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CONTACTS, ELECTRICAL CONNECTOR, PIN CRIMP REMOVABLE (FOR AS81511 SERIES 1 & 2 CONNECTORS)AS39029/47C (Current)2/25/2025
AE-8C1 Connectors Committee
WASHER, FLAT - AMS5510AS9549A (Current)2/18/2019
E-25 General Standards for Aerospace and Propulsion Systems
CONTACTS, ELECTRICAL CONNECTOR SOCKET, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, III, IV CONNECTORS)AS39029/88C (Current)11/12/2025
AE-8C1 Connectors Committee
FLANGE END, SOLID, WIDE DESIGN STANDARDAS4751/3A (Current)10/21/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
660B CNS/ATM Avionics Architectures Supporting NextGen/SESAR ConceptsARINC660B (Current)1/1/2014
This document identifies and describes the aircraft avionics capability necessary for operation in the evolving Communications Navigation Surveillance/Air Traffic Management (CNS/ATM) environment expected for the FAA NextGen program, Single European Sky ATM Research (SESAR) program and considerations of the Japan Collaborative Actions for Renovation of Air Traffic Systems (CARATS). These capabilities are intended to satisfy the industry's long-term CNS/ATM operational objectives.
Airlines Electronic Engineering Committee
660A CNS/ATM Avionics, Functional Allocation and Recommended ArchitecturesARINC660A (Current)1/1/2001
This standard expands ARINC 660 to include industry-defined architectures for the CNS/ATM operating environment. These architectures are intended to meet long-term requirements (e.g., ADS-B, CPDLC, etc.) and provide growth for the future. Airlines support the implementation of these architectures for the long-term. This standard represents broad airline consensus for developing avionics equipment providing CNS/ATM operating capabilities.
Airlines Electronic Engineering Committee
Rolling Element Bearing Test MethodsARP5483B (Current)4/26/2023
This SAE Aerospace Recommended Practice (ARP) establishes methods for testing airframe rolling element bearings. The purpose of ARP5483 and its associated slash sheets is to document test methods commonly used to evaluate airframe bearings. These test methods may be referenced in standards, purchase orders, etc. when the test is deemed appropriate to the intended use of the bearing by the end user of the bearing. These test methods are not intended to encompass every conceivable requirement for an airframe bearing. The end user of the bearing must exercise engineering judgment to determine the most appropriate standard and/or nonstandard tests for the application.
ACBG Rolling Element Bearing Committee
COUPLINGS, CLAMP, GROOVED, V-BAND, 1.75 TO 6.25 FLANGE OD (-65 TO 250 °F)AS5355/2B (Current)3/28/2017
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Abuse Load Testing for In-Seat Deployable Video SystemsARP5475A (Current)11/28/2011
This SAE Aerospace Recommended Practice (ARP) provides guidelines for abuse load testing of a deployable Individual Video System (IVS). The abuse load testing defined in this ARP is intended to only address the evaluation of the deployable IVS regarding stowage of the system and injurious projections/protrusions as a result of passenger interaction with the video system. Other aspects of the video system design or qualification may require additional testing or analysis and are outside the scope of this ARP. This ARP is not intended to address customer satisfaction or reliability aspects of individual designs.
Aircraft Seat Committee
SCREW – FLAT FILLISTER HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN. .1900-32 UNF-3AAS115401B (Current)5/22/2014
E-25 General Standards for Aerospace and Propulsion Systems
Fittings, Cargo Tiedown, AircraftAS7092B (Current)10/15/2012
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
AGE-2 Air Cargo
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, MIL-DTL-83723 SERIES I AND III, AND MIL-DTL-83733 CONNECTORS)AS39029/4D (Current)7/23/2024
AE-8C1 Connectors Committee
Hot Stamp Wire Marking Concerns for Aerospace Vehicle ApplicationsAIR5575A (Current)1/24/2017
This SAE Aerospace Information Report (AIR) discusses the often overlooked relationship between hot stamp marking and the environmental conditions that contribute aircraft wiring problems and discusses current beliefs of military service experts, regulatory agencies and industry standard writing bodies about the potential hazards imposed by the hot stamping process.
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
CONTACTS, ELECTRICAL CONNECTORS, PIN, SOLDER, REMOVABLE, SHIELDED, SIZE 12 (FOR MIL-DTL-83723 SERIES III CONNECTORS)AS39029/74C (Current)8/23/2021
AE-8C1 Connectors Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE CRES BRAID REINFORCED, 400 °F, 5080 PSI FLARELESS, 45° ELBOW TO 45° ELBOWAS5964C (Current)11/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE CRES BRAID REINFORCED, 400 °F, 5080 PSI FLARELESS, STRAIGHT TO STRAIGHTAS5961C (Current)11/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
PIN, STRAIGHT, HEADED .497 DIAMETER, AMS5735AS9468A (Current)10/18/2018
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, SHEAR – DOUBLE HEX HEAD, DRILLED SHANK UNS N07718 – 185 ksiAS3532A (Current)6/3/2019
E-25 General Standards for Aerospace and Propulsion Systems
777-2 Recorder Independent Power Supply (RIPS)ARINC777-2 (Current)10/11/2010
This Characteristic provides the definitions for the physical form and fit dimensions, the electrical interfaces, and the functions of an independent power supply for cockpit voice recorders or crash survivable recorders that combine voice with other recording functions. The RIPS is used to provide backup power that is independent of the aircraft generated power buses. Supplement 2 introduces a description of charge rates for alternate power sources and revises the electrical interface to accommodate monitoring of the RIPS status.
Airlines Electronic Engineering Committee
Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Silver-Coated Copper Alloy Conductor, 600-Volt, 110°CAS50861/6A (Current)1/2/2018
AE-8D Wire and Cable Committee
619-5 ACARS Protocols for Avionic End SystemsARINC619-5 (Current)8/9/2017
The purpose of this document is to delineate, in an organized fashion, the protocols used by Aircraft Communication Addressing and Reporting System (ACARS) Management Units (MU) defined in ARINC Characteristic 724B and Communications Management Unit (CMU) defined in ARINC Characteristic 758, in their interactions with other onboard avionics equipment.
Airlines Electronic Engineering Committee
764 Head-Up Display (HUD) SystemARINC764 (Current)7/8/2005
This document defines a Head-Up Display (HUD) system intended for installation in all types of aircraft. It describes the physical form factors, fit dimensions, electrical interface definition and typical HUD functions, including the display of navigation and guidance information in the flight crew's forward field of view. The HUD accomplishes this by projecting images onto a combiner with symbology that conforms to the outside world view. Guidance for HUD architectures include single, twin, dual and HUD integrated with Primary Flight Display (PFD). This document is an practical guide for the design of federated equipment and integrated modular avionics.
Airlines Electronic Engineering Committee
659 Backplane Data BusARINC659 (Current)12/1/1993
Defines standards for the transfer of digital data between components within an IMA cabinet. Includes the protocol and timing characteristics for a synchronous backplane data bus capable of transferring data at 60 Mbps using a data path that is two bits wide. The electrical characteristics and behavior expected of the participating modules are defined.
Airlines Electronic Engineering Committee
727-1 Airborne Microwave Landing SystemARINC727-1 (Current)8/1/1987
This standard sets forth the characteristics of MLS receiver processors intended for installation in all types of commercial transport aircraft. The function of the airborne MLS receiver processor is the reception and processing of the MLS azimuth signals, the elevation signals, and the data transmitted from the MLS ground stations.
Airlines Electronic Engineering Committee
Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement SpecificationAS5272G (Current)9/11/2024
This SAE Aerospace Standard (AS) establishes the requirements for heat-cured solid film lubricants. For other general or high-temperature applications, refer to AS1701. This document requires qualified products.
E-25 General Standards for Aerospace and Propulsion Systems
Procedures for Determining and Verifying Peening IntensityJ443_202512 (Current)12/11/2025
This SAE Standard defines the method for deriving and verifying the peening intensity exerted onto a part surface during shot peening or other surface enhancement processes.
Surface Enhancement Committee
739-1 Multi-Purpose Control and Display Unit (MCDU)ARINC739-1 (Current)6/1/1990
MCDU consists of an alphanumeric keyboard and display unit capable of interfacing with a number of aircraft systems. Dedicated keys on the MCDU provide the means for system selection with programmable soft keys. ARINC 429 interfaces are used to communicate with participating systems.
Airlines Electronic Engineering Committee
CABLE, FIBER OPTIC, MULTI-MODE, 50/125/450 µm, GRADED INDEX, HERMETIC COATED, TIGHT BUFFERAS5382/5B (Current)9/21/2021
AS-3 Fiber Optics and Applied Photonics Committee
Aircraft Fuel Weight Penalty Due to Air ConditioningAIR1168/8A (Current)7/25/2011
The purpose of this section is to provide methods and a set of convenient working charts to estimate penalty values in terms of take-off fuel weight for any given airplane mission. The curves are for a range of specific fuel consumption (SFC) and lift/drag ratio (L/D) compatible with the jet engines and supersonic aircraft currently being developed. A typical example showing use of the charts for an air conditioning system is given. Evaluation of the penalty imposed on aircraft performance characteristics by the installation of an air conditioning system is important for two reasons: 1 It provides a common denominator for comparing systems in the preliminary design stage, thus aiding in the choice of system to be used. 2 It aids in pinpointing portions of existing systems where design improvements can be most readily achieved. All factors that influence the flight performance of an aircraft can be expressed in terms of weight, external and momentum drags, and changes in powerplant
AC-9 Aircraft Environmental Systems Committee
ARINC 835-2 Guidance for Security of Loadable Software Parts Using Digital SignaturesARINC835-2 (Current)12/2/2025
This document provides a comprehensive overview of methods and standards for securing loadable software parts (LSPs) used in aircraft systems. It focuses on ensuring the integrity, authenticity, and trustworthiness of aircraft software, independent of the transport mechanism or media type, through the use of digital signatures and Public Key Infrastructure (PKI) technologies. The document captures solutions developed by major aerospace manufacturers and industry participants and encourages standardization to reduce costs and complexity in software security processes.
Airlines Electronic Engineering Committee
628P1-8 Cabin Equipment Interfaces, Part 1, Cabin Management and Entertainment System - PeripheralsARINC628P1-8 (Current)6/26/2023
This document defines system architectural philosophy and specific design guidance for the design and interface of various cabin related components. System performance parameters are described for connectors, electrical interfaces, operational mode control/protocols, BITE reporting, reliability, environmental conditions, and software data loading. Supplement 8 defines an IEEE 802.11n compliant Cabin Wireless Access Point (CWAP) suitable for installation in a wide variety of cabins. It provides an update to the digital overhead monitor mounting provisions and connectors for compatibility with the CWAP definition. Supplement 8 includes new generation implementation solutions for Cabin Wireless Access Points (CWAP) and Cabin Cell Modems (CCM). The description and interface definitions for an HD cabin and cargo video surveillance system is added. Finally, it includes the component definition and network specifications.
Airlines Electronic Engineering Committee
807-4 Fiber Optic Training RequirementsARINC807-4 (Current)1/10/2019
This document is based upon the SAE ARP5602 document, A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education. ARINC Report 807: Fiber Optic Training Requirements is a subset of the SAE ARP5602 document designed to meet the requirements of the commercial air transport industry. Certification to the SAE ARP5602 document fulfills the requirements of ARINC Report 807. This document defines recommended general practices for training requirements of aerospace fiber optic systems. It is the intention of this document to outline proven training practices and general standards of workmanship for technicians engaged in aerospace fiber optic manufacturing, installation, maintenance, and repair for the air transport industry. It is also recommended that management and purchasing personnel receive fundamental training to familiarize themselves with the requirements of aerospace fiber optics.
Airlines Electronic Engineering Committee
653P1-6 Avionics Application Software Standard Interface, Part 1, Required ServicesARINC653P1-6 (Current)12/16/2024
This standard defines a general-purpose Application/Executive (APEX) software interface between the Operating System of an avionics computer and the application software. The interface requirements between the application software and operating system services are defined in a manner that enables the application software to control the scheduling, communication, and status of internal processing elements.
Airlines Electronic Engineering Committee
623-3 Character-Oriented Air Traffic Service (ATS) ApplicationsARINC623-3 (Current)4/1/2005
This standard defines the application text formats for character-oriented ATS messages that can be transmitted over the ACARS data link. Several ACARS data links are available, including but not limited to VHF, HF and satellite. The messages defined herein are not specific to any data link. This standard is limited in scope to character-oriented applications.
Airlines Electronic Engineering Committee
429P4 Digital Information Transfer System (DITS), Part 4, Archive of ARINC 429 SupplementsARINC429P4 (Current)10/29/2012
This document was prepared in conjunction with Supplement 18 to ARINC Specification 429, Part 1. It is an archive of all ARINC Specification 429 Supplements, currently published in parts. The technical content of each Supplement (unchanged in contents and in form) are reproduced for historical reference.
Airlines Electronic Engineering Committee
702-6 Flight Management Computer System (FMCS)ARINC702-6 (Current)6/1/1994
This standard defines a FMCS for installation in commercial transport aircraft. The FMCS provides performance data, performance computations, fuel management functions, and navigation and guidance to a desired flight plan.
Airlines Electronic Engineering Committee
678 Guidance for Distributed Radio ArchitecturesARINC678 (Current)7/15/2021
The purpose of this document is to evaluate Communication, Navigation, and Surveillance (CNS) Distributed Radio architectures and the feasibility of distributing the RF and systems processing sections to ensure the following: Reduce cost of equipment Reduce Size, Weight, and Power (SWaP) Ease of aircraft integration Growth capability built into the design Maintain or improve system availability, reliability, and maintainability It provides a framework to determine whether it is feasible to develop ARINC Standards that support CNS distributed radio architectures.
Airlines Electronic Engineering Committee
WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, EXTRUDED ETFE, LIGHT WEIGHT, SILVER-COATED HIGH STRENGTH COPPER ALLOY CONDUCTOR, 600-VOLT, 150 °C, ROHSAS22759/19A (Current)10/24/2019
AE-8D Wire and Cable Committee
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SHIELDED (FOR MIL-C-26482 SERIES 2 AND MIL-C-81703 SERIES 3 CONNECTORS)AS39029/7A (Current)3/24/2011
AE-8C1 Connectors Committee
641-1 Logical Software Part Packaging for TransportARINC641-1 (Current)11/16/2020
The purpose of this standard is to provide a method for packaging aircraft software parts for distribution using contemporary media or by electronic distribution. This project intends to standardize and provide guidance for the storage of floppy based software, currently packaged in media set parts. This standard format can be then stored or distributed on a single physical media member (CD-ROM), or by electronic crate. The obsolescence of floppy disks drive an urgent need for this guidance.
Airlines Electronic Engineering Committee
WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, EXTRUDED TFE, SILVER-COATED HIGH STRENGTH COPPER ALLOY CONDUCTOR, 600 VOLT, ROHSAS22759/22A (Current)9/18/2020
AE-8D Wire and Cable Committee
CIRCUIT BREAKER, AIRCRAFT, TRIP-FREE PUSH PULL, TYPE I, DUAL SAFETY, −55 THRU +121 °CAS58091/1A (Current)5/31/2019
AE-7P Protective and Control Devices
655 Remote Data Concentrator (RDC) Generic DescriptionARINC655 (Current)4/1/1999
The RDC have been used for years on commercial aircraft. The extensive use of digital data transfer has prompted the need for a standard for collecting analog, digital and discrete information from sensors on the airplane. This information is digitized and processed in traditional ARINC 700-series equipment or in IMA cabinets.
Airlines Electronic Engineering Committee
Labels, Aluminum Foil Etched and EnameledAMS7294A (Current)1/1/1987
This specification has been 'Cancelled' by the Aerospace Materials Division, SAE, as of September 1996.
AMS D Nonferrous Alloys Committee
688 Intersystem Network IntegrationARINC688 (Current)6/24/2021
The purpose of this document is to provide guidelines for integrating previously standalone cabin systems such as cabin management systems, In-Flight Entertainment (IFE) systems, In-Flight Connectivity (IFC) systems, galley systems, surveillance systems, etc. Resource sharing between systems can reduce airline costs and/or increase functionality. But, as systems expose their internal resources to external systems, the risk of an intrusion that could degrade function and/or negatively expose the supplier's or airline's brand increases. This document provides a recommended IP networking design framework between aircraft systems to reduce the operational security threats while still supporting the necessary intersystem routing.
Airlines Electronic Engineering Committee
CLAMP, LOOP, PLAIN, SUPPORT, AIRCRAFTAS5587C (Current)6/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
429P2-17 Digital Information Transfer System (DITS), Part 2, Discrete Word Data StandardsARINC429P2-17 (Current)8/1/2019
This standard defines the air transport industry's standards for the transfer of digital data between avionics system elements. Part 2 provides the formats of data words with discrete bit encoding.
Airlines Electronic Engineering Committee
WRENCHING ELEMENT SPLINE DRIVE - DIMENSIONS FORAS5443C (Current)12/7/2022
E-25 General Standards for Aerospace and Propulsion Systems
561-11 Air Transport Inertial Navigation System (INS)ARINC561-11 (Current)1/1/1975
This standard defines the requirements of an INS, which provides sensor and steering command outputs. The INS includes inertial sensing and provides outputs for aircraft attitude, present position, and steering signals suitable for operating the pilot's instruments. The basic INS provides complete self-contained horizontal navigation capability intended to serve as the sole means of navigation on a worldwide basis.
Airlines Electronic Engineering Committee
827-2 Electronic Distribution of Software by Crate (EDS Crate)ARINC827-2 (Current)12/3/2025
This standard describes the format for electronic distribution of aircraft software parts and other contents between aerospace business partners using a digital container referred to as an EDS crate. This EDS standard is intended to promote consistent, secure distribution of EDS content to any appropriate destination.
Airlines Electronic Engineering Committee
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