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Items (221,567)

J3226_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

664P1-2 Aircraft Data Network, Part 1, Systems Concepts and Overview

ARINC664P1-2 (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

628 Part 6 Cabin Equipment Interfaces (CEI) Part 6 Fiber Optic Cable Assembly General Specification

ARINC628P6 (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 Wiring

ARINC628P4B (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

429P3-19 Mark 33 Digital Information Transfer System (DITS) - Part 3 - File Data Transfer Techniques

ARINC429P3-19 (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

626-3 Standard ATLAS Language for Modular Test

ARINC626-3 (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

653P3Bc1 Avionics Application Software Standard Interface, Part 3B, Conformity Test Specifications for ARINC 653 Extended Services

ARINC653P3BC1 (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

818-3 Avionics Digital Video Bus (ADVB) High Data Rate

ARINC818-3 (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

On-Highway Equipment Control and Communication Network

J1939/1_202109 (Current)9/21/2021

SAE J1939-1 specifies the minimum set of SAE J1939 documents that define the Truck and bus control and communications vehicle network as it applies to on-highway equipment. Vehicles covered include all on-highway straight trucks and combination vehicles. A combination vehicle consists of one towing vehicle (tractor) and one or more towed vehicles (trailers and dollies). Dolly axles within the road train are considered to be towed vehicles.

Truck and Bus Control and Communications Network Committee

RESOLUTION OF INSERVICE ANOMALIES THROUGH ASAPP

ARINC640 (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

BOSS - PLUG/PIN, EXPANSION TYPE HOLE PREPARATION

AIR3276A (Current)

2/19/2026

E-25 General Standards for Aerospace and Propulsion Systems

Sealing Compound, Polythioether For Aircraft Windshields and Canopies, For Use Up to 300 °F (149 °C)

AMS3258A (Current)

9/23/2011

This specification covers a polythioether based sealing compound supplied as a two-component system suitable for application by brush, or by extrusion gun or spatula.

AMS G9 Aerospace Sealing Committee

653P5-1 Avionics Application Software Standard Interface, Part 5, Core Software Recommended Capabilities

ARINC653P5-1 (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

Rubber, Chlorosulfonated Polyethylene Elastomer, Sheet and Molded Shapes, Ozone Resistant

AMSR81828A (Current)

9/23/2011

This specification covers the requirements for ozone resistant chlorosulfonated polyethylene rubber in sheet form and as molded or extruded parts.

AMS CE Elastomers Committee

Tubing, Irradiated Polyolefin Plastic, Electrical Insulation Pigmented, Semi-Rigid, Heat Shrinkable, 2 to 1 Shrink Ratio

AMS3638G (Current)

1/16/2012

This specification covers an irradiated, thermally-stabilized, flame-retardant, modified polyolefin plastic in the form of thin-wall tubing.

AMS P Polymeric Materials Committee

Silicone Resin, Elastomeric, Transparent Elevated Temperature Cure

AMS3368B (Current)

1/17/2012

This specification covers a silicone rubber in the form of a two-component liquid.

AMS G9 Aerospace Sealing Committee

WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED EXTRUDED TFE, POLYIMIDE COATED, SILVER-COATED HIGH STRENGTH COPPER ALLOY CONDUCTOR, 600-VOLT, ROHS

AS22759/30B (Current)

4/5/2019

AE-8D Wire and Cable Committee

CLAMP, RECTANGULAR, 2 PIECE, CUSHIONED, WITH WEDGES, PHOSPHATE ESTER FLUID RESISTANT, METRIC

MA2154/2 (Current)

4/27/2015

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Nadcap Requirements for Rotational Friction/Inertia Welding

AS7110/7D (Current)3/6/2007

This document has been declared "CANCELLED" as of March 2007 and has been superseded by PRI AC7110/7. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index noting that it is superseded by PRI AC7110/7. Cancelled specifications are available from SAE.

Nadcap Management Council

ARC FAULT CIRCUIT BREAKER, TRIP FREE, PUSH-PULL, FUSIBLE LINK DESIGN, 2 ½ -15 AMPS, TYPE I

AS5692/1 (Current)

3/27/2023

AE-7P Protective and Control Devices

CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, ENGINE APPLICATION, (FOR MIL-DTL-38999 SERIES I, III, AND IV CONNECTORS)

AS39029/117 (Current)

12/22/2020

AE-8C1 Connectors Committee

Integrated Rudder and Brake Pedal Unit, General Requirements for Fly-By Wire Transport and Business Aircraft

ARP6252 (Current)

10/15/2018

This Aerospace Recommended Practice (ARP) provides general requirements for a generic, integrated rudder and brake pedal unit, incorporating a passive force-feel system that could be used for fixed-wing fly-by wire transport and business aircraft. This ARP addresses the following: The functions to be implemented The mechanical interconnection between captain and F/O station The geometric and mechanical characteristics The mechanical, electrical, and electronic interfaces The safety and certification requirements

A-6A3 Flight Control and Vehicle Management Systems Cmt

Pilot-System Integration

ARP4033A (Current)

11/3/2020

A recommended pilot-system integration (i.e., crew interface and system integration) approach for concept development is described in Figure 1. The approach emphasizes the fundamental need for a top-down design methodology with particular focus on clear operational performance requirements and functional integration. While this document is primarily aimed at aircraft systems design and integration, the methodology is applicable to a wide range of design and integration situations. It is derived from well established human factors engineering design principles.

G-10EAB Executive Advisory Group

Gland Design, O-Ring and Other Elastomeric Seals, Static Applications

AS5857A (Current)

8/17/2022

This SAE Aerospace Standard (AS) provides standardized gland (groove) design criteria and dimensions for elastomeric seal glands for static applications. The glands have been specifically designed for applications using SAE AS568 size O-rings at pressures exceeding 1500 psi (10.3 MPa) utilizing one or two anti-extrusion (backup) rings and applications at pressures under 1500 psi (10.3 MPa) without backup rings. The glands have been sized to provide increased squeeze as compared to AS4716 for more effective sealing at low temperatures and low seal swell conditions. These glands are not recommended for dynamic use. Primary usage is for static external sealing. The rod dimensions are the same as AS4716. The cylinder bore dimensions are the same as AS4716 except for sizes -001 thru -011 and -104 thru -113.

A-6C2 Seals Committee

717-15 Flight Data Acquisition and Recording System

ARINC717-15 (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

591 Quick Access Recorder for AIDS System (QAR)

ARINC591 (Current)7/1/1972

This standard provides design guidance for development and installation of a QAR, whose basic functions are to store digital data supplied at the output of an ARINC 573 FDAU or other similar acquisition unit and provide an easy access to this stored data for systematic ground processing for performance monitoring, maintenance monitoring or other purposes.

Airlines Electronic Engineering 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

Aluminum Alloy 2219, Plate and Sheet

AMSQQA250/30A (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 Model

AIR6515A (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 Notice

AIR4757 (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 Tubing

AMS2253F (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 for

AMS7101A (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 Applications

AMS6497B (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 Aged

AMS4306C (Current)

1/12/2018

This specification covers an aluminum alloy in the form of plate.

AMS D Nonferrous Alloys Committee

Polytetrafluoroethylene Film General Purpose Grade

AMS3662D (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 Hardness

AMSP5315C (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 Treated

AMS5442B (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