP6481A (Current)9/9/2024
This SAE Aerospace Recommended Practice (ARP) details the recommended process for correcting measured non-volatile particulate matter (nvPM) mass and number data for particle losses in the sampling and measurement system specified in ARP6320B. This technique is only recommended for conditions where both nvPM mass and number concentration measurements are in the valid measurement ranges of the instruments that are discussed in the tool limitations section. This ARP also supplies an Excel software tool with documentation to automate the process. The body of this ARP details the recommended calculation method, uncertainties, and limitations of the system loss correction factors. It explains, in detail, the required inputs and outputs from the supplied Excel software tool (developed on Windows 7, Excel 2016). Also included are: The Excel correction tools (refer to Attachments I and V). Installation instructions for a Windows-based computer (refer to Attachment II). A user technical manual
E-31P Particulate Matter Committee
Coupling Assembly, V-Band Sheet Metal Wide Flange, Pneumatic TubeAS4751A (Current)10/21/2025
This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems. The rigid coupling joint assembly, hereafter referred to as “the joint”, shall operate within the temperature range of -65 °F external ambient to +800 °F internal fluid.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Minimum Design and Performance of Airplane Galley In-Flight Carts, Containers, and Associated ComponentsAS8056A (Current)10/16/2025
This SAE Aerospace Standard (AS) establishes minimum design and performance requirements for carts, containers, and associated components intended for installation in galleys and other areas of transport category airplanes. The requirements include establishing installation criteria for use by compartment designers and installers of the equipment.
S-9B Cabin Interiors and Furnishings Committee
Pass-Thru Extended Feature - Resource DocumentJ2534-2/RE_0500_202201 (Current)1/17/2022
This SAE Recommended Practice is part of the SAE J2534-2/X_0500 set of documents that extends the SAE J2534-1_0500 API (version 05.00) specification. It defines the common data structures and constants that will be used to implement the extension to the SAE J2534 API. This document will only include the items that are used by the V05.00 API and that are NOT included in SAE J2534-1_0500. It will not include items from older API versions unless they are used by the V05.00 API.
Vehicle E E System Diagnostic Standards Committee
Thermophysical Properties of the Natural Environment, Gases, Liquids, and SolidsAIR1168/9A (Current)7/25/2011
This AIR is arranged in the following four sections: 2A - Properties of the Natural Environment 2B - Properties of Gases 2C - Properties of Liquids 2D - Properties of Solids A summary of each section is given below.
AC-9 Aircraft Environmental Systems Committee
CUSHION, LOOP CLAMP, MULTIPLE, 2-TUBE, AMS3303AS9393A (Current)10/13/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
ALUMINUM ALLOY SHEET, CLAD TWO SIDES 0.6Mg - 0.35Si - 0.28Cu (No. 22-0 Brazing Sheet) AnnealedAMS4055C (Current)1/1/1987
This specification covers an aluminum alloy in the form of sheet.
AMS D Nonferrous Alloys Committee
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, DRILLED, CLOSE TOL SHANK, AMS5643 (UNS S17400), 140 KSI, .1900-32 UNJF-3AAS3174B (Current)9/10/2019
E-25 General Standards for Aerospace and Propulsion Systems
CONNECTORS, RECEPTACLE, ELECTRICAL, BOX MOUNTING, SOLDER CONTACT, HERMETIC, AN TYPEAS31421A (Current)2/14/2020
AE-8C1 Connectors Committee
National Aerospace and Defense Contractors Accreditation Program Requirements for Painting and Dry Film CoatingsAS7108/1B (Current)6/11/2009
This document has been declared "CANCELLED" as of June 2009 and has been superseded by PRI AC7108/1. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7108/1. Cancelled specifications are available from SAE.
Nadcap Management Council
National Aerospace and Defense Contractors Accreditation Program, Requirements for Electrochemical Grinding (ECG)AS7116/2A (Current)7/30/2008
This document has been declared "CANCELLED" as of July 2008 and has been superseded by PRI AC7116/2. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7116/2. Cancelled specifications are available from SAE.
Nadcap Management Council
Direct Ship - Recommended Practices for Aerospace CompaniesARP9004A (Current)3/6/2006
Limited to the Aerospace industry where an approved manufacturer requests a supplier to ship an article against the approved manufacturer's quality system directly to a customer. The direct ship process is not required or applicable to standard parts or military parts. In this process the approved manufacturer is responsible for assurance that the article conforms to Type Design information.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Silica Cloth, "B" Stage Phenolic Resin Impregnated High Pressure MoldingAMS3830A (Current)7/1/1990
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of January 1990.
AMS P17 Polymer Matrix Composites Committee
BOLT, SPLINE DRIVE EXTENDED WASHER HEAD, REDUCED HEAD, RETAINER LOCKED, PD SHANK, AMS5708, METRICMA3449A (Current)3/15/2022
E-25 General Standards for Aerospace and Propulsion Systems
STUD, LOCKED IN, KEY LOCKED, UNS S66286, 140 KSI/1200 °F HEAVY-DUTY, SELF-BROACHING KEYSAS3544A (Current)5/5/2026
E-25 General Standards for Aerospace and Propulsion Systems
800P2-2 Cabin Connectors and Cables, Part 2, Specification of Connectors, Contacts, and BackshellsARINC800P2-2 (Current)9/9/2021
This specification describes the general connectors, contacts, and backshells in their shape and characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.
Airlines Electronic Engineering Committee
848 Media Independent Secure Offboard NetworkARINC848 (Current)6/19/2020
ARINC Specification 848 is a functional standard based on a protocol specification profile for a secured network interface. The purpose is to define a common method of initiating a mutually authenticated tunnel between an aircraft service and its Enterprise service. ARINC Specification 848 defines a standard implementation for securing the communications between an onboard Local Area Network (LAN) and an Enterprise LAN on the ground. Various aircraft network architectures and various air to ground communication channels (aka media) are accommodated in this document. For example, L-band Satellite Communication (Satcom), Ku/Ka-band Satcom, Gatelink Cellular, and Gatelink are considered.
Airlines Electronic Engineering Committee
Steel, Bars, and Forgings and Forging Stock 0.90Si - 1.0Cr - 2.0Ni - 3.2Mo - 2.0Cu - 0.10V (0.07 - 0.13C) Vacuum Arc or Electroslag RemeltedAMS6308G (Current)5/1/2023
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
424-23 Navigation System DatabaseARINC424-23 (Current)3/30/2022
This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment.
Airlines Electronic Engineering Committee
485P1-4 Cabin Equipment Interfaces, Part 1, Head End Equipment ProtocolARINC485P1-4 (Current)6/30/2020
This standard defines the electrical characteristics, protocol and data content for a modified version of the EIA RS-485 data bus adapted for use with cabin electronics equipment. Specific cabin equipment interfaces are defined by ARINC 628.
Airlines Electronic Engineering Committee
Aluminum Alloy, Plate 1.0mg 0.60si 0.28cu 0.25crAMS4043B (Current)1/1/1989
AMS D Nonferrous Alloys Committee
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