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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
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
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
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, 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
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
Graphite Fiber Tape and Sheet, Epoxy Resin Impregnated, G 150,000 (1034) Tensile, 15,000,000 (103) Modulus, 350 (177)AMS3894/6B (Current)12/1/1994
This specification covers one type of epoxy-resin-impregnated graphite fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
ADAPTER 10” TO 5” BOLT CIRCLEAS515A (Current)1/1/2001
AE-1 Engine Accessory Installations Committee
Validation Test Plan for AS4074 Linear Token Passing Multiplex Data BusAS4290A (Current)5/3/2012
This test plan defines the test requirements for determining that Bus Interface Units (BIUs) meet the requirements of SAE AS4074, Linear Token Passing Multiplex Data Bus.
AS-1A Avionic Networks Committee
Liquid Salt Bath Ferritic Nitrocarburizing Non-Cyanide BathAMS2753D (Current)7/12/2019
This specification covers the requirements for an epsilon-iron nitride case on ferrous parts produced by immersion in a low-temperature, agitated, fused salt bath.
AMS B Finishes Processes and Fluids Committee
Insulation Sleeving, Electrical, Shrinkable Without Heat, General Specification ForAS85080A (Current)3/7/2012
This specification establishes requirements for chemically expanded, flexible, electrical insulating sleeving that shrinks to a predetermined size upon solvent evaporation.
AE-8D Wire and Cable Committee
SPARK IGNITER OUTLINE FLANGE MOUNTINGAS423A (Current)7/1/1994
E-30 Propulsion Ignition Systems Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS4967 (UNS R56400), 160 KSI, .4375-20 UNJF-3AAS3151B (Current)12/3/2019
E-25 General Standards for Aerospace and Propulsion Systems
HOSE ASSEMBLY, 3000 PSI, PTFE, FLARELESS, STRAIGHT TO 45°, HEAVYWEIGHTAS622D (Current)5/26/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, THREADED, ENVIRONMENT RESISTANT, REMOVABLE CRIMP CONTACTS, NUT, HEXAGON, CONNECTOR MOUNTINGAS29600/7 (Current)To be published on 08/01/2990
AE-8C1 Connectors Committee
NUT, FLARED, LONGAS5206B (Current)8/16/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aluminum Alloy, Extrusions, 0.68Mg - 0.40Si (6063-T6), Solution and Precipitation Heat TreatedAMS4156M (Current)4/22/2026
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to and including 1.000 inch (25.4 mm) in diameter, least thickness, or tube wall thickness (see 8.6).
AMS D Nonferrous Alloys Committee
CONDUIT ASSEMBLY, FLEXIBLE, RADIO FREQUENCY SHIELDINGAS25067B (Current)11/23/2021
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
Connectors, Electrical, Bayonet Coupling, Environment Resisting, Umbilical, Dummy Stowage ReceptacleAS81582/10A (Current)11/22/2011
No scope available.
AE-8C1 Connectors Committee
INSULATION SLEEVING, ELECTRICAL, SHRINKABLE WITHOUT HEAT, POLYURETHANE FLEXIBLEAS85080/3A (Current)3/7/2012
AE-8D Wire and Cable Committee
FITTING, ELBOW, 90°, PIPE, INTERNAL THREADAS4856B (Current)1/31/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, 3000 PSI, PTFE, FLARELESS, STRAIGHT TO STRAIGHT, HEAVYWEIGHTAS621D (Current)5/26/2022
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), . 3750-24, UNJF-3AAS3170B (Current)4/24/2024
E-25 General Standards for Aerospace and Propulsion Systems
manual for theSAE 17.6 CUBIC INCHSPARK PLUG RATING ENGINEincluding maintenance and overhaulAS840 (Current)7/1/1994
E-30 Propulsion Ignition Systems Committee
IGNITER, SPARK, AERONAUTICAL ENGINE (LOW TENSION)AS803 (Current)5/1/1991
This specification establishes the qualification and acceptance limits for aeronautical engine low tension spark igniters.
E-30 Propulsion Ignition Systems Committee
Steel, Corrosion-Resistant, Sheet, Strip, and Plate 19Cr - 9.2Ni (SAE 30304) Solution Heat TreatedAMS5513L (Current)3/1/2022
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
SPARK IGNITER GASKET-FLANGEAS453A (Current)7/1/1994
E-30 Propulsion Ignition Systems Committee
SPARK IGNITER OUTLINE RIGHT ANGLE FLANGE MOUNTINGAS422A (Current)7/1/1994
E-30 Propulsion Ignition Systems Committee
FITTING, TEE, BEAM SEAL, BULKHEAD ON SIDE, 5000 PSIAS5004D (Current)5/20/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
ADAPTER 10” TO 8” BOLT CIRCLEAS516A (Current)1/1/2001
AE-1 Engine Accessory Installations Committee
FITTING, CROSS, PIPE, INTERNAL THREADAS4858B (Current)2/12/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Compound, Rust Inhibiting Aircraft Engine ComponentsAMS3060B (Current)4/29/2020
This specification covers a rust-inhibiting compound in the form of a liquid concentrate or a water soluble powder.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Elastomer: Phenyl Methyl Vinyl Silicone (PVMQ) Low Temperature/Engine Oil Resistant High Strength/High Tear 55 to 65 Type “A” Hardness For Products in Aircraft Piston Engine Oil/Low Temperature EnvironmentsAMS3346H (Current)10/24/2019
This specification covers a phenyl vinyl silicone rubber material that can be used to manufacture product in the form of sheet, strip, tubing, molded shapes, and extrusions. 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
TUBING END DOUBLE FLARE, STANDARD DIMENSIONS FORAS33583 (Current)11/1/2007
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Compound, Corrosion Preventive Soft Film, Thixotropic, Cold ApplicationAMS3077A (Current)4/24/2018
This specification covers a ready-mixed thixotropic compound in the form of a stable film-forming compound suitable for application by brushing or spraying.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Acrylonitrile Butadiene (NBR) Rubber Aromatic Fuel Resistant 75 - 85AMS3213N (Current)4/12/2023
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Hose Assemblies, Metal Medium Pressure, High Temperature, MetricMA2100 (Current)8/1/2007
This specification covers metric medium pressure, high temperature, flexible metal hose assemblies suitable for continuous operation in liquid and pneumatic systems from 55 to 400°C, with short duration excursion to 650°C, and primarily for use on jet aircraft power plants.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, ELBOW, 90°, BEAM SEAL, 5000 PSIAS5002D (Current)5/20/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING ASSEMBLY, TEE, BEAM SEAL, RETAINED NUT ON RUNAS4809D (Current)4/28/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Towed Vehicle Drivetrain Test Procedure Passenger Cars, Vans, and Light-Duty TrucksJ1144_201910 (Current)10/28/2019
This SAE Recommended Practice provides a means for evaluating the drivetrain of the passenger car, van, or light-duty truck being towed under a variety of road conditions. The towing equipment used is explained in SAE J1142. NOTE—For the purpose of this document, the drivetrain refers to the combination of a specific transmission (make, model, size, type), a specific differential assembly (make, model, size, type), and a specific driveline, if required.
Motor Vehicle Council
FITTING ASSEMBLY, ELBOW, 90°, BEAM SEAL, RETAINED NUTAS4807D (Current)4/28/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, SLEEVE, FLAREDAS5176D (Current)4/2/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, ADAPTER, PORT, REDUCERAS5172F (Current)6/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING END, SPHERICAL, 37° FLARED TUBE CONNECTION DESIGN STANDARDAS5309A (Current)4/22/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Webbing, Woven, Nylon 2600 Pounds Force (11,565 N)AMS3778/4B (Current)2/9/2012
This specification covers one type of nylon webbing.
AMS P Polymeric Materials Committee
Carbon Fiber Tape and Sheet Epoxy Resin Impregnated G 150000 (1034) Tensile, 20000000 (138) Modulus, 175 (347)AMS3894/2C (Current)9/14/2016
This specification covers one type of epoxy-resin-impregnated carbon fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
Cloth, Nylon, Polyurethane Coated Plain Weave, 9.2 ounces/square yard (310 g/m2)AMS3272/3B (Current)8/25/2011
This specification covers a woven nylon cloth coated with polyether (EU)urethane.
AMS P Polymeric Materials Committee
Aluminum Alloy, Plate (7140-T7651) 6.6Zn - 1.8Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved, and OveragedAMS4408B (Current)5/17/2024
This specification covers an aluminum alloy in the form of plate 4.000 to 10.000 inches (101.6 to 254.0 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
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