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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
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
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
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
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
AS8494-8504 B.S.1 Chain (8mm Pitch) and 8 UNC. Fittings Assembly CodeAS8494-3 (Current)1/13/1969
No scope available.
Engine and Airframe Technical Standards Committee (TSC)
Columbium (Niobium) Alloy Sheet, Strip, and Plate, 10Hf - 1.0TiAMS7852D (Current)5/19/2026
This specification covers a columbium (niobium) alloy in the form of sheet, strip, and plate.
AMS G Titanium and Refractory Metals 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
Columbium (Niobium) Alloy Bars, Rods, and Extrusions 10Hf - 1.0Ti, Recrystallization AnnealedAMS7857D (Current)5/20/2026
This specification covers a columbium (niobium) alloy in the form of bars, rods, and extrusions.
AMS G Titanium and Refractory Metals Committee
Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile StrengthAMS6317L (Current)8/9/2022
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings 1.00 inches (25.4 mm) and under in nominal cross section or diameter and for hexagonal shapes, least distance between parallel sides.
AMS E Carbon and Low Alloy Steels Committee
CIRCUIT BREAKER - AIRCRAFT, TRIP-FREE, PUSH-PULL, 50 THRU 100 AMP, TYPE IAS25361B (Current)7/7/2014
AE-7P Protective and Control Devices
Cleaner for Aircraft Exterior Surfaces Wipe-On, Wipe-Off, Containing Suspended Abrasive SolidsAMS1531D (Current)4/29/2020
This specification covers a water-soluble cleaner containing suspended abrasive solids in the form of a ready-to-use liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Aircraft Tire-to-Wheel Performance CharacteristicsARP5507A (Current)5/9/2024
This SAE Aerospace Recommended Practice (ARP) defines the performance criteria and validation for tire circumferential movement on the rim, in the laboratory, by a static test, as well as a performance assessment in service. This document is applicable to braked wheel positions using both bias ply and radial aircraft tires.
A-5C Aircraft Tires Committee
WIRE, ELECTRICAL, POLYTETRAFLUOROETHYLENE/POLYIMIDE INSULATED, NORMAL WEIGHT, SILVER COATED, HIGH STRENGTH OR ULTRA HIGH STRENGTH COPPER, ALLOY, 200 °C, 600 VOLTS ROHSAS22759/89E (Current)3/10/2022
AE-8D Wire and Cable Committee
Steel Bars, Forgings, Mechanical Tubing, and Forging Stock, Aircraft Quality, 0.88Cr - 1.8Ni - 0.42Mo - 0.08V (0.28 - 0.33C) (4330 Mod)AMS6427P (Current)10/20/2023
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy Forgings and Rolled Rings 4.4Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T6) Solution and Precipitation Heat TreatedAMS4133F (Current)6/9/2022
This specification covers an aluminum alloy in the form of die forgings up to 4 inches in nominal thickness, hand forgings up to 8 inches in nominal thickness, rolled rings up to 3 inches in nominal thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Castings, Centrifugal, 7.0Si - 0.30Mg (356.0-T6), Solution and Precipitation Heat TreatedAMS4285G (Current)8/1/2025
This specification covers an aluminum alloy in the form of centrifugal castings (see 8.6).
AMS D Nonferrous Alloys Committee
Recommended Part Numbering Guidelines for Fluid System Components Inch System of MeasurementsARP1590A (Current)10/6/2014
This SAE Aerospace Recommended Practice (ARP) presents a recommended part numbering scheme for fluid system component parts, which may require complex standard numbers. Standardizing on certain numbering systems provides for numbering simplicity, ease of interchangeability and supersession (when required), standardization and limitation of usable codes. This ARP is similar to ISO/TC20/SC10 and its usage is recommended for commonality in international standard part numbering practices.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Crew Station Lighting - Commercial AircraftARP1161B (Current)10/18/2019
This SAE Aerospace Recommended Practice covers the recommended requirements for the lighting and characteristics of instruments; information plates and displays, emergency, cautionary, advisory and status displays; circuit breaker and toggle switch positions; and the recommended requirements for the utility lighting system.
A-20A Crew Station Lighting
Safe Carriage of Impaired and Disabled PassengersAIR1815A (Current)4/4/2013
This AIR defines the major groups of impairments and disabilities among passengers who use aircraft as a transportation mode, and the types of safety problems which might be associated with each impairment. These impairments, and their safety-related problems, should be considered when referring to ARP's related to the design of cabin furnishings and equipment.
S-9B Cabin Interiors and Furnishings Committee
Procedure for the Calculation of Airplane Noise in the Vicinity of AirportsAIR1845A (Current)8/16/2012
A-21 Aircraft Noise Measurement Aviation Emission Modeling
Aluminum Alloy Die Forgings 4.0Cu - 2.0Ni - 0.68Mg (2018-T61) Solution and Precipitation Heat TreatedAMS4140K (Current)12/11/2014
This specification covers an aluminum alloy in the form of die forgings and forging stock.
AMS D Nonferrous Alloys Committee
STANDARDIZATION OF DRIVE END OF HYDRAULIC OR GEARED TORQUE WRENCHES FOR USE TO AN UPPER LIMIT OF 500,000 INCH POUNDSARP911 (Current)12/16/2002
This recommended practice covers the dimensions of an inside splined driver-wrench adapter, envelope of the housing-wrench reaction, the mechanical method of adapting the driver-wrench adapter to the wrench adapter driven end, and the housing-wrench reaction to the holder-counter torque.
EG-1B Hand Tools Committee
400-Cycle Generator Characteristics for Civil Aircraft Ground Support ApplicationsARP717 (Current)12/16/2002
AGE-3 Aircraft Ground Support Equipment Committee
Aerospace-Interface Definition for Mechanical Actuation SubsystemsARP5311 (Current)1/1/2022
This SAE Aerospace Recommended Practice (ARP) defines all the relevant issues that affect the generation of an Interface Control Document for Mechanical Actuation Sub-Systems. It is intended to provide to all parties involved with the generation of Mechanical Actuation Sub-Systems, a definition of documentation, drawings, reports and design parameters required to assure a successful development of mechanical actuation sub-systems for Aerospace-Military and Commercial applications.
A-6B3 Electro-Mechanical Actuation Committee
I - SECTION - EXTRUDEDAMS10140B (Current)3/20/2012
AMS D Nonferrous Alloys Committee
Cleaner for Aircraft Exterior Surfaces Emulsion, Pressure-Spray TypeAMS1528D (Current)4/29/2020
This specification covers an emulsion-type, low-foaming cleaner in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Coating, Urethane, Aliphatic Isocyanate Polytetrafluoroethylene FilledAMS3140B (Current)7/22/2013
This specification covers a two-component, polytetrafluoroethylene-filled polyurethane coating material supplied in kit form.
AMS G8 Aerospace Organic Coatings Committee
Motorcycle Stop Lamp SwitchJ1167_202109 (Current)9/1/2021
This SAE Standard defines the test conditions, procedures, and performance specifications for 6 V and 12 V stop lamp switches intended for use on motorcycles.
Motorcycle Technical Steering Committee
Compound, Corrosion, Preventive, Hard Film, Cold ApplicationAMS3076C (Current)12/1/2000
Primarily for preservation, during extended periods of shipment and/or storage, of miscellaneous metal parts, tools, subassemblies, and equipment where the compound is readily accessible for removal and removal does not damage the parts.
AMS B Finishes Processes and Fluids Committee
Identification, Titanium and Titanium Alloy Wrought ProductsAMS2809B (Current)5/24/2024
This specification covers procedures for identifying wrought products of titanium and titanium alloys.
AMS G Titanium and Refractory Metals Committee
Silicone Resin, Elastomeric, Opaque, Room Temperature CureAMS3371A (Current)6/16/2009
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED". Cancelled specifications are available from SAE.
AMS G9 Aerospace Sealing Committee
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR MIL-DTL-26482 SERIES 1, MIL-DTL-26500 AND MIL-DTL-26518 CONNECTORS)AS39029/31D (Current)1/28/2022
AE-8C1 Connectors Committee
Yarn, Organic Fiber (Para-Aramid), Intermediate Modulus, 1000 Denier, 1.5% Finish for WeavingAMS3904/4B (Current)3/1/1999
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
FITTING, ADAPTER, REDUCER/EXPANDER, FLARED TO BOSSAS934C (Current)1/9/2013
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Organic Fiber (Para-Aramid), Yarn and Roving Intermediate Modulus For Cables, Cordage, and Woven GoodsAMS3904C (Current)8/1/2016
This specification and its supplementary detail specifications cover intermediate modulus para-aramid organic fibers in the form of continuous, multifilament yarn and roving.
AMS P17 Polymer Matrix Composites Committee
Aluminum Alloy, Sheet and Plate, 1.25Mn - 0.12Cu (3003-O), AnnealedAMS4006K (Current)9/13/2007
This specification covers an aluminum alloy in the form of sheet and plate.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate, Alclad 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075; -T6 Sheet - T651 Plate) Solution and Precipitation Heat TreatedAMS4049N (Current)8/5/2022
This specification covers an aluminum alloy in the form of sheet and plate with thickness from 0.008 to 4.000 inches (0.20 to 101.6 mm), inclusive, clad on two sides (see 8.6).
AMS D Nonferrous Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings, and Forging Stock, 17Cr - 0.50Mo (0.95 - 1.20C) (440F), Free-Machining, AnnealedAMS5632K (Current)5/22/2023
This specification covers two types of corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Castings, Investment 0.80Cr - 1.8Ni - 0.35Mo (0.28 - 0.36C) (SAE 4330 Modified) AnnealedAMS5328E (Current)8/4/2017
This specification covers a low-alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
Iron-Nickel Alloy, Strip 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al Solution Heat Treated, Cold Rolled, 50% ReductionAMS5225G (Current)6/1/2021
This specification covers an iron-nickel alloy in the form of strip.
AMS F Corrosion and Heat Resistant Alloys Committee
Iron-Nickel Alloy Strip 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al Solution Heat TreatedAMS5221G (Current)8/7/2025
This specification covers an iron-nickel alloy in the form of strip 0.020 to 0.250 inch (0.51 to 6.35 mm), inclusive, in thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings and Stock for Forgings and Rings, 25Cr - 20Ni - 2.0Si (314), Solution Heat TreatedAMS5652K (Current)9/25/2025
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
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