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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
BOLT, MACHINE - DOUBLE HEXAGON, EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, UNS N07001, 165 KSI, .4375-20 UNJF-3AAS9727A (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
WASHER, KEY - 90°, LOCKING, CRES, UNS S32100AS9581D (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3AAS9676C (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, STEEL SAE 8740, CADMIUM PLATED, 125 KSI MIN UTS, .4375-20 UNJF-3AAS9918C (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
Driveline Parking Brake Test Procedure for Medium Duty VehiclesJ2690_202606 (Current)6/3/2026
This SAE Recommended Practice establishes uniform test procedures for friction based parking brake components used in conjunction with hydraulic service braked vehicles with a gross vehicle weight rating greater than 4500 kg (10 000 lb). The components covered in this document are the primary actuation and the foundation park brake. Various peripheral devices such as application dashboard switches or indicators are not included. These test procedures include the following: a Brake Related Tests 1 Brake Functional Performance 2 Brake Dynamic Torque Performance 3 Brake Corrosion Resistance 4 Brake Endurance with Torque 5 Brake Endurance without Torque 6 Vibration Resistance 7 Brake Ultimate Static Load 8 Brake Lining Wear Adjuster Function b Actuation Related Tests 1 Mechanical Actuator Functional Performance 2 Mechanical Actuator Endurance 3 Mechanical Actuator Quick Release 4 Mechanical Actuator Ultimate Load 5 Spring Apply Actuator Functional Performance 6 Spring Apply Actuator
Truck and Bus Hydraulic Brake 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
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
J1979-DA, Digital Annex of E/E Diagnostic Test ModesJ1979DA_202508 (Current)5/27/2026
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
Electric Vehicle Test ProcedureJ227_199212 (Current)2/9/2009
Light Duty Vehicle Performance and Economy Measure Committee
Automatic Transmissions - Schematic DiagramsJ647_202512 (Current)12/1/2025
The following schematic diagrams reflect various methods of illustrating automotive transmission arrangements. These have been developed to facilitate a clear understanding of the functional interrelations of the gearing, clutches, hydrodynamic drive unit, and other transmission components. Two variations of transmission diagrams are used: in neutral (clutches not applied) and in gear. For illustrative purposes, some typical transmissions are shown.
Automatic Transmission and Transaxle Committee
Low Speed Thorax Impact Test Procedure for the HIII 50th Male DummyJ2779_202206 (Current)6/29/2022
Dummy Testing and Equipment Committee
Mobile Crane Working Area DefinitionsJ1028_202209 (Current)9/1/2022
This SAE Recommended Practice applies to stationary usage of mobile construction-type cranes, crawler or rubber-tire mounted, on outriggers or on tires, when used for lifting, clamshell, dragline, magnet, pile driver, or similar service.
Cranes and Lifting Devices Committee
Passenger Car and Light Truck Tire Dynamic Driving Traction in SnowJ1466_200102 (Current)4/12/2001
This SAE Recommended Practice defines the best known techniques for evaluating dynamic passenger car and light truck tire driving traction in snow. There are many snow conditions which a typical driver will encounter that are not specifically addressed in this Recommended Practice. Dynamic driving traction in this Recommended Practice is under a narrow, controlled range of conditions of temperature, snow compaction and depth (commonly called the 'Test Window') to minimize test variability. Tire rankings may differ on other types of snow and ice conditions.
Highway Tire Committee
Manual Slack Adjuster Test ProcedureJ1461_201404 (Current)4/28/2014
This SAE Recommended Practice is intended for testing of manual slack adjusters as they are used in service, emergency, or parking brake systems for vehicles that can be licensed for on-road use.
Truck and Bus Foundation Brake Committee
Digital Annex of Diagnostic Trouble Code Definitions and Failure Type Byte DefinitionsJ2012DA_202510 (Current)10/24/2025
The J2012 Digital Annex of Diagnostic Trouble Code Definitions Spreadsheet provides DTC information in an excel format for use in your organization's work processes. The column headings include the same information as contained in the J2012 standard. Information in the excel spreadsheet will be updated several times annually and the spreadsheet includes a column heading denoting which DTCs have been updated in the current version.
Vehicle E E System Diagnostic Standards Committee
Engine Rotation and Cylinder NumberingJ824_202206 (Current)6/29/2022
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry.
Engine Power Test Code Committee
Tubing, Polyolefin Plastic, Electrical Insulation Selectively Crosslinked, Semi-Rigid, Heat-ShrinkableAMS3634E (Current)1/16/2012
This specification covers an irradiated, thermally-stabilized, modified-polyolefin plastic in the form of dual-wall tubing.
AMS P Polymeric Materials Committee
FITTING END, FLARELESS, BLUNT NOSE, DESIGN STANDARDAS4458B (Current)4/20/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Elastomer: Acrylonitrile Butadiene Rubber (NBR) Aromatic Fuel Resistant 55 to 65 Type ‘A’ Durometer Hardness For Products in: Aromatic and Aliphatic Fuel SystemsAMS3212R (Current)4/28/2020
This specification covers an Acrylonitrile Butadiene Rubber (NBR) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. For molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications, use the AMS7000 series specification.
AMS CE Elastomers Committee
FLANGE END, FEMALE, TYPE I STANDARD PROFILE DESIGN STANDARDAS1895/13E (Current)3/4/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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, Corrosion-Resistant, Welding Wire 17Cr - 7.1Ni - 1.0AlAMS5824G (Current)10/7/2022
This specification covers a corrosion-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion Resistant, Seamless Tubing, 19Cr - 10Ni (304), Solution Heat TreatedAMS5560P (Current)1/21/2022
This specification covers a corrosion-resistant steel in the form of seamless tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
Tube Fittings, Aerospace Fluid Systems, Separable, for 24 Degree Cone, General Specification, Metric (ISO 7169)MA2005C (Current)6/10/2021
This document specifies performance and quality requirements for the qualification and manufacture of 24 degree cone fittings to ensure reliable performance in aircraft hydraulic systems. This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines. This document covers fittings of temperature types and pressure classes specified in MA2001.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
GASKET - TYPE XII, XIV-A, AND XIV-B ENGINE ACCESSORY DRIVEAS100003D (Current)1/3/2013
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Corrosion and Heat-Resistant, Welding Wire 16.4Cr - 4.8Ni - 0.22Cb (Nb) - 3.6Cu Consumable Electrode or Vacuum Induction MeltedAMS5803H (Current)10/19/2021
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Inspection, Ultrasonic, of Thin Materials 0.50 Inch (12.7 mm) and Under in Cross-Sectional ThicknessAMS2632C (Current)6/2/2022
This specification covers the procedure for ultrasonic inspection of flat, contoured, round, and hollow cylindrical products having a cross-sectional thickness of 0.02 to 0.50 inch (0.5 to 12.7 mm). This specification does not apply to inspection of composite materials.
AMS K Non Destructive Methods and Processes Committee
Titanium Alloy, Welding Wire, 6AI - 2Sn - 4Zr - 2MoAMS4952H (Current)4/25/2026
This specification covers a titanium alloy in the form of welding wire (see 8.5).
AMS G Titanium and Refractory Metals Committee
ALUMINUM ALLOY SHEET AND PLATE 3.5Mg - 0.25Cr (5154-H32)AMS4019A (Current)1/2/1989
AMS D Nonferrous 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
Rivets-Aluminum 99alAMS7220E (Current)10/1/1990
AMS D Nonferrous Alloys Committee
Alloy Pm Shapes, Corrosion, Wear, and Heat Resistant 60co 29cr 4.5w (0.90-1.40c)AMS7239B (Current)5/1/2001
This specification covers a corrosion, wear, and heat resistant cobalt alloy in the form of powder-metallurgy shapes.
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
Aluminum Alloy, Extrusions, 4.4Cu - 1.5Mg - 0.60Mn (2024-O), AnnealedAMS4421A (Current)12/4/2024
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross-sectional area of 32 square inches (206 cm2), maximum (see 8.5).
AMS D Nonferrous Alloys Committee
Low Voltage Primary CableJ1128_202508 (Current)8/22/2025
This SAE Standard covers low voltage primary cable intended for use at a nominal system voltage of 60 VDC (25 VAC) or less in surface vehicle electrical systems. The tests are intended to qualify cables for normal applications with limited exposure to fluids and physical abuse.
Cable Standards Committee
FITTING ASSEMBLY, ELBOW 45°, REDUCER AND NONREDUCER, INTERNAL FLARE TO FLARED TUBEAS4409E (Current)5/2/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Software Life Cycle Processes – Implementation ConsiderationsIEEEEIA12207_2 (Current)7/1/2015
This guide provides implementation consideration guidance for the normative clauses of IEEE/EIA 12207.0. The guidance is based on software industry experience with the life cycle processes presented in IEEE/EIA 12207.0.
Systems Management Council
Yarn, Organic Fiber (Para-Aramid), High Modulus 380 Denier, (420 d tex), 0.6% FinishAMS3901/2D (Current)7/30/2014
This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.
AMS P17 Polymer Matrix Composites Committee
BOLTS AND SCREWS, LOW-ALLOY STEEL Heat Treated, Roll ThreadedAMS7452L (Current)5/1/1995
AMS E Carbon and Low Alloy Steels Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb [Nb] + Ta) - 2.5Ti - 0.70Al - 7.0Fe (X750) Consumable Electrode, Remelted or Vacuum Induction Melted, Solution Heat Treated, Precipitation-HardenableAMS5598G (Current)7/15/2024
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet and strip up to 0.187 inch (4.75 mm) thick, inclusive, and plate up to 4.000 inches (101.6 mm) thick, inclusive.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion and Heat Resistant, Seamless Tubing 23Cr - 13.5Ni (309S) Solution Heat TreatedAMS5574F (Current)7/31/2019
This specification covers a corrosion and heat resistant steel in the form of seamless tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
System EngineeringSYSB1 (Current)7/1/2015
G-47 Systems Engineering
Failure Mode and Effect AnalysesRB9 (Current)7/1/2015
G-41 Reliability
Nickel Wire and Ribbon 99NiAMS5555G (Current)4/1/2024
This specification covers a nickel in the form of round wire and rectangular ribbon.
AMS F Corrosion and Heat Resistant Alloys Committee
Center Hole, MetricMA1759B (Current)2/18/2019
This SAE Metric Aerospace Standard (MA) specifies the drawing requirements for center holes when center holes are required on the finished part.
E-25 General Standards for Aerospace and Propulsion Systems
External Hydraulic Leakage for In-Service ComponentsARP1084B (Current)12/16/2022
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 °F (38 °C) temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual.
A-6A1 Commercial Aircraft Committee
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