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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, 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, 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, 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
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5708 (UNS N07001), .1900-32 UNJF-3AAS3404B (Current)3/2/2022
E-25 General Standards for Aerospace and Propulsion Systems
Landing Gear System Development PlanARP1598D (Current)4/24/2025
A-5 Aerospace Landing Gear Systems Committee
Water Repellent, Window and Windshield, Glass and PlasticAS6882 (Current)7/1/1999
This specification covers the requirements for one type of water repellent compound.
Aerospace Council
BEARING, BALL, ANNULAR, PRIMARILY FOR AIRCRAFT GENERATORS AND MOTOR-GENERATORS, THIN EXTRA LIGHT, TYPE IIIAS17109A (Current)11/13/2014
ACBG Rolling Element Bearing Committee
645-2 Secure Software Data LoadingARINC645-2 (Current)6/15/2026
The ARINC 645-2 standard emphasizes comprehensive cybersecurity practices for software data loading in aviation, including digital signatures, access controls, device hardening, and detailed logging to ensure software integrity, authenticity, and system security.
Airlines Electronic Engineering Committee
857 Securing Non-Safety SATCOM CommunicationsARINC857 (Current)6/15/2026
This document provides comprehensive guidance on cybersecurity practices, threat assessment, and security controls for non-safety satellite communication (Satcom) systems onboard commercial aircraft, emphasizing protection of data, system integrity, and privacy.
Airlines Electronic Engineering Committee
PROTECTIVE COVER, CONNECTOR PLUG, REVERSE BAYONET COUPLINGAS95234/10A (Current)9/18/2025
AE-8C1 Connectors Committee
INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE, POLYVINYLIDENE FLUORIDE, SEMI-RIGID, CROSSLINKEDAS23053/8A (Current)2/14/2023
AE-8D Wire and Cable 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
Tubular Assemblies, Fusion Welded, Inspection Processes and Acceptance Standards ForAS4488A (Current)9/18/2025
This specification classifies fusion welds according to structural integrity requirements and establishes inspection methods and acceptance standards for welded tubular assemblies used in aerospace applications.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
664P1-2 Aircraft Data Network, Part 1, Systems Concepts and OverviewARINC664P1-2 (Current)6/20/2019
The purpose of this document is to provide an overview of data networking standards recommended for use in commercial aircraft installations. These standards provide a means to adapt commercially defined networking standards to an aircraft environment. It refers to devices such as bridges, switches, routers and hubs and their use in an aircraft environment. This equipment, when installed in a network topology, can optimize data transfer and overall avionics performance.
Airlines Electronic Engineering Committee
RESOLUTION OF INSERVICE ANOMALIES THROUGH ASAPPARINC640 (Current)9/30/1997
Defines a generalized process by which anomalies in aircraft systems can be detected. This process is intended to improve timely isolation and resolution of those anomalies. The objective is to reduce costs to the airlines, airframe manufacturers and aircraft systems suppliers by removing anomalous behavior from aircraft systems in a timely manner.
Avionics Maintenance Committee
653P3Bc1 Avionics Application Software Standard Interface, Part 3B, Conformity Test Specifications for ARINC 653 Extended ServicesARINC653P3BC1 (Current)7/18/2019
ARINC 653, Part 3B is the Compliance Test Specification for ARINC 653 Extended Services presently defined in ARINC 653 Part 2. The document specifies a set of stimuli and the expected responses. Future work on the ARINC 653 document set includes an effort to define Operating System services for multi-core processor environments. The Compliance Test Specification is expected to be updated in step with ARINC 653, Part 2.
Airlines Electronic Engineering Committee
666 - Electronic Distribution of SoftwareARINC666 (Current)5/1/2002
This document describes a secure internet facility for sending all types of aviation software using the world wide web (www). Software suppliers may use this document as a starting point for the construction of a secure web server utility. It provides sufficient flexibility and is compatible with numerous software distribution models. The file management structure is consistent with other ARINC standards for loadable software, and references ARINC 665 and ARINC 667 in particular.
Airlines Electronic Engineering Committee, Avionics Maintenance 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
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
CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, ENVIRONMENTAL RESISTANT, REMOVABLE CRIMP CONTACTS, STOWAGE RECEPTACLE (SERIES B)AS29600/6A (Current)9/18/2014
AE-8C1 Connectors Committee
709A-1 Precision Airborne Distance Measuring Equipment (DME/P)ARINC709A-1 (Current)8/17/1994
This standard provides general and specific design guidance for the development of a DME/P, which provides slant range distance from an aircraft to a selected DME ground facility. For landing purposes, the DME/P complements the angle MLS/ILS with precise range data.
Airlines Electronic Engineering Committee
717-15 Flight Data Acquisition and Recording SystemARINC717-15 (Current)6/6/2011
This document provides design guidance for the development and installation of a Digital Expandable Flight Data Acquisition and Recording System (DEFDARS) primarily intended for airline use. As such, this guidance will include specific requirements necessary to accommodate mandatory flight data recording and other flight data acquisition needs plus the requirements to ensure customer controlled interchangeability of equipment in a standard aircraft installation. The system capability was expanded to accommodate a data bus speed of 1024 words per second.
Airlines Electronic Engineering Committee
818-3 Avionics Digital Video Bus (ADVB) High Data RateARINC818-3 (Current)12/16/2019
ARINC 818 defines the digital video interface standard intended for use in all types of flight deck displays. This document represents the aviation version of ANSI Fibre Channel Audio Video (FC-AV) defined by ANSI INCITS 356-2002. Supplement 3 Supports the latest digital video rates of 12 Gbps and higher using 64B/66B encoding and 28 Gbps using 256B/257B encoding.
Airlines Electronic Engineering Committee
626-3 Standard ATLAS Language for Modular TestARINC626-3 (Current)1/1/1995
This standard defines an airline-recommended subset of the Abbreviated Test Language for All Systems (ATLAS)intended to be used in conjunction with test systems that are compliant with ARINC 608A. ATLAS is a standard abbreviated English language used in preparation and documentation of test procedures that can be implemented with automatic or semiautomatic test equipment.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
CLAMP, LOOP STYLE, CUSHIONED, WITH WEDGE, HYDROCARBON FLUID RESISANT, METRICMA2150/1 (Current)4/27/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
Fittings, 24° Cone Flareless, Fluid Connection, 5000 psiAS4444A (Current)7/7/2025
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone flareless fluid connection fittings and nuts and bite type flareless sleeves (see Section 6) for use in aircraft fluid systems at an operating pressure of 5000 psi for the fittings and nuts and 3000 psi for the bite type sleeves.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
665-5 Loadable Software StandardsARINC665-5 (Current)8/13/2019
This document defines the aircraft industry's standards for Loadable Software Parts (LSPs) and Media Set Parts (MSPs). It describes the common principles and rules to be applied to any part of a data load system to ensure compatibility and inter-operability of software parts. It includes part numbering, content, labeling, and formatting of an LSP, and a Media Set containing LSPs. Supplement 5 refers to a companion document, ARINC Report 645: Common Terminology and Functions for Software Distribution and Loading.
Airlines Electronic Engineering Committee
High-Strength Carbon and Alloy Die Drawn SteelsJ935_202606 (Current)6/22/2026
This SAE Recommended Practice is intended to provide basic information on properties and characteristics of high-strength carbon and alloy steels which have been subjected to special die drawing. This includes both cold drawing with heavier-than-normal drafts and die drawing at elevated temperatures.
Metals Technical Committee
653P5-1 Avionics Application Software Standard Interface, Part 5, Core Software Recommended CapabilitiesARINC653P5-1 (Current)8/7/2019
Part 5 defines additional ARINC 653 core software capabilities to ease integration on a variety of Integrated Modular Avionics (IMA) hardware platforms by allowing platform suppliers to extend and customize it for use with their unique hardware platform. Supplement 1 expands the guidance provided on resource profiling and execution profiling pertinent to the use of multicore processors in avionics.
Airlines Electronic Engineering Committee
628 Part 6 Cabin Equipment Interfaces (CEI) Part 6 Fiber Optic Cable Assembly General SpecificationARINC628P6 (Current)2/28/2002
ARINC Specification 628, Cabin Equipment Interfaces (CEI) Part 6 Fiber Optic Cable Assembly General Specification, defines the minimum acceptable provisions for connectorized fiber optic cable assemblies used in permanently installed airframe wire bundles that are part of ARINC 628 supported systems. The intent is for the cable assembly supplier to use this specification as a guideline to provide the prospective IFE contractor with cable assemblies that have adequate quality and performance for the intended application. These assemblies are suitable for cabin systems applications only. Applicable guidelines not found in this specification may be found in Section 9 of ARINC Specification 628 Part 4A.
Airlines Electronic Engineering Committee
628 Part 4B - Cabin Equipment Interfaces (CEI), Part 4B, Cabin Management and Entertainment System - Cabin Distribution System (CDS) - Star WiringARINC628P4B (Current)6/18/1999
Cabin equipment interfaces Part 4B is similar to description provided for Part 4A. The significant difference is that Part 4B specifies a CDS using a star wiring topology. Standardized wiring, connectors and installation requirements for a passenger seat network, overhead video network, and cabin management equipment network are included. Electrical and fiber optic networks are covered.
Airlines Electronic Engineering Committee
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 HEXAGON, DRILLED, EXTENDED WASHER HEAD, PD SHANK, NICKEL ALLOY, UNS N07718, 220 KSI MINAS3662 (Current)1/26/2026
E-25 General Standards for Aerospace and Propulsion Systems
429P3-19 Mark 33 Digital Information Transfer System (DITS) - Part 3 - File Data Transfer TechniquesARINC429P3-19 (Current)6/25/2009
This standard defines the air transport industry's standards for the transfer of digital data between avionics system elements. Part 3 defines the data link layer protocol standards.
Airlines Electronic Engineering Committee
BOLT, MACHINE - HEXAGON HEAD, PD SHANK, CORROSION AND HEAT RESISTANT STEEL UNS S66286, .5000-20 UNJF-3AAS3104B (Current)4/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Night Vision Imaging Systems (NVIS) Integrally Illuminated Information PanelsARP4967C (Current)8/21/2023
This document is intended to highlight critical design issues that a panel designer should understand when designing panels for NVIS applications. It is not intended to be a discussion of the benefits of one lighting technology versus another. Refer to ARP4168 for a more complete discussion of these lighting technologies.
A-20A Crew Station Lighting
Alloy Bars and Forgings, Corrosion and Heat Resistant 25fe 20.5cr 20ni 20co 4.0mo 4.0w 4.0(Cb + Ta) Solution and Precipitation Heat TreatedAMS5770D (Current)1/1/1990
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of Januray 1990.
AMS F Corrosion and Heat Resistant Alloys Committee
CONNECTOR, RECEPTACLE, REVERSE BAYONET COUPLING, JAM NUTAS95234/7A (Current)11/27/2023
AE-8C1 Connectors Committee
ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONSAS5831 (Current)1/9/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Clamp Assembly, Saddle Type, Cushioned, General Specification ForAS85449C (Current)5/27/2025
This SAE Aerospace Standard (AS) defines the requirements for saddle-type clamps. Tests and criteria noted do not indicate any specific areas of application or usage. Supplemental testing may be necessary to determine suitability for specific environments and applications.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Test Plan for the Digital Time Division Command/Response Multiplex Data Bus SystemAS4115A (Current)8/15/2017
This test plan consists of two major sections for testing of MIL-STD-1553B data bus systems: Bus Network and System Integration Tests.
AS-1A Avionic Networks Committee
RING, LOCK, SERRATEDAS51990C (Current)2/10/2020
E-25 General Standards for Aerospace and Propulsion Systems
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