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Helicopter Engine-Rotor System CompatibilityARP704A (Current)7/2/2026
This SAE Aerospace Recommended Practice (ARP) recommends a methodology to be used for the design, analysis and test evaluation of modern helicopter gas turbine propulsion system stability and transient response characteristics. This methodology utilizes the computational power of modern digital computers to more thoroughly analyze, simulate and bench-test the helicopter engine/rotor system speed control loop over the flight envelope. This up-front work results in significantly less effort expended during flight test and delivers a more effective system into service. The methodology presented herein is recommended for modern digital electronic propulsion control systems and also for traditional analog and hydromechanical systems.
S-12 Powered Lift Propulsion Committee
ARINC 834A-1 Internet Protocol Based Aircraft Data Interface Function (ADIF)ARINC834A-1 (Current)7/2/2026
This standard defines the services, 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. Supplement 1 introduces bi-directional communication between the EFB and FMS. It also enables mutual Transport Layer Security, incorporating client authentication.
Airlines Electronic Engineering Committee
Aircraft Flight Control Actuation System Failure-Detection MethodsAIR5273A (Current)12/16/2022
This SAE Aerospace Information Report (AIR) provides descriptions of aircraft flight control actuation system failure-detection methods. The fault-detection methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight controls.
A-6A3 Flight Control and Vehicle Management Systems Cmt
Aluminum Alloy Alclad 2014, Plate and SheetAMSQQA250/3A (Current)3/6/2014
This specification covers the specific requirements for 2014 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (2014) core with thin layers of an aluminum alloy (6003) anodic to the core and of approximately equal thickness bonded to both surfaces.
AMS D Nonferrous Alloys Committee
Passenger Reading LightsARP378E (Current)5/17/2023
This document presents criteria for design and location of passenger reading lights in commercial aircraft. For LED reading light requirements, see ARP5873, titled: LED Passenger Reading Light Assembly.
A-20C Interior Lighting
644 Portable Maintenance Access Terminal (PMAT)ARINC644 (Current)5/1/1993
This standard contains the electrical interface definition, and a functional description of a PMAT. The intent of this standard is to provide general and specific design guidance for the development of a PMAT primarily for airline use.
Airlines Electronic Engineering Committee
Coating, Cadmium (Vacuum Deposited)AMSC8837A (Current)10/22/2015
This specification covers the requirements for three types and three classes for vacuum deposited cadmium coating.
AMS B Finishes Processes and Fluids Committee
Type 7 Virgin Polytetrafluoroethylene (PTFE) Moldings or Extrusions with 25% Carbon and GraphiteAMS3678/7B (Current)2/29/2016
This specification covers a polytetrafluoroethylene (PTFE) resin filled with carbon and graphite in the form of extruded or molded rods or tubes which are sintered after molding or, in the case of extrusions, sintered during the extrusion process.
AMS P Polymeric Materials Committee
Bolts, Screws, and Studs, Geometric Control RequirementsAS3063C (Current)4/10/2024
This SAE Aerospace Standard (AS) establishes the geometric control requirements for bolts, screws, and studs where worded notes and symbolized notes are used for straightness, concentricity, squareness, and runout.
E-25 General Standards for Aerospace and Propulsion Systems
Heat Treatment of Aluminum Alloy CastingsAMS2771F (Current)4/11/2017
This specification covers the engineering requirements for heat treatment of aluminum alloy castings and for parts machined from castings.
AMS D Nonferrous Alloys Committee
437-1 Guidelines For Training FacilitiesARINC437-1 (Current)11/7/2012
The purpose of ARINC Report 437 is to provide guidance when planning a new training facility, extending an existing training facility, or adding new equipment to an existing facility.
Flight Simulator Engineering and Maintenance 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
791P1-3 Mark I Aviation Ku-Band and Ka-Band Satellite Communication System, Part 1, Physical Installation and Aircraft InterfacesARINC791P1-3 (Current)9/19/2019
This standard sets forth the desired characteristics of Aviation Ku-band Satellite Communication (Satcom) and Ka-band Satcom Systems intended for installation in all types of commercial air transport aircraft. The intent of this characteristic is to provide guidance on the interfaces, form, fit, and function of the systems. This document also describes the desired operational capability of the equipment needed to provide a broadband transport link that can be used for data, video, and voice communications typically used for passenger communications and/or entertainment. The systems described in this characteristic are not qualified, at this writing, for aviation safety functions.
Airlines Electronic Engineering Committee
Aluminum Alloy, Forgings 7.8Zn - 2.2Mg - 1.6Cu - 0.15Cr (7249-T74 and -T7452)AMS4334B (Current)4/21/2017
This specification covers an aluminum alloy in the form of die forgings, hand forgings, and forging stock.
AMS D Nonferrous Alloys 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
607-3 Design Guidance for Avionics EquipmentARINC607-3 (Current)8/1/1998
This standard provides general guidelines for the design of avionics equipment. It represents the desires of the airline industry resulting from extensive airline experience. Manufacturers are urged to use this standard when initially starting the design of new equipment. Airplane Personality Module (APM) specifications are included.
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
Rubber Cellular Sheet, Molded and Hand-Built Shapes; Latex FoamAMSR5001A (Current)4/13/2015
This specification covers cored and uncored open cell latex foam rubber sheets, molded and hand- built shapes having good shock-absorbing, vibration-damping, and comfort cushioning characteristics (see 6.1).
AMS P Polymeric Materials 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
Sealing Compound, Silicone Rubber, Two-Part, Electrically Conductive and Corrosion Resistant (Nonchromated) for Use from -67 to 500 °F (-55 to 260 °C)AMS3262A (Current)9/23/2011
This specification covers a silicone, electrically conductive and corrosion-inhibiting sealing compound.
AMS G9 Aerospace Sealing Committee
613 Guidance for Using the Ada Programming Language in Avionics SystemsARINC613 (Current)1/1/1988
In 1986 the airlines selected Ada as the high-order development language for avionics. ARINC 613 describes the Ada domain most suited for avionics software development. The standard provides valuable guidance to Ada compiler developers and Ada programmers.
Airlines Electronic Engineering Committee
791P2-2 Mark I Aviation Ku-Band and Ka-Band Satellite Communication System, Part 2, Electrical Interfaces and Functional Equipment DescriptionARINC791P2-2 (Current)1/29/2024
This document (ARINC Characteristic 791, Part 2) provides the non-networking interface definition of the Mark I (ARINC 791) and Mark II (ARINC 792) Ku-Band and Ka-Band Satellite Communication (satcom) system intended for passenger entertainment on commercial transport aircraft. ARINC Characteristic 791 Part 1 of this document provides an overview of Ku-band and Ka-band satcom systems. System provisions, including Line Replaceable Unit (LRU) form factors, attachments, cooling, and inter-system wiring, are defined. Signals between the Modem/Modem Manager (Modman) and the Antenna Subsystem are described to permit interchangeability between any Modman and any Antenna Subsystem. ARINC Characteristic 791 Part 2 of this document provides the non-networking interface definition of the satcom system. Any signal crossing into or out of the communication system is documented to ease aircraft integration. Signals within the satcom system, and in particular, between the Modman and the Antenna
Airlines Electronic Engineering 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
CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, ENVIRONMENT RESISTANT, REMOVABLE CRIMP CONTACTS, BACKSHELL, SHIELD TERMINATING, (SERIES A AND B)AS29600/2A (Current)8/14/2014
AE-8C1 Connectors Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Powder for Additive Manufacturing 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18FeAMS7006 (Current)3/21/2022
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 μm) and that no powder (0.0 wt%) greater than 40 mesh (425 μm) is allowed.
AMS AM Additive Manufacturing Metals
Aluminum Alloy Bar, Rod, and Shapes, Extruded, 7075-T76 Improved Exfoliation ResistanceAMSQQA200/15B (Current)7/31/2013
This specification covers the specific requirements for aluminum alloy 7075-T76 bar, rod, and shapes produced by extrusion (See AMS-QQ-A-200/11 for specific requirements for 7075 extrusions in other tempers).
AMS D Nonferrous Alloys Committee
Synchro, Torque Differential Receiver, Type 31TDR6BAS20708/67B (Current)4/18/2017
AE-7A Generators and Controls Motors and Magnetic Devices
Steel Castings, Tubular, Centrifugal, Corrosion Resistant 15Cr - 4.6Ni - 0.22 (Cb+Ta) - 2.8Cu Solution Heat TreatedAMS5348C (Current)4/4/2017
This specification covers a corrosion-resistant steel in the form of tubular centrifugal castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Cloth, Glass Finished for Resin LaminatesAMS3824C (Current)10/4/2022
This specification covers “E” glass in the form of woven cloth.
AMS P17 Polymer Matrix Composites Committee
Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03LaAMS7013 (Current)1/3/2019
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt.%) greater than 40 mesh (425 µm) is allowed.
AMS AM Additive Manufacturing Metals
Silicone Rubber Compound Room Temperature Vulcanizing, 50,000 Centipoise Viscosity Durometer 30 - 45AMS3363E (Current)1/17/2012
This specification covers a silicone rubber in the form of a two-component liquid compound.
AMS G9 Aerospace Sealing Committee
Measurement Uncertainty and Consumer RiskAIR6553 (Current)1/28/2026
This document addresses measurement uncertainty and consumer risk as they relate to AS8879 thread inspection. It describes the rationale, theory and methodology used to generate the technical content of the AS5870. The document describes how to calculate measurement consumer risk. It documents all of the calculation methods which industry employs today to calculate what is commonly called measurement uncertainty (Appendices A, B, C, D, E and F). These, in turn, are used to calculate measurement uncertainty ratios which are required inputs to calculate measurement consumer risk. Users of this document can apply the information described herein for the evaluation of the capability of their measurements based on the measurement consumer risk. It involves the analysis of the measurement (product) distribution and biases of both the product and measurement system distributions. It protects the consumer from the worst case distribution results.
E-25 General Standards for Aerospace and Propulsion Systems
Rivets, Blind, Corrosion Resistant Alloy 67Ni - 31Cu Procurement Specification ForAS7234A (Current)4/23/2024
This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivets.
E-25 General Standards for Aerospace and Propulsion Systems
Aluminum Alloy, Bars, Rods, and Wire 4.4cu 1.5mg 0.60mn Rolled, Drawn, Or Cold FinishedAMS4112D (Current)1/1/1996
This specification has been declared 'CANCELLED' by the Aerospace Materials Division, SAE, as of January 1996. Alloy: 2024-T6 UNS Number: A92024
AMS D Nonferrous Alloys Committee
NUT, SELF-LOCKING, 12 POINT, REDUCED HEIGHT, SILVER PLATE, UNS S66286, CLASS 160 KSI/1200 °FAS3485C (Current)2/13/2026
E-25 General Standards for Aerospace and Propulsion Systems
Aluminum Alloy Castings, Sand, 6.8Mg - 0.18Ti - 0.18Mn (535.0-F), As CastAMS4238E (Current)9/22/2006
This specification covers an aluminum alloy in the form of sandcastings.
AMS D Nonferrous Alloys Committee
350 °F Autoclave Cure, Low Flow Toughened Epoxy Prepregs, Type 35, Class 1, Grade 190, Fiber 1AMS3961/3 (Current)12/2/2015
The intent of this specification is for the procurement of the material listed on the QPL and, therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall refer to the Quality Assurance section of the base specification, AMS3961. All material qualification and equivalency data has been archived and is available for review upon request. Contact the CMH-17 Secretariat (www.cmh17.org) for additional information.
AMS P17 Polymer Matrix Composites Committee
Aluminum Alloy 5086, Plate and SheetAMSQQA250/7A (Current)2/15/2007
This specification covers the specific requirements for 5086 aluminum alloy plate and sheet; the general requirements are covered in AMS-QQ-A-250.
AMS D Nonferrous Alloys Committee
Chloroprene (CR) Rubber Weather Resistant 45 - 55AMS3208N (Current)3/18/2014
This specification covers a chloroprene (CR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers 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)
Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 25Cr - 20Ni (310S) Solution Heat TreatedAMS5521K (Current)3/1/2019
This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Acrylonitrile Butadiene (NBR) Rubber Aromatic Fuel Resistant 35 - 45AMS3214M (Current)7/3/2019
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Flux, Brazing, High TemperatureAMS3417C (Current)10/31/2007
This specification covers a high temperature brazing flux in the form of paste or powder.
AMS B Finishes Processes and Fluids Committee
MINIMUM PERFORMANCE STANDARD ANGLE OF ATTACK EQUIPMENTAS8046 (Current)8/4/2022
This SAE Aerospace Standard (AS) establishes the minimum performance requirements for an angle of attack (AOA) system.
A-4ADWG Air Data Subcommittee
Synthetic Rubber and Cork Composition General Purpose FirmAMS3252K (Current)9/23/2011
This specification covers a synthetic rubber and cork composition in the form of sheet, strip, and molded shapes.
AMS CE Elastomers Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire 27Cr - 21.5NiAMS5694K (Current)11/18/2022
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Laminated Sheet, Aluminum Alloy, Aramid Fiber Reinforced 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (Alclad, One Side 7475-T761) 5 or 7 PlyAMS4258B (Current)5/25/2017
This specification covers an aluminum alloy in the form of sheet laminated with two or more layers of unidirectional aramid fiber/epoxy prepreg.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, 2024, Bar, Rod, and Wire; Rolled, Drawn, or Cold FinishedAMSQQA225/6B (Current)3/4/2018
This specification covers the specific requirements for 2024 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing.
AMS D Nonferrous Alloys Committee
Insulating Compound, Electrical, Ceramic, Class LAMSI10A (Current)6/29/2016
This specification covers class L, low dielectric constant (12 or under), ceramic, electrical, insulating compounds, for use in electronic, communications, and allied electrical equipments, and the grading thereof (see 6.1).
AMS P Polymeric Materials Committee
Continuous Identification Marking of Iron and Steel ProductsAMSSTD183A (Current)1/30/2003
This standard establishes uniform physical item identification marking in constantly recurring symbols for selected iron and steel products which are procured and issued for Government agencies. Shipment and inspection acceptance marking are not within the scope of this standard. The marking requirements of this standard are applicable when included in the item specification or individual contract. Government decision to include the marking requirements of this standard in a Government specification for iron and steel products shall be subject to coordination between the Government and the iron and steel industry.
AMS E Carbon and Low Alloy Steels Committee
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