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Procedure for Thermal Aging Test for Polyol Ester Gas Turbine Engine LubricantsARP6299A (Current)7/17/2026
This method is intended to evaluate the thermal and oxidative stability of synthetic, ester-based aviation lubricants under defined conditions of time and temperature. This method is applicable to lubricants meeting the compositional and performance requirements of AS5780.
E-34 Propulsion Lubricants Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .2500-28 UNJF-3AAS9677C (Current)7/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
Exposure Levels of UV Radiation in Nondestructive Inspection ProcessesAIR4964A (Current)7/17/2026
Long wave ultraviolet or UV-A irradiation (between 320 and 400 nm) is used for fluorescent inspections in magnetic particle and liquid penetrant examinations. UV-A irradiation is obtained from either LED, fluorescent, or high intensity discharge lamps that are stationary or portable. Commercially available UV-A lamps possess a large variation in intensity output that may introduce a legitimate concern for possible health hazards. This document reviews the nature of UV-A irradiation emitted by lamps and acceptable UV dosage limits adopted by the American Conference of Governmental Industrial Hygienists (ACGIH®) and European Union and recommendation of proper practices when working with UV-A irradiation.
AMS K Non Destructive Methods and Processes Committee
EUROCAE/SAE WG80/AE-7AFC Hydrogen Fuel Cells Aircraft Fuel Cell Safety GuidelinesAIR6464 (Current)7/17/2026
This document defines the technical guidelines for the safe integration of Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS), fuel (considered to be liquid and compressed hydrogen storage types only), fuel storage, fuel distribution and appropriate electrical systems into the aircraft. Editorial Note: Today PEM systems and fuel storage represent the most mature FCS technology and currently forms the basis for this standard. Other types of fuel cell systems and fuels (including reforming technologies and electrolyzers), may be covered by a further update to this document.
AE-7F Hydrogen and Fuel Cells
J1979-DA, Digital Annex of E/E Diagnostic Test ModesJ1979DA_202607 (Current)7/16/2026
The SAE J1979 document set includes the communication between the vehicle's On-Board Diagnostic (OBD) systems and test equipment implemented across vehicles within the scope of regulated emissions and propulsion related OBD. The SAE J1979 Digital Annex supplements the J1979 base documents primarily by maintaining a global registry of regulated emissions and propulsion related data identifiers.
Vehicle E E System Diagnostic Standards Committee
Lighting, Aircraft Interior, Installation ofAS18276B (Current)7/16/2026
This specification covers the installation of aircraft interior lighting for military aircraft.
A-20C Interior Lighting
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
Cobalt Alloy, Corrosion and Heat Resistant, Bars 62Co-28Cr-6Mo Warm-WorkedAMS5918 (Current)5/12/2022
This specification covers a corrosion and heat-resistant cobalt-chromium-molybdenum alloy in the form of bars.
AMS F Corrosion and Heat Resistant Alloys Committee
CAP ASSEMBLY, PRESSURE SEAL, FLARED TUBE FITTINGAS4329A (Current)5/10/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BASKET, REMOVABLE SELF-LOCKING NUT, UNS S66286AS3548A (Current)8/16/2021
E-25 General Standards for Aerospace and Propulsion Systems
Plug, Expansion - Tapered, AMS 5040AS91761A (Current)8/18/2005
No scope available.
E-25 General Standards for Aerospace and Propulsion Systems
800P3-2 Cabin Connectors and Cables, Part 3, Specification of CablesARINC800P3-2 (Current)7/7/2025
This specification describes the general cable and wire characteristics recommended for use in cabin systems for commercial aircraft. Supplement 1 adds new definitions of 26 AWG 2-pair (Quad), 4-pair (Oct) data cables, and copper-fiber optic hybrid composite cables. Supplement 2 includes definitions of shielded twisted pair ethernet over single pair for data rates up to 1000Base-T1.
Airlines Electronic Engineering Committee
Synchro, Torque Transmitter, Type 26V-11TX4CAS20708/6B (Current)6/9/2016
AE-7A Generators and Controls Motors and Magnetic Devices
792-2 Second-Generation Ku-Band and Ka-Band Satellite Communication SystemARINC792-2 (Current)8/25/2023
This standard sets forth the desired characteristics of a second-generation aviation Ku-band and Ka-band satellite communication (satcom) system intended for installation in all types of aircraft.
Airlines Electronic Engineering Committee
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PTFE, METAL BRAID, MEDIUM PRESSURE, BEAM SEAL, 45° TO 90°AS4010A (Current)4/26/2017
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
TEST PROCEDURES FOR EVALUATING BOLT-LOAD RETENTION OF MAGNESIUM ALLOYSUSCAR35-1 (Current)11/19/2020
A bolt-load retention (BLR) test is a practical test to determine the bolt load of a fastener joint with time and at given temperatures. There are three types of BLR tests described in this standard, namely general-purpose test, design-purpose test, and screening material test. A general-purpose BLR test may be used for screening materials, while a design-purpose BLR test is usually used to verify the BLR behavior of a specific joint. The screening material test is an example of the general-purpose test for typical automotive applications.
USCAR
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
CUSHION - TUBE CLAMP SUPPORT, PTFE, METRICMA3296A (Current)10/13/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
763-3 Network Server System (NSS)ARINC763-3 (Current)8/1/2005
The network server system description includes a common file server, data processing, mass storage and interface capabilities to a number of terminals connected via an onboard aircraft Local Area Network (LAN). The Network Server System is a central node through which terminals are able to communicate with avionics systems, access data and applications stored in the NSS mass memory storage.
Airlines Electronic Engineering Committee
Hydrogen Embrittlement Testing of Ultra High Strength Steels and Stampings by Acid ImmersionJ3215_202303 (Current)3/8/2023
This standard describes a test method for evaluating the susceptibility of uncoated cold rolled and hot rolled Ultra High Strength Steels (UHSS) to hydrogen embrittlement. The thickness range of materials that can be evaluated is limited by the ability to bend and strain the material to the specified stress level in this specification. Hydrogen embrittlement can occur with any steel with a tensile strength greater than or equal to 980 MPa. Some steel microstructures, especially those with retained austenite, may be susceptible at lower tensile strengths under certain conditions. The presence of available hydrogen, combined with high stress levels in a part manufactured from high strength steel, are necessary precursors for hydrogen embrittlement. Due to the specific conditions that need to be present for hydrogen embrittlement to occur, cracking in this test does not indicate that parts made from that material would crack in an automotive environment. Results from this test should be
Metals Technical Committee
Bolts and Screws Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Roll Threaded, Stress-Rupture ResistantAMS7467B (Current)1/1/1991
AMS F Corrosion and Heat Resistant Alloys Committee
Covers, Aircraft Components, General Requirements ForAS5778 (Current)11/3/2017
This specification covers general requirements for covers intended to protect the following aircraft parts: Cockpit Fuselage Canopy Engine Armament Propeller or Rotor Miscellaneous
AGE-2 Air Cargo
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, UNS S17400, .1900-32 UNJF-3AAS9732C (Current)3/20/2023
E-25 General Standards for Aerospace and Propulsion Systems
Adhesive Film, Epoxy-Base, High Durability For 175 °C (350 °F) ServiceAMS3695/3 (Current)1/20/2022
This specification covers an adhesive compounded from modified epoxy resins in ready-to-use film supplied in rolls or sheets, either supported by mat or by woven monofilaments or unsupported.
AMS P17 Polymer Matrix Composites Committee
HOSE ASSEMBLY, CONVOLUTED NONMETALLIC, TFE FLARELESS, STRAIGHT TO 45°MA2121 (Current)8/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, RUBBER, FLARELESS, FIELD ATTACHABLE FITTING, 45° TO 90°AS1867A (Current)9/17/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Performance Classification of Headlamp Outer LensesJ3086_202308 (Current)8/22/2023
This SAE Recommended Practice is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances. This document establishes performance requirements and guidelines for coating materials and plastic substrate testing.
Lighting Materials Standards Committee
WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYIMIDE INSULATED, SMOOTH SURFACE, LIGHT WEIGHT, NICKEL-COATED COPPER CONDUCTOR, 260 °C, 600 VOLTS ROHSAS22759/192A (Current)10/24/2019
AE-8D Wire and Cable Committee
716-11 Airborne VHF Communications TransceiverARINC716-11 (Current)6/10/2003
This standard sets forth characteristics of a VHF Communications Transceiver for installation in all types of commercial transport aircraft. The VHF transceiver can support 8.33 kHz AM or 25 kHz AM voice or ACARS (2400 bps) data communications.
Airlines Electronic Engineering Committee
664P2-3 Aircraft Data Network, Part 2, Ethernet Physical and Data Link Layer SpecificationARINC664P2-3 (Current)10/24/2018
This specification provides Ethernet physical parameters and data link layer specifications for use in a commercial aircraft environment. This specification provides general and specific guidelines for the use of IEEE 802.3 compliant Ethernet, 2000 edition. Physical layer and Medium Access Control (MAC) sub-layers are expected to comply with the Open System Interconnection (OSI) Reference Model to enable maximal utilization of off-the-shelf components, both hardware and software, for aviation use. The Ethernet Physical layer specification defines the electrical and optical parameters for the 10BASE-T, 100BASE-TX, and 100BASE-FX Ethernet implementations. This specification references ARINC Specification 600: Air Transport Avionics Equipment Interfaces for definition of copper-based implementations of the Ethernet Physical layer.
Airlines Electronic Engineering Committee
742 Design Guidance for Windshear Warning and Guidance Equipment LanguageARINC742 (Current)1/27/1988
This standard describes stand-alone windshear warning system comprised of a windshear warning computer and associated cockpit displays. The system uses data pertaining to aircraft movement with respect to air movement to detect and annunciate a windshear condition. As an option, it may also provide instrument guidance to the crew indicating optimum pitch to endure the windshear encounter.
Airlines Electronic Engineering Committee
728 Avionics Refrigeration Cooling System (ARCS)ARINC728 (Current)10/31/1979
This standard provides standards for the in accordance with which aircraft operators and manufacturers can order avionics refrigeration units and can design installations for an ARCS.
Airlines Electronic Engineering Committee
Network End-to-End Data Link Evaluation System Transceiver Health MonitoringAIR6552/3 (Current)12/22/2020
This document establishes methods to obtain, store, and access data about the health of a fiber optic network using commercial sensors located in or near the transceiver. This document is intended for: Managers, Engineers, Contracting Officers, Third Party Maintenance Agencies, and Quality Assurance.
AS-3 Fiber Optics and Applied Photonics Committee
714-6 Mark 3 Airborne SELCAL SystemARINC714-6 (Current)8/15/1990
Ground-to-air selective calling system characteristics are defined by this standard. The system allows selective calling of individual aircraft over radio communications circuits linking the ground station to the aircraft. Elements comprising overall system are ground selecting calling unit (coder), ground-to-air transmitter (HF or VHF), airborne receiver (HF or VHF), airborne selective calling unit (decoder), and code selection panel.
Airlines Electronic Engineering Committee
CLIP, SPRING RETENTION - ELECTRICAL CABLEAS5117A (Current)2/13/2026
SCOPE IS UNAVAILABLE.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock, 0.50Cr - 0.12Mo (0.89 - 1.01C)AMS6476G (Current)7/8/2026
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging or tubing stock.
AMS E Carbon and Low Alloy Steels Committee
FITTING ASSEMBLY, ELBOW, 90°, BULKHEAD FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSIAS5805B (Current)5/5/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For (Supplement 1)AS85421SUP1A (Current)7/7/2026
This supplement forms a part of SAE Aerospace Specification AS85421. It shall be used to identify fitting standards citing this procurement specification.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING ASSEMBLY, CROSS, AXIALLY SWAGED, HYDRAULIC, 5080 PSIAS5973B (Current)6/2/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING ASSEMBLY, ELBOW, 45°, FEMALE FLARELESS, AXIALLY SWAGED, HYDRAULIC, 3000 PSIAS5803B (Current)5/6/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, POLYETRAFLUOROETHYLENE, PTFE, METAL BRAID, MEDIUM PRESSURE, BEAM SEAL, 90° TO 90°AS4011A (Current)4/26/2017
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aluminum Alloy, Rolled or Cold-Finished, Bars, Rods, Wire, and Flash-Welded Rings, Annealed, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O)AMS4115L (Current)6/19/2026
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, wire, and flash-welded rings and of stock for flash-welded rings.
AMS D Nonferrous Alloys Committee
STUD, STEPPED, 2.5 DIA ENGAGEMENT, PD SHANK, AMS5731, .5625-18 UNJF-3A X .500-20 UNJF-3AAS3144B (Current)3/29/2022
E-25 General Standards for Aerospace and Propulsion Systems
Gas Turbine Engine Inlet Flow Distortion GuidelinesARP1420C (Current)4/27/2017
The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion. Practices employed to quantify these effects continue to develop and, therefore, periodic updates are anticipated. The effects of other forms of distortion on flow stability and performance, and of any distortion on aeroelastic stability are not addressed. The guidelines can be used as necessary to create a development method to minimize the risk of inlet/engine compatibility problems. The degree to which guidelines for descriptor use, assessment techniques, and testing outlined in this document are applied to a specific program should be consistent with the expected severity of the compatibility problem.
S-16 Turbine Engine Inlet Flow Distortion Committee
PIN, STRAIGHT, HEADED, .0937 DIAMETER, UNS S41800AS9842B (Current)4/23/2024
E-25 General Standards for Aerospace and Propulsion Systems
CABLE, LIGHTWEIGHT OPTIMIZED HIGH SPEED DATA QUAD, 110 OHM, 200 °CAS6070/8A (Current)5/7/2019
AE-8D Wire and Cable Committee
Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Tin-Coated Copper Conductor, 600-Volt, 110°CAS50861/5A (Current)12/7/2017
AE-8D Wire and Cable Committee
Heat Treatment of Steel Raw MaterialsAMS2761 (Current)7/8/2020
This specification establishes general requirements for the heat treatment of steel raw material (see 8.2.1) by producers or for producers.
AMS E Carbon and Low Alloy Steels Committee
Requirements for Developing and Qualifying Alternate Inspection Frequency PlansAS13002 (Current)3/17/2015
This document covers the process to be applied to design characteristics (as defined in AS9102), parts or inspection processes as defined by the purchaser. Design characteristics not included within the scope include electronic, electromechanical or mechanical systems where alternative means of acceptance are approved such as through acceptance test procedures (ATPs). This document does not define processes for identifying or communicating the classification of the parts or design characteristics. This document does not define the procedure to qualify a supplier to undertake these requirements. It is expected that each purchaser will have a procedure to manage the flow-down of these requirements. This document applies to suppliers that demonstrate adequate proficiency in applicable process control methods as determined by the purchaser.
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
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