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J1939 Digital AnnexJ1939DA_202606 (Current)6/29/2026
This document is intended to supplement the J1939 documents by offering the J1939 information in a form that can be sorted and searched for easier use.
Truck and Bus Control and Communications Network Committee
EVALUATION OF HELICOPTER TURBINE ENGINE LINEAR VIBRATION ENVIRONMENTAIR1289A (Current)6/29/2026
This SAE Aerospace Information Report (AIR) outlines a recommended procedure for evaluation of the vibration environment to which the gas turbine engine powerplant is subjected in the helicopter installation. This analysis of engine vibration is normally demonstrated on a one-time basis upon initial certification, or after a major modification, of an engine/helicopter configuration. This AIR deals with linear vibration as measured on the basic case structure of the engine and not, for example, torsional vibration in drive shafting or vibration of a component within the engine such as a compressor or turbine airfoil. In summary, this AIR discusses the engine manufacturer’s "Installation Test Code" aspects of engine vibration and proposes an appropriate measurement method.
S-12 Powered Lift Propulsion Committee
Defining and Measuring Factors Affecting Helicopter Turbine Engine Power AvailableARP1702B (Current)6/29/2026
This SAE Aerospace Recommended Practice (ARP) identifies and defines a method of measuring those factors affecting installed power available for helicopter powerplants. These factors are installation losses, accessory power extraction, and operational effects. Accurate determination of these factors is vital in the calculation of helicopter performance as described in the RFM. It is intended that the methods presented herein prescribe and define each factor as well as an approach to measuring said factor. Only basic installations of turboshaft engines in helicopters are considered. Although the methods described may apply in principle to other configurations that lead to more complex installation losses, such as an inlet particle separator, inlet barrier filter (with or without a bypass system), or infrared suppressor, specialized or individual techniques may be required in these cases for the determination and definition of engine installation losses. Some rotorcraft may use an
S-12 Powered Lift Propulsion Committee
Passenger Oxygen MaskAS8025A (Current)6/29/2026
This standard covers oronasal type masks which use a continuous flow oxygen supply. Each such mask comprises a facepiece with valves as required, a mask suspension device, a reservoir, or rebreather bag (when used), a length of tubing for connection to the oxygen supply source, and a means for allowing the crew to determine if oxygen is being delivered to the mask. The assembly shall be capable of being stowed suitably to meet the requirements of its intended use.
A-10 Aircraft Oxygen Equipment Committee
Safety Alert Symbol for Agricultural, Construction, and Industrial EquipmentJ284_202606 (Current)6/29/2026
This SAE Recommended Practice covers the safety alert symbol intended for use on construction and industrial equipment as defined in SAE J1116 and on agricultural tractors and machinery as defined in ASABE S390.
HFTC2, Machine Displays and Symbols
Chemical Oxygen SystemsAIR825/4A (Current)6/29/2026
This SAE Aerospace Information Report (AIR) provides an orientation regarding the general technology of chemical oxygen generators to aircraft engineers for assistance in determining whether chemical oxygen generators are an appropriate oxygen supply source for hypoxia protection in a given application and as an aid in specifying such generators. Information regarding the details of design and manufacture of chemical oxygen generators is generally beyond the scope of this document.
A-10 Aircraft Oxygen Equipment Committee
Remover, Organic Coating, Hot Tank TypeAMSR81835 (Current)1/25/2008
This specification covers the requirements for one grade of remover of various organic coatings from aircraft parts.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Aerospace Series - Non-Deliverable Software RequirementsAS9125 (Current)10/1/2024
This standard defines the requirements for the effective control of non-deliverable software. This standard can be used during the design, development, test, production, release, use, maintenance, and retirement of non-deliverable software. This can include non-deliverable software procured from external suppliers and utilized in the design, production, evaluation, test, acceptance, or calibration of a deliverable product. This standard focuses solely on the unique requirements of the operational processes that pertain to non-deliverable software as identified by clause 1.2. Operational processes not covered in this standard are addressed by the respective organization’s Quality Management System (QMS), based on the 9100-series (i.e., 9100, 9110, 9120) and/or ISO 9001 standards. If there is a conflict between the requirements of this standard, and customer or applicable statutory/regulatory requirements, the latter shall take precedence.
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Aluminum Alloy, Bar, Rod, and Wire, Rolled, Drawn, or Cold Finished, 6262AMSQQA225/10A (Current)6/18/2007
This specification covers the specific requirements for 6262 aluminum alloy bar, rod, and wire produced by rolling, drawing or cold finishing.
AMS D Nonferrous Alloys Committee
DRUMS, METAL - SHIPPING AND STORAGE 3 TO 12 GALLONSAS27684 (Current)11/6/2017
AGE-2 Air Cargo
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
DRUMS, METAL - SHIPPING AND STORAGE 16 TO 80 GALLONSAS27683 (Current)11/6/2017
AGE-2 Air Cargo
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
SCREW - FLAT FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS G87400, 125 KSI MIN .2500-20 UNC - 3AAS115851C (Current)5/9/2022
E-25 General Standards for Aerospace and Propulsion Systems
724B-6 Aircraft Communications Addressing and Reporting System (ACARS)ARINC724B-6 (Current)2/24/2012
This standard describes the 724B version of the airborne components of ACARS, and is intended for use in conjunction with VHF radio equipment existing on the plane. This ACARS enhancement improves the ability of the system to provide air-to-ground and ground-to-air data communications.
Airlines Electronic Engineering Committee
858P2-1 Internet Protocol Suite (IPS) for Aeronautical Safety Services, Part 2, IPS Gateway Air-Ground InteroperabilityARINC858P2-1 (Current)7/12/2024
ARINC 858 Part 2 provides aviation ground system gateway considerations necessary to transition to the Internet Protocol Suite (IPS). ARINC 858 Part 2 describes the principles of operation for an IPS gateway that enables ACARS application messages to be exchanged between an IPS aircraft and a ground ACARS host. ARINC 858 Part 2 also describes the principles of operation for an IPS gateway that enables OSI-based application messages to be exchanged between an IPS host and an OSI end system. This product was developed in coordination with ICAO WG-I, RTCA SC-223, and EUROCAE WG-108.
Airlines Electronic Engineering Committee
768-2 Integrated Surveillance System (ISS)ARINC768-2 (Current)6/1/2011
This document defines an Integrated Surveillance System (ISS) capable of providing traffic, terrain and weather information to the flight deck crew. Supplement 2 provides enhancements in the traffic surveillance area to support ADS-B Out and ADS-B In functionality, ADS-Re-broadcast capability, and Traffic Information Services  Broadcast (TIS-B).
Airlines Electronic Engineering Committee
719-5 Airborne HF/SSB SystemARINC719-5 (Current)7/6/1984
This standard sets forth characteristics of a new-generation HF/SSB System intended for installation in all types of commercial transport aircraft. Covers requirements for airborne transmitter-receiver equipment capable of transmitting and receiving HF radio intelligence.
Airlines Electronic Engineering Committee
615-4 Airborne Computer High Speed Data LoaderARINC615-4-ER2 (Current)5/1/2002
This standard provides general and specific guidance for the development of a Portable Data Loader (PDL) for carry-on application and an Airborne Data Loader (ADL) for on-board the airplane. It specifies use of a 3.5 inch floppy disk to upload and download of data and operational programs using an ARINC 429 data bus connected to avionics computers.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee, Flight Simulator Engineering and Maintenance Committee
781-9 Mark 3 Aviation Satellite Communication SystemsARINC781-9 (Current)7/31/2024
This document sets forth the desired characteristics of an aviation satellite communication (satcom) system intended for installation in all types of commercial transport and business aircraft. This document provides general and specific guidance on the form factor and pin assignments for the installation of the avionics primarily for airline use. It also describes the desired operational capability of the equipment to provide data and voice communications, as well as additional standards necessary to ensure interchangeability. This Characteristic specifies equipment using Inmarsat satellites operating in L-band. Ku-band and Ka-band equipment are specified in ARINC Characteristic 791, ARINC Characteristic 792, and ARINC Characteristic 793. Supplement 8 added Diplexer Low Noise Amplifiers (DLNA) to protect Inmarsat's Classic Aero and SwiftBroadband satcom equipment from possible ground-based LTE and ATCt (Ligado) interference. Supplement 9 expands the Dual Satcom Operation description
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
439B Simulated Air Traffic Control Environments in Flight Simulation Training DevicesARINC439B (Current)8/31/2020
This document provides guidance on provision of SATCE systems in Flight Simulation Training Devices (FSTDs) for the benefit of flight crew training. This work builds upon that originally undertaken by International Air Transport Association (IATA) Flight Simulator Working Group in 2002, and further developed in the International Civil Aviation Organization (ICAO) Doc. 9625 Vol 1, Part 2, Editions 3 and 4. This document is intended to be a practical starting point that can serve as the basis for future developments of SATCE.
Flight Simulator Engineering and Maintenance Committee
595 Barometric Altitude Rate Computer (BARC)ARINC595 (Current)2/1/1975
This standard provides general guidance for the design and installation of a BARC for use with a GPWS. The BARC generates an electrical rate signal from pneumatic pressure supplied by the aircraft static pressure system. The BARC unit is intended primarily for use with ground proximity warning equipment in aircraft that do not have a suitable electrical signal for altitude rate.
Airlines Electronic Engineering Committee
628P8-1 Cabin Equipment Interfaces, Part 8, In-Flight Entertainment (IFE) Equipment Standard Availability Measurement GuidelinesARINC628P8-1 (Current)12/18/2009
Cabin equipment is required to operate with high standards of availability. This standard provides a standard methodology for measuring and calculating availability. Quantitative measurement guidelines are included.
Airlines Electronic Engineering Committee
735B-2 Traffic Computer TCAS and ADS-B FunctionalityARINC735B-2 (Current)8/6/2015
This document defines a Traffic Surveillance capability for NextGen and SESAR airspace environments. Supplement 2 adds hybrid surveillance functionality. It satisfies recent updates to FAA Airworthiness Circular AC 20-151B - Airworthiness Approval of Traffic Alert and Collision Avoidance Systems (TCAS II), and Technical Standard Order TSO-119d requiring the annunciation of a hybrid surveillance failure. Supplement 2 also adds strobe program pinning, updates TCAS inputs status, improves aircraft troubleshooting, and supports recent central maintenance computer function block point updates.
Airlines Electronic Engineering Committee
Aircraft Seat Design Guidance and ClarificationsARP5526F (Current)5/24/2022
This SAE Aerospace Recommended Practice (ARP) documents a common understanding of terms, compliance issues, and design criteria to facilitate certification of seat installations specific to Part 25 aircraft. This ARP provides general guidance for seats to be installed in Part 23 aircraft and Parts 27 and 29 rotorcraft and does not specify specific designs or design methods for such certification.
Aircraft Seat Committee
Lubricant Application, Solid Film, Heat Cured, Corrosion InhibitingAS5528F (Current)1/17/2023
This SAE Aerospace Standard (AS) establishes the surface pretreatment, temperature, and baking time required to cure AS5272 lubricant when it is applied over the surfaces of manufactured parts of various metals.
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, CADMIUM PLATED, STEEL, UNS G87400, 125 KSI MIN, .3750 - 16 UNS X .3750 - 24 UNF-3AAS126587C (Current)6/2/2022
E-25 General Standards for Aerospace and Propulsion Systems
538B-1 Hand-Held MicrophoneARINC538B-1 (Current)2/1/1983
This standard describes a hand-held microphone for use with airborne radio installations.
Airlines Electronic Engineering Committee
446 Guidance for Flight Training Device Documentation Structure, Content, and MaintenanceARINC446 (Current)1/1/2016
The intent of this standard is to provide guidance so the documentation provided with the Flight Simulation Training Device (FSTD) reflects and describes the delivered FSTD, including the description and definition of third party equipment and content. In the context of documentation guidance found in this report, the term FSTD is meant to include all levels of flight simulation devices. The documentation described herein is required for the operator to independently support the FSTD in the maintenance, operation, and update of the device throughout the lifetime of the device. This report describes a superset of a possible range of documentation involved in the initial delivery or an update of a FSTD. The deliverable documentation set for a particular FSTD may vary depending on the level of device (e.g., flat panel trainer versus a full flight simulator) as well as issues related to intellectual property, export compliance, technical requirements, and/or contractual agreements.
Flight Simulator Engineering and Maintenance Committee
ELBOW, TUBE, 45°, BULKHEAD, FLARELESS TUBE UNIVERSAL TO FLARED TUBEAS24654B (Current)1/17/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
609 Design Guidance for Aircraft Electrical Power SystemsARINC609 (Current)1/1/1987
This standard describes electrical power system design and performance standards brought about by extensive use of digital avionics. This Report provides guide lines for designers of aircraft power system components and of power utilization components, both avionics and power converters such as motors and heaters.
Airlines Electronic Engineering Committee
Steel Bars, Forgings, Tubing, and Rings 0.48cr 8.0ni 4.0co 0.48mo 0.09v (0.24 - 0.30c) AnnealedAMS6540C (Current)1/15/1979
AMS E Carbon and Low Alloy Steels Committee
670 Guidance for Materials, Processes, and Parts EquivalenciesARINC670 (Current)4/1/2005
Industry rules and guidelines support/mandate equivalency, but provide very little guidance on how to realize MPP substitution. Currently, industry guidelines fail to provide adequate direction to maintenance facilities for material, process, and part equivalencies. Suitable substantiation procedures to be able to select alternate materials are demanded by the air transport industry. The purpose of ARINC Report 670 is to provide clear definitions for materials, processes, parts, substantiation requirements, decision boundaries and limitations, and a standard process for equivalency determination. This report is intended as general guidance for avionics maintenance facilities; however, this does not preclude its use for other sectors of aircraft maintenance as appropriate.
Avionics Maintenance Committee
413A Guidance for Aircraft Electrical Power Utilization and Transient ProtectionARINC413A (Current)10/1/1989
This standard provides guidance to airframe manufacturers concerning the utilization of aircraft electrical power. This standard covers the description of basic power characteristics, and detailed guidance concerning transient protection, interference control, and equipment installation considerations.
Airlines Electronic Engineering Committee
677 Installation Standards for Low Frequency Underwater Locator Beacon (LF-ULB)ARINC677 (Current)7/1/2015
This document provides aircraft installation requirements for a Low Frequency Underwater Locator Beacon (LF-ULB) transmitting on a frequency of 8.8 kHz. ICAO Annex 6 Amendment 36, states that a LF-ULB shall be installed on all aircraft with a maximum certified take-off mass of over 27,000 kg, operating over water at particular distances to land suitable for making an emergency landing. ICAO Annex 6 Amendment 36 further states that an LF-ULB shall be installed by January 1, 2018.
Airlines Electronic Engineering Committee
436-1 Guidelines for Electronic Qualification Test GuideARINC436-1 (Current)9/20/2010
The purpose of ARINC Report 436 is to provide Flight Simulation Training Device (FSTD) users, suppliers and regulatory authorities a set of guidelines for Electronic Qualification Test Guide (eQTG) systems. This document is intended to be supplementary to existing regulatory authority requirements. This document is not designed to direct the use of certain technologies or platforms, but to outline the minimum requirements of an eQTG system. The choice of the technology used to meet these requirements is left to the system's designers and users.
Flight Simulator Engineering and Maintenance Committee
Heat Treatment, Carbon, Low-Alloy and Specialty SteelsAMS2760A (Current)1/1/1987
This specification covers the procedure for through-hardening and related heat treatments of carbon, low-alloy, and specialty steel parts to produce specified mechanical properties within the capability of each respective steel. Heat treating processes such as induction hardening, flame hardening, carburizing, nitriding, austempering, and martempering are recognized processes but are not covered by this specification.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Forgings 4cu 2ni 1.5mg 0.7si as FabricatedAMS4142C (Current)1/1/1991
AMS D Nonferrous Alloys Committee
722 Projection Video System (PVS)ARINC722 (Current)11/5/1980
This standard sets forth design guidance and airplane interfaces for the development and installation of a PVS in commercial transport aircraft. Basic function of the PVS is to display projected television images to each passenger.
Airlines Electronic Engineering Committee
718A-5 Mark 4 Air Traffic Control Transponder (ATCRBS/Mode S)ARINC718A-5 (Current)10/5/2022
Mark 4 Air Traffic Control Transponder (ATCRBS/MODE S) describes an Air Traffic Control Radar Beacon System/Mode Select (ATCRBS/Mode S) airborne transponder with Extended Interface Functions (EIF). The ATC surveillance system is made up of airborne transponders and ground interrogator-receivers, processing equipment, and antenna systems. Mode S is a cooperative surveillance system for air traffic control with ancillary communications capabilities. ARINC 718A supports elementary surveillance. Provisional enhanced surveillance functionality is also defined as a customer option. The Mark 4 transponder, like its predecessor, will support Collision Avoidance System which includes TCAS and ACAS X functions.
Airlines Electronic Engineering Committee
614 Standard Firmware Loader for Avionics ShopsARINC614 (Current)9/1/1989
This standard describes the characteristics of a standard firmware loader for avionic shops. It is capable of copying digital information into memory devices installed in circuit card assemblies, Line Replaceable Modules (LRMs) and On-Board Replaceable Modules (OBRMs). It contains the recommendations of the air transport community concerning the design and development of firmware loader equipment.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
625-4 Industry Guide for Component Test Development and ManagementARINC625-4 (Current)7/27/2020
This standard provides guidance to those who develop avionics test programs and the source documentation on which they are based. This includes guidelines for all steps and phases within the TPS life cycle.
Avionics Maintenance Committee
Aluminum Alloy, Forgings 4.5Cu 0.85Si 0.8Mn 0.5MgAMS4135M (Current)4/1/1986
This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and stock for forgings on rolled rings. Primarily for applications, such as aircraft structural members, requiring material with moderately high strength. Certain design and processing procedures may cause these forgings to become susceptible to stress corrosion cracking; ARP 823 recommends practices to minimize such conditions.
AMS D Nonferrous Alloys Committee
ARINC 834A Internet Protocol Based Aircraft Data Interface Function (ADIF)ARINC834A (Current)2/27/2023
This standard will define the Secure Open Data and Avionics Services (SODAS), the transport layers, and the suggested security mechanisms to enable communication between aircraft systems and an Electronic Flight Bag (EFB). Herein is the definition of a set of protocols and services for the exchange of aircraft avionics data across aircraft networks. The purpose is to define a common set of services to be used to access specific avionics data that will enhance EFB applications.
Airlines Electronic Engineering Committee
CABLE, FIBER OPTIC, SINGLE-MODE, 4.6/125/450 µm, HERMETIC COATED, TIGHT BUFFERAS5382/4B (Current)9/21/2021
AS-3 Fiber Optics and Applied Photonics Committee
Oxygen Cylinder Installation GuideARP5021B (Current)9/13/2024
This document provides guidance for oxygen cylinder installation on commerical aircraft based on airworthiness requirements, and methods practiced within aerospace industry. It covers considerations for oxygen systems from beginning of project phase up to production, maintenance, and servicing. The document is related to requirements of DOT-approved oxygen cylinders, as well to those designed and manufactured to standards of ISO 11119. However, its basic rules may also be applicable to new development pertaining to use of such equipment in an oxygen environment. For information regarding oxygen cylinders itself, also refer to AIR825/12.
A-10 Aircraft Oxygen Equipment Committee
STUD, LOCKED IN-RING LOCKED, SERRATEDAS51989C (Current)9/28/2018
E-25 General Standards for Aerospace and Propulsion Systems
440 Guidelines for the Provisioning and Support of Training Equipment DataARINC440 (Current)10/1/2005
This document provides guidelines for the aviation industry to ensure that data and solutions for training are adequately provided in content and schedule, are cost effective, and are completely supported throughout the life of the equipment. It should be used at all appropriate levels within a company (e.g., Purchasing, Operations, Training) when purchasing or developing new aircraft, major aircraft modifications or training systems.
Flight Simulator Engineering and Maintenance Committee
428 Considerations for Avionics Network DesignARINC428 (Current)10/1/1995
This standard provides the framework for developing a set of requirements for an avionics data bus network. This standard is intended to provide system-level considerations for the development of such a network, which may include a mix of standard data buses and private data buses.
Airlines Electronic Engineering Committee
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