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Landing Gear Structural Health MonitoringAIR6168A (Current)7/27/2026
This SAE Aerospace Information Report (AIR) discusses past and present approaches for monitoring the landing gear structure and shock absorber (servicing), opportunities for corrosion detection, methods for transient overload detection, techniques for measuring the forces seen by the landing gear structure, and methods for determining the fatigue state of the landing gear structure. Landing gear tire condition and tire pressure monitoring are detailed in ARP6225, AIR4830, and ARP6137, respectively. Aircraft Brake Temperature Monitoring Systems (BTMS) are detailed in AS1145.
A-5 Aerospace Landing Gear Systems Committee
BEARING, BALL, ANTI-FRICTION, AIRFRAMEAS20218C (Current)7/24/2026
ACBG Rolling Element Bearing Committee
Plain Bearing No-Load Rotational Breakaway Torque MeasurementARP5448/5C (Current)7/24/2026
This test method provides a procedure for measuring no-load rotational breakaway torque of self-lubricating spherical bearings.
ACBG Plain Bearing Committee
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE,CRIMP CONTACTS, (SINGLE INSERT, TYPE IV, CLASS 1,(−65 °C TO +125 °C), SERIES 2, SHELL DESIGNATOR A, CLINCH NUT MOUNTING)AS81659/67B (Current)1/26/2022
AE-8C1 Connectors Committee
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE,CRIMP CONTACTS, (SINGLE INSERT, TYPE IV, CLASS 1,(−65 °C TO +125 °C), SERIES 2, SHELL DESIGNATOR A)AS81659/66B (Current)1/26/2022
AE-8C1 Connectors Committee
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE, CRIMP CONTACTS, QUADRUPLE INSERT, TYPE III, CLASS 1(−65 °C TO +125 °C), SERIES 2, SHELL DESIGNATOR AAS81659/64B (Current)1/28/2022
AE-8C1 Connectors Committee
Hydrogen Embrittlement Effect on Metals By Aircraft Maintenance Chemicals, Mechanical Test MethodsARP1525 (Current)7/1/1977
The Test Procedure of ARP 1525 is Embodied in ASTM F519, Hydrogen Embrittlement Testing of Aerospace Materials. The requirements of the latest issue of ASTM F519 shall be fulfilled whenever reference is made to ARP1525.)
AMS J Aircraft Maintenance Chemicals and Materials Committee
Integrated Flight Instruments and Flight Control SystemsAIR722 (Current)12/16/2002
A-4 Aircraft Instruments Committee
Type 2 15% Graphite Filled Virgin Polytetrafluoroethylene (PTFE) Moldings or ExtrusionsAMS3678/2B (Current)2/29/2016
This specification covers a polytetrafluoroethylene (PTFE) resin filled with 15% 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
Steel, Maraging, Sheet, Strip, and Plate 18Ni - 7.8Co - 4.9Mo - 0.40Ti - 0.10Al Consumable Electrode Melted, Solution Heat TreatedAMS6520E (Current)11/7/2016
This specification covers a premium aircraft-quality, maraging steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
CONNECTORS, ELECTRICAL, RECTANGULAR, RECEPTACLE, CRIMP CONTACTS, (SINGLE INSERT, TYPE IV, CLASS 1, (−65 °C TO +125 °C), SERIES 2, SHELL DESIGNATOR A, FLOAT MOUNTING)AS81659/68B (Current)1/26/2022
AE-8C1 Connectors Committee
A Guide to Landing Gear System IntegrationAIR5451A (Current)9/8/2022
The landing gear system is a major and safety critical airframe system that needs to be integrated efficiently to meet the overall aircraft program goals of minimizing the penalties of weight, cost, dispatch reliability and maintenance. As the landing gear system business develops and large-scale teaming arrangements and acquisitions become increasingly common, it may be desirable in some instances to procure an Integrated Landing Gear System. This document provides guidelines and useful references for developing an integrated landing gear system for an aircraft. The document structure is divided into four sections: Landing Gear System Configuration Requirements (Section 3) Landing Gear System Functional Requirements (Section 4) Landing Gear System Integrity Requirements (Section 5) Landing Gear System Program Requirements (Section 6) The landing gear system encompasses all landing gear structural and subsystem elements. Structural elements include shock struts, truck beams, torsion
A-5 Aerospace Landing Gear Systems Committee
CLAMP, LOOP STYLE, CUSHIONED, WITH WEDGE, PHOSPHATE ESTER FLUID RESISANT, METRICMA2150/2 (Current)4/27/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
TS355 Test for Electrical Connectors Contact Deformation after CrimpingTS355-1 (Current)10/1/1987
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS50 Manufacturing and Inspection Requirements for Alloy Steel 'Jo-Bolt' FastenersTS50-6 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Landing Gear StorageARP5936 (Current)4/23/2021
This document categorizes the different types of storage requirements, either on the aircraft or new unused or overhauled on the shelf, for aircraft landing gears/components. Recommendations and examples of proper landing gear storage are outlined. Reclamation recommendations are provided for aircraft landing gear returning from long-term storage.
A-5 Aerospace Landing Gear Systems Committee
Clamp - Tube Support, Spring Clips and PTFE Cushion, Procurement Specification forMA3399A (Current)4/24/2024
This procurement specification covers the requirements for metal tube support clamps comprising of two spring clips made of corrosion and heat resistant steel and the associated PTFE single split cushion that supports the tube. See Figure 1.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
INVOLUTE SPLINES, SERRATIONS, AND INSPECTIONJ498B_196507 (Current)7/1/1965
Spline Committee -B92
Coupling Assemblies, Non-Locking Probe Style, Self-Aligning, Self-Sealing DisconnectsAS4251A (Current)4/14/2025
This specification establishes the requirements for a probe type self-sealing, self-aligning, non-locking coupling intended for aerospace hydraulic and cooling systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Brake System Road Test Code - Passenger Car and Light-Duty TruckJ843_201303 (Current)3/28/2013
This SAE Recommended Practice establishes a uniform procedure for the level road test of the brake systems of new light-duty trucks and new multipurpose passenger vehicles1 up to and including 2700 kg (6000 lb) GVW and all classes of new passenger cars.
Road Test Procedures Standards Committee
Test Plan for The Digital Time Division Command/Response Multiplex Data Bus Couplers, Terminators, and Data Bus CablesAS4117A (Current)8/10/2017
This test plan defines the requirements of data bus components which comply with the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
AS-1A Avionic Networks Committee
NOx Tracking Parameter AccuracyJ3349_202607 (Current)7/23/2026
This SAE Information Report provides SAE’s recommendations for meeting the requirements for Real Emissions Assessment Logging (REAL) oxides of nitrogen (NOx) accuracy demonstration and for the implementation of REAL NOx binning requirements as defined in onboard diagnostics (OBD) regulations 13 CCR 1971.1 and 13 CCR 1968.2.
Vehicle E E System Diagnostic Standards Committee
Vehicle OBD II Compliance Test Cases for SAE J1979-2/J1979-3J1699/5_202607 (Current)7/23/2026
The primary objective of this recommended practice is to confirm that vehicles can communicate a minimum set of information in accordance with diagnostic test services specified in SAE J1979-2, or the equivalent ISO 14229-1:2013 (Ed. 2) and SAE J1979-3 documents. A successful result using the SAE J1699-5 Automotive Alliance for Innovation (AAI) software for OBD-II testing indicates that the main aspects of UDS communication have been examined, but it does not provide assurance of complete compliance with all aspects of SAE J1979-2 or SAE J1979-3. SAE J1699-5 tests run with a SAE J2534 device hardware and API that is not fully compliant will result in a test failure. This specification takes precedence over all conflicts in the documents cited in this section.
Vehicle E E System Diagnostic Standards 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
Copper-Beryllium Alloy Castings 97Cu - 2.1Be - 0.52Co - 0.28Si Solution Heat Treated (TB00)AMS4890D (Current)1/2/2018
This specification covers a copper-beryllium alloy in the form of sand, investment, or centrifugal castings.
AMS D Nonferrous Alloys Committee
Chemical Milling of Metals, Specification forAMSC81769A (Current)1/5/2015
This specification covers the requirements for surface metal removal of ferrous and non-ferrous metals by milling processes using controlled immersion of parts in chemical etching solutions.
AMS B Finishes Processes and Fluids Committee
Plastic Sheets, Rods and Tubing, Rigid Cast, Methacrylate (Multiapplication)AMSLP391A (Current)8/25/2011
This specification covers methacrylate sheets, rods and tubes produced by casting or machining cast blanks. This specification does not apply to heat-formed and molded or extruded shapes, or shapes made by assembling two or more pieces.
AMS P Polymeric Materials Committee
Inboard Mounted Disc Brake Rotor/Disc Wheel Hub Interface Dimensions - Commercial VehiclesJ2696_202306 (Current)6/27/2023
This SAE Recommended Practice establishes dimensions and tolerances for the interface between inboard mounted disc brake rotors and disc wheel hubs. This document is intended for inboard mounted disc brake rotors and disc wheel hubs for Class 5, 6, 7, and 8 commercial vehicles. Special and less-common applications are not covered.
Truck and Bus Wheel Committee
Engine Electrostatic Gas Path MonitoringAIR4986A (Current)10/28/2009
Turbine engine malfunctions account for a substantial portion of the maintenance actions required to keep both fixed and rotary wing aircraft operational. Undetected incipient component failures can result in secondary engine damage and expensive unscheduled maintenance actions. Recent developments of electrostatic methods now provide the potential for the detection of foreign object ingestion and early detection of distress in gas path components. This SAE Aerospace Information Report (AIR) seeks to outline the history of the electrostatic technique and provides examples of state-of-the-art systems for both inlet and exhaust gas debris monitoring systems along with examples of most recent testing.
E-32 Aerospace Propulsion Systems Health Management
TS17 Performance Specification for Inserts Screw Thread, Metric, Screw Locking Helical Coil, AMS 7246 (Inconel X750) Silver CoatedTS17-2 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS367 Test for Electrical Connectors Contact Retention System Effectiveness (Removable Contact Walkout)TS367-1 (Current)10/1/1987
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
TS156 Performance Specification for Insert Salvage Metric Thinwall Screw Locking, Inconel 718 Silver CoatedTS156-2 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Elastomer: Silicone Rubber, (VMQ) General Purpose 75 – 85 Durometer Type ‘A’ HardnessAMS3305K (Current)4/5/2019
This specification covers a silicone (MQ/VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection of this material.
AMS CE Elastomers Committee
TS4 Performance Specification for All Metal Self Locking Nuts (Unified Threads) 160,000 lbf/in² Min. Tensile (71 tonf/in²) 250°CTS4-5 (Current)12/1/2004
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si - 0.90Cu - 0.60Mn - 0.90Mg Solution Heat Treated and Naturally AgedAMS4405C (Current)4/10/2018
This specification covers an aluminum alloy procured in the form of sheet 0.078 to 0.197 inch (2.00 to 5.00 mm), inclusive, in nominal thickness, Alclad on both sides (see 8.5).
AMS D Nonferrous Alloys Committee
TS147 Silicone Elastomer, Glassfibre Fabric Reinforced Cushion (for Use in Loop Style Clamp Assemblies)TS147-8 (Current)7/1/2015
This technical specification document describes tests that certain parts may be required to meet. For example, this tech spec applies to All parts to TS147. To view suppliers qualified against this standard, visit https://ts200.sae-itc.org/.
Engine and Airframe Technical Standards Committee (TSC)
Ethylene-Propylene-Diene (EPDM) Rubber General Purpose 45 - 55AMS3260D (Current)6/17/2019
This specification covers an ethylene propylene (EPDM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Steel, Bars, Forgings, and Forging Stock 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11) Consumable Electrode Vacuum Re-MeltedAMS6487M (Current)11/23/2021
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Roving, Type "S-2" Glass Epoxy Resin ImpregnatedAMS3832D (Current)12/16/2016
This specification covers continuous, multiple-strand, roving of Type "S-2" glass impregnated with a heat-curable epoxy resin matrix and processed to a "B" stage condition.
AMS P17 Polymer Matrix Composites Committee
Polytetrafluoroethylene Film General Purpose GradeAMS3662D (Current)5/13/2015
This specification covers one grade of polytetrafluoroethylene resin in the form of film.
AMS P Polymeric Materials Committee
Metal Injection Molded Nickel Based Alloy 718 Parts Hot Isostatically Pressed, Solutioned and AgedAMS5917 (Current)6/19/2026
This specification covers a corrosion and heat-resistant nickel alloy in the form of metal injection molded (MIM) parts.
AMS F Corrosion and Heat Resistant Alloys Committee
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
Considerations for Hydrogen Fuel Cells in Airborne ApplicationsAIR7765 (Current)11/18/2019
The scope of this joint EUROCAE/SAE report is to compile the considerations relating to airborne application of hydrogen fuel cells. This document provides a comprehensive analysis of the use of hydrogen as a fuel by describing its existing applications and the experience gained by exploiting fuel cells in sectors other than aviation. The use of hydrogen fuel cells in aircraft can help in meeting aviation environmental targets (including noise pollution) and can be vital to achieving efficient electrically propelled air vehicles. The experience gained with mature fuel cells in terrestrial applications and the handling of other gases in aviation, as presented herein, will help in alleviating safety concerns and in demystifying the usage of hydrogen in aviation.
AE-7F Hydrogen and Fuel Cells
Core, Honeycomb, Glass/Phenolic Bias Weave Fiber ConstructionAMS3716C (Current)8/10/2022
This specification covers expanded honeycomb core made from glass fabric impregnated with phenolic resin and oriented so the fabric weave is on the 45-degree bias with the ribbon direction and supplied in the form of blocks, slices, and ordered shapes.
AMS P17 Polymer Matrix Composites Committee
Quality Program Guidelines for Deicing/Anti-Icing of Aircraft on the GroundARP5646A (Current)6/19/2019
The scope of the Quality Program Guidelines, in the format of a checklist, is to help ensure compliance with the current documents as listed in §2 "Applicable Documents " that meet Airline Operator's and regulatory requirements. It is the responsibility of all other personnel that performs the deicing/anti-icing task to adhere to these requirements.
G-12T Training and Quality Programs Committee
Fiber Optic Wavelength Division Multiplexed (WDM) Singlemode Interconnect and Component Standards Mapping for Aerospace Platform Applications – Device Level SpecificationAIR5667 (Current)10/8/2024
The purpose of this document is to serve as a resource to aerospace designers who are planning to utilize Wavelength Division Multiplexed (WDM) interconnects and components. Many WDM commercial systems exist and they incorporate a number of existing, commercially supported, standards that define the critical parameters to guide the development of these systems. These standards ensure interoperability between the elements within these systems. The commercial industry is motivated to utilize these standards to minimize the amount of tailored development. However, since some of the aerospace parameters are not satisfied by the commercial devices, this document will also try to extend the commercial parameters to those that are necessary for aerospace systems. The document provides cross-references to existing or emerging optical component and subsystem standards. These parameter definitions, test methods, and procedures typically apply to telecommunications application and in some cases
AS-3 Fiber Optics and Applied Photonics Committee
ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONSAS5831 (Current)1/9/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Insulating Components, Molded, Electrical, Heat Shrinkable, Boot, Strain Relief and Sealing, StraightAS5258/1A (Current)2/8/2011
The complete requirements for acquiring the molded components described herein shall consist of this document and the latest issue of AS 5258.
AE-8C1 Connectors Committee
HOSE ASSEMBLY, CONVOLUTED NONMETALLIC, TFE FLARELESS, STRAIGHT TO 45°MA2121 (Current)8/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BRAKING SYSTEM TEST PROCEDURES AND BRAKING PERFORMANCE CRITERIA FOR AGRICULTURAL TRACTORSJ1041_199110 (Current)10/1/1991
The test procedures and performance criteria are directed to operation and parking of agricultural tractors equipped with braking system(s) and having a maximum design speed exceeding 6 km/h. Combinations of agricultural towing machines equipped with braking systems and towed agricultural machines without braking systems are included in this SAE Standard.
Agricultural Tractor Standards Committee (ATSC)
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