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Aircraft Pressures and Temperatures – Resource DocumentAIR8471 (Current)
This SAE AIR covers Forced Air technology including: reference material, equipment, safety, operation, and methodology. It is intended to provide pressure and temperature (temps pages 26 & 31) information and minimum safety guidelines regarding use of equipment to remove frozen contaminants related to: i) Forced air ii) Forced air/fluid iii) Deicing fluid
G-12M Methods Committee
Aircraft Skin Pressures and TemperaturesAIR8469 (Current)
This information report covers all known aircraft with respect to deicing operations, especially with regard to OEM pressure and temperature limitations on the airframe. It provides data for airlines/operators on compliance with OEM limits and confirms that OEM limits are not exceeded during deicing operations.
G-12M Methods Committee
Missile Hydraulic Pumps and Their Power SourcesAIR560D (Current)
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
Steel, Corrosion-Resistant, Wire, 18Cr - 9.0Ni (302), Spring TemperAMS5688N (Current)6/1/2026
This specification covers a corrosion-resistant steel in the form of wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Functional, Performance, and Safety Guidelines for Tire Pressure Monitoring Systems (TPMS) for AircraftARP6137A (Current)6/1/2026
This SAE Aerospace Recommended Practice (ARP) establishes the overall component and system function guidelines and minimum performance levels for a TPMS. These guidelines include, but are not limited to: Design recommendations for system components, which: Monitor tire inflation Are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment Recommended performance and safety guidelines for a TPMS.
A-5 Aerospace Landing Gear Systems Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, SILVER PLATED, NICKEL ALLOY, UNS N07718, 185 KSI MIN, .2500-28 UNJF-3AAS3251E (Current)5/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
566A-9 Mark 3 VHF Communications TransceiverARINC566A-9 (Current)1/1/1998
Document Status: Legacy This standard defines the characteristics of a VHF Communications Transceiver unit capable of providing voice or data communications capability with the ground. Supplement 8 introduces 8.33 kHz channel spacing.
Airlines Electronic Engineering Committee
542A Digital Flight Data RecorderARINC542A (Current)1/1/1988
Document Status: Legacy This standard includes specific requirements necessary to support flight data recording and other flight data acquisition needs. Design details necessary to ensure interchangeability of equipment in a standard aircraft installation is included.
Airlines Electronic Engineering Committee
603-1 Airborne Computer Data LoaderARINC603-1 (Current)11/1/1985
Document Status: Legacy This standard describes the desired characteristics of a data loader intended for use with airborne computers installed on commercial transport aircraft. The data loader transfers data from a tape cartridge to an avionics computer via an ARINC 429 data bus.
Airlines Electronic Engineering Committee
636 Onboard Local Area Network (OLAN)ARINC636 (Current)1/1/1993
Document Status: Legacy This standard provides general and specific design guidance for the development and implementation of an OLAN for use in an aeronautical Open Systems Interconnection (OSI) communications environment. Only the physical layer and data link layer of the OSI Basic Reference Model (ISO 7498) are specified by this standard.
Airlines Electronic Engineering Committee
421 Guidance for Standard Subdivision of ATA Spec 100 Numbering System for AvionicsARINC421 (Current)10/1/1971
Document Status: Historical This guidance standard was prepared in response to a need stated by air transport operators for uniformity in further subdividing the ATA Spec. 100 number system to better accommodate avionics systems. The ATA numbers are widely used in the maintenance community for inventory control, instruction manuals and equipment modification Service Bulletins.
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
Fiberboard Test ProcedureJ315_202208 (Current)8/26/2022
This SAE Standard provides test methods for determining the critical characteristics of basic or finished fiberboard products. Where applicable, methods of test developed by SAE and ASTM have been referenced.
Textile and Flexible Plastics Committee
Method of Testing Resistance to Crocking of Organic Trim MaterialsJ861_202204 (Current)4/25/2022
This test can be used to determine the resistance to crocking (color rub-off) of organic trim materials such as fabrics, vinyl coated fabrics, leather, coated fiberboard and carpet. This method is similar to AATCC Method 8 –Colorfastness to Crocking.
Textile and Flexible Plastics Committee
Application of Direct Pressure to Resin in Curing of Epoxy and Addition Type PolyimidesARP1927 (Current)6/7/2022
This recommended practice describes the materials, related equipment, and particular processing techniques utilized in process science curing of composite hardware where pressure is imparted specifically to the resin of curing composites. Included as Appendix "A" to this ARP is a discussion of the particular techniques developed for a processing science philosophy which has consistently produced void and porosity-free, large area, thick composite structures.
AMS P17 Polymer Matrix Composites Committee
Composites and Metal Bonding GlossaryAIR4844D (Current)6/13/2024
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures.
AMS CACRC Commercial Aircraft Composite Repair Committee
Portable Controlled Contamination Area (CCA)AIR7522 (Current)12/18/2024
This SAE Aerospace Information Report (AIR) provides guidelines for the design of portable Controlled Contamination Areas (CCAs) that can provide localized environmental control when processing a repair at the airplane or in a hangar environment. The use of a portable CCA may result in a better quality repair. The use of a portable CCA may assist in achieving the environmental requirements for bonded repairs specified in an approved repair procedure. This provides an option to accomplish a repair on nonremovable structure or difficult to remove components.
AMS CACRC Commercial Aircraft Composite Repair Committee
Heat Application for Thermosetting Resin CuringARP5144A (Current)8/14/2023
This SAE Aerospace Recommended Practice (ARP) describes standard methods of heat application to cure thermosetting resins for commercial aircraft composite repairs. The methods described in this document shall only be used when specified in an approved repair document or with the agreement of the Original Equipment Manufacturer (OEM) or regulatory authority.
AMS CACRC Commercial Aircraft Composite Repair Committee
751 Gate-Aircraft Terminal Environment Link (Gatelink) - Aircraft SideARINC751 (Current)1/1/1994
Document Status: Historical This standard describes the electrical and optical interface definitions for Gatelink communications. Gatelink is a 100 Mbps full-duplex communication link between a communication system inside the airport terminal (or at the maintenance position) and a communication system onboard a parked aircraft.
Airlines Electronic Engineering Committee
638 OSI Upper Layer SpecificationARINC638 (Current)2/1/1993
Document Status: Historical This standard provides general and specific guidance for the development and implementation of end system upper layer communication protocols in onboard and air/ground end systems operating in the aeronautical OSI based communications environment.
Airlines Electronic Engineering Committee
637P1-1 Aeronautical Telecommunications Network (ATN) Implementation Provisions, Part 1, Protocols and ServicesARINC637P1-1 (Current)6/1/2000
Document Status: Historical This standard provides general and specific design guidance for the development and installation of the ATN protocols and services needed to route and relay bit-oriented air-ground data link messages in an aviation environment. It applies principles defined in the Open Systems Interconnection (OSI) Reference Model.
Airlines Electronic Engineering Committee
Quality Inspection Procedure, Composites Tracer Fluoroscopy and RadiographyARP1611A (Current)6/5/2022
This document describes an inspection procedure for detecting, by use of a radiographic opaque tracer and fluoroscopy or radiography methods, flaws which have been produced as the result of cutting, machining, or drilling operations in composite or laminate structures.
AMS P17 Polymer Matrix Composites Committee
HOSE, POLYTETRAFLUOROETHYLENE (TFE), HIGH TEMPERATURE AND MEDIUM PRESSURE (1500 PSIG) WITH INTEGRAL SILICONE COMPOSITE FIRE PROTECTIONAS1723A (Current)9/9/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
743 Airborne Global Positioning System ReceiverARINC743 (Current)3/1/1990
Document Status: Legacy This standard provides design guidance for the development of GPS sensors for airline use. It describes the operational capability of the GPS receiver and the standards necessary to ensure interchangeability. GPS provides navigation data to pilots and provides data for use by other aircraft systems.
Airlines Electronic Engineering Committee
579-2 Airborne VOR ReceiverARINC579-2 (Current)8/1/1989
Document Status: Legacy This standard sets the basic requirements for a VOR receiver, whose function is to receive and process VOR signals in the frequency band 108.00 to 117.95 MHz. Provides traditional analog outputs and a digital output of omni bearing.
Airlines Electronic Engineering Committee
656 Avionics Interface Definition for Flight Management and Communications Management FunctionsARINC656 (Current)12/1/1999
Document Status: Legacy A generic data transfer interface is defined for use between avionics computing equipment that exchanges binary message-oriented data. This interface was developed so that various manufacturers can partition Air Traffic Services (ATS) applications and protocols in different manners between various equipment.
Airlines Electronic Engineering Committee
Automated Manufacture of Continuous Multi-Ply Carbon Fiber/Epoxy Resin Impregnated BroadgoodsARP1674A (Current)6/5/2022
This document describes a manufacturing method for processing unidirectional carbon fiber/epoxy resin impregnated sheet and tape into multi-ply broadgoods and tape produced on an automated cross-plying machine. Broadgoods or tape of two or more ply configurations may be processed, where ply orientations of 0°, 45°, 90°, and 135° (as examples) may be automatically layed in a programmed sequence. In all configurations, the 0° ply direction is parallel to the length of the broadgoods roll or sheet, or tape.
AMS P17 Polymer Matrix Composites Committee
605 Users Guide for ARINC 616 Avionics Subset of ATLAS LanguageARINC605 (Current)2/1/1985
Document Status: Legacy This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).This guide has been written as an applications manual for writing avionics test specifications that conform to ARINC Specification 616. It provides advice for converting ATLAS test specifications into ATLAS test programs and implementing them on Automatic Test Equipment (ATE).
Airlines Electronic Engineering Committee, Avionics Maintenance Committee
632 Gate-Aircraft Terminal Environment Link (Gatelink) Ground SideARINC632 (Current)12/1/1994
Document Status: Historical This standard contains necessary definitions and recommendations to implement the gatelink ground system and infrastructure, and provides general and specific guidelines for development and installation of gatelink systems and related communications infrastructure. Gatelink is defined as a high-speed, two-way communication link between a parked aircraft and a ground-based communications system.
Airlines Electronic Engineering Committee
646 Ethernet Local Area Network (ELAN)ARINC646 (Current)12/1/1995
Document Status: Legacy This standard provides general and specific design and implementation guidelines for the use of IEEE 802.3 (ISO/IEC 8802-3) compliant Ethernet Local Area Networks (ELAN) in the commercial avionics environment. Maximum utilization of commercial components (hardware and/or software) and equipment is emphasized.
Airlines Electronic Engineering Committee
Design Considerations for Composite Secondary Structure on Landing GearAIR6827 (Current)1/21/2025
This AIR provides commonly used design considerations for using composite component parts as secondary structures in landing gear applications.
A-5B Gears, Struts and Couplings Committee
Teaching Points for a Class on “Critical Issues in Composite Maintenance, Repair, and Overhaul”AIR5719B (Current)2/13/2026
This document is to be used as a checklist by curriculum developers to create courses or training for critical composite repair, maintenance, and overhaul issues. This document will not take the place of courses or training requirements for specific job roles of a composite repair technician, inspector, or engineer.
AMS CACRC Commercial Aircraft Composite Repair Committee
Recommendations for an Additive Manufacturer Designing/Repairing Aircraft ComponentsARP7043 (Current)8/5/2022
This SAE Aerospace Recommended Practice (ARP) provides recommendations for additive manufacturing (AM) designed/repaired aircraft components.
AMS AM Additive Manufacturing Metals
Sampling, Conformance Strategies, and Recommended Practices for Closed Loop Processing of Powder for Additive ManufacturingARP7302 (Current)4/8/2026
This SAE Aerospace Recommended Practice (ARP) establishes methods and identifies opportunities to sample used powder feedstock circulating within closed loop equipment of an additive manufacturing (AM) process for the purpose of showing conformance to a powder specification. Powder within the entirety of closed loop equipment cannot be represented by sampling and testing of discrete, in-process lots. Because powder processing (i.e., reconditioning, conveyance, and storage) is asynchronous with a build cycle, individual samples and their associated tests do not represent the totality of powder committed to a machine. Powder consumed as part of an individual build cycle may only represent a subset of feedstock in circulation within such equipment. Therefore, regular testing to substantiate conformance to a powder specification is required to assert conforming feedstock was consumed during individual build cycles of the AM workflow to fabricate parts or preforms. Operation of some
AMS AM Additive Manufacturing Metals
407-1 ARINC Synchro System Manual (Combined issue of Report 407 and 407-1, ARINC Synchro Signal Practices)ARINC407-1 (Current)6/1/1961
Document Status: Legacy The Synchro System Manual provides valuable information to designers and maintainers of avionics equipment that employ synchro devices. Synchro theory, synchro applications and signal definitions are included in this standard. Originally published in 1950, it is considered to be the classic guide for synchro devices.
Airlines Electronic Engineering Committee
Recommended Practice to Design for Recycling Proton Exchange Membrane (PEM) Fuel Cell SystemsJ2594_202301 (Current)1/9/2023
While there are various types of Fuel Cell architectures being developed, the focus of this document is on Proton Exchange Membrane (PEM) fuel cell stacks and ancillary components for automotive propulsion applications. Within the boundaries of this document are the: Fuel Supply and Storage, Fuel Processor, Fuel Cell Stack, and Balance of Plant, as shown in Figure 1.
Fuel Cell Standards Committee
Guidelines for Bonded Repair Process Evaluation of Fiber Reinforced Composite StructureAIR6292 (Current)7/15/2024
This SAE Aerospace Information Report (AIR) is a process verification guide for evaluating implementation of key factors in repair of fiber reinforced composite bonded parts or assemblies in a repair shop, hangar, or on-wing environment. This guide is to be used in conjunction with a regulatory approved and substantiated repair and is intended to promote consistency and reliability.
AMS CACRC Commercial Aircraft Composite Repair Committee
Impregnation of Dry Fabric and Ply Lay-UpARP5319 (Current)8/14/2023
This SAE Aerospace Recommended Practice (ARP) describes and gives general guidelines on use and applicability of standard methods for impregnating dry fabric and lay-up of the impregnated plies. The methods of impregnating dry fabric and ply lay-up described in this document have specific application and are not interchangeable. The methods should only be used when specified in an approved repair procedure or with the agreement of the Original Equipment Manufacturer (OEM) or regulatory authority.
AMS CACRC Commercial Aircraft Composite Repair Committee
732-1 Mark 2 Airborne Passenger Audio Entertainment Tape ReproducerARINC732-1 (Current)3/20/1996
Document Status: Legacy This standard defines an airborne tape reproducer for passenger entertainment. The function of this equipment is to play pre-recorded tapes to the passengers through the airplane passenger entertainment system. Some channels may be used for boarding music through the public address system.
Airlines Electronic Engineering Committee
INSPECTION GAGE, FOR AS81790/1 CONNECTORS AIRCRAFT EXTERNAL ELECTRIC POWERAS81790/3A (Current)5/20/2026
AE-8C1 Connectors Committee
Fueling Protocol for Gaseous Hydrogen Powered Heavy Duty VehiclesJ2601/2_202307 (Current)7/6/2023
The purpose of this document is to provide performance requirements for hydrogen dispensing systems used for fueling 35 MPa heavy duty hydrogen transit buses and vehicles (other pressures are optional). This document establishes the boundary conditions for safe heavy duty hydrogen surface vehicle fueling, such as safety limits and performance requirements for gaseous hydrogen fuel dispensers used to fuel hydrogen transit buses. For fueling light-duty vehicles SAE J2601 should be used. SAE J2601-2 is a performance based protocol document that also provides guidance to fueling system builders, manufacturers of gaseous hydrogen powered heavy duty transit buses, and operators of the hydrogen powered vehicle fleet(s). This fueling protocol is suitable for heavy duty vehicles with a combined vehicle CHSS capacity larger than 10 kilograms aiming to support all practical capacities of transit buses. It is non-prescriptive in how to achieve a full fill or 100% state of charge (SOC) in the
Fuel Cell Standards Committee
Lithium and Lithium-Ion Cell and Battery Containment Performance Recommended PracticeJ3303_202510 (Current)10/2/2025
Prescribe test conditions to quantify the effectiveness of containment devices for containing thermal runaway hazards of lithium/lithium-ion cells, batteries, and equipment during storage resulting from the failure of a cell within the container. Due to the many storage locations (indoors, outdoors, etc.), the hazards shall be classified individually to allow for varying performance based on a given storage location.
Battery Transportation and Storage Committee
Outdoor Weathering of Exterior MaterialsJ1976_202205 (Current)5/18/2022
This test method specifies the exposure racks, black boxes, and instrumentation, which shall be used for the outdoor weathering of materials for automotive exterior application.
Textile and Flexible Plastics Committee
Laboratory Testing of Vehicle and Industrial Heat Exchangers for Durability Under Vibration-Induced LoadingJ1598_202605 (Current)5/15/2026
This SAE Recommended Practice is applicable to all liquid-to-gas, liquid-to-liquid, gas-to-gas, and gas-to-liquid heat exchangers used in vehicle and industrial cooling systems. This document outlines the test to determine durability characteristics of the heat exchanger from vibration-induced loading.
Cooling Systems Standards Committee
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings and Stock for Forging, Flash-Welded Rings or Heading, 13Cr - 2.0Ni - 3.0W (Greek Ascoloy), AnnealedAMS5616P (Current)5/9/2026
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 18Cr - 9Ni - 0.21Pb (303Pb) Free-Machining, Solution Heat TreatedAMS5635H (Current)8/22/2023
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Iron-Nickel Alloy, Heat Resistant, Bars, Wire, Forgings, Rings and Stock for Rings and Forgings 44Fe - 18.5Cr - 35.5Ni - 1.1Si Solution Heat TreatedAMS5716L (Current)7/8/2022
This specification covers a heat-resistant iron-nickel alloy in the form of bars, wire, forgings, flash welded rings. Product covered by this specification is limited to 8.0 inches (203 mm) and under in nominal diameter or maximum cross sectional dimension between parallel sides (thickness), and stock of any size for forging or flash welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Cobalt Alloy, Corrosion and Heat-Resistant, Covered Welding Electrodes 51.5Co - 20Cr - 10Ni - 15WAMS5797E (Current)1/2/2018
This specification covers a corrosion and heat-resistant cobalt alloy in the form of covered welding electrodes.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire, 16.5Cr - 4.5Ni - 2.9Mo - 0.10N (AM350)AMS5774F (Current)1/1/2026
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Alloy, Corrosion and Heat Resistant, Welded Tubing 32Fe - 21Cr - 20Ni - 20Co - 3Mo - 2.5W - 1.0Cb (Nb) - 0.15N Solution Heat TreatedAMS5585J (Current)11/9/2021
This specification covers a corrosion and heat resistant alloy in the form of welded and drawn tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion Resistant, Sheet, Strip, and Plate 15Cr - 6.5Ni - 0.75Mo - 0.60Cb - 1.5Cu Solution Heat Treated, Precipitation HardenableAMS5863F (Current)7/23/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
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