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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
Numerical Modeling Techniques for Jet Engine Test Cell AerodynamicsAIR6355 (Current)6/5/2026
This SAE Aerospace Information Report (AIR) has been written for individuals associated with ground level testing of turbofan and turbojet engines, and particularly for those who might be interested in investigating steady-state performance characteristics of a new test cell design or of proposed modifications to an existing test cell by means of numerical modeling and simulation. It is not the intent of this standard to provide specific test cell design recommendations, which are covered in the reference documentation.
EG-1E Gas Turbine Test Facilities and Equipment
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
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
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
Contrast Dye Penetrant InspectionAMS2646D (Current)4/1/1999
Detection of discontinuities such as cracks, laps, porosity, cold shuts, lack of bond, and similar defects. Because inspection can be performed in normal light, this method can be used when fluorescent penetrant inspection is impracticable.
AMS K Non Destructive Methods and Processes Committee
Aluminum Alloy Forgings 7.7Zn - 2.5Mg - 1.5Cu - 0.16Cr (7049-T73) Solution and Precipitation Heat TreatedAMS4111F (Current)5/17/2023
This specification covers an aluminum alloy in the form of die forgings or hand forgings up to 5 inches (125 mm) in thickness, and forging stock of any size (see 8.7).
AMS D Nonferrous Alloys Committee
Flame Resistant Properties for Aircraft MaterialsAMS3852A (Current)1/1/1987
AMS CE Elastomers Committee
Enamel, Phenolic Black BakingAMS3122G (Current)7/22/2013
This specification covers a semigloss black baking enamel based on a phenolic resin.
AMS G8 Aerospace Organic Coatings Committee
Oil, Fluorescent Penetrant, Solvent-SolubleAMS3155E (Current)12/15/2008
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS2644. The requirements of the latest issue of AMS2644 shall be fulfilled whenever reference is made to the cancelled AMS3155. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS2644.
AMS K Non Destructive Methods and Processes Committee
Identification Carbon and Low-Alloy Steels, Corrosion- and Heat-Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft TubingAMS2807C (Current)5/17/2024
This specification covers procedures for identifying carbon and low-alloy steels, corrosion- and heat-resistant steels and alloys, maraging and other highly alloyed steels, and iron alloy sheet, strip, and plate, and aircraft tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
Fluid, Aircraft CompassAMS3151C (Current)10/6/2009
This specification covers one grade of hydrocarbon compass fluid.
AMS B Finishes Processes and Fluids Committee
Coating Material, Silicone Resin 400 °F (205 °C)AMS3135G (Current)7/22/2013
This specification covers an unpigmented silicone-resin-base coating material.
AMS G8 Aerospace Organic Coatings Committee
Identification, Aluminum and Magnesium Alloy Wrought ProductsAMS2811A (Current)5/1/1998
This specification covers procedures for identifying wrought products of aluminum and magnesium alloys.
AMS D Nonferrous Alloys Committee
Thread Compound, Anti-Seize, Graphite-PetrolatumAMS2518D (Current)2/3/2012
This specification covers an anti-seize compound in the form of a grease.
AMS M Aerospace Greases Committee
Connections, Electrical Solderless, Wire-WrappedAMS2695E (Current)12/5/2013
This specification covers electrical connections made with single, solid, round copper or copper alloy wire wrapped around copper alloy terminals without the use of solder.
AMS B Finishes Processes and Fluids Committee
Aluminum Coating Material, Corrosion and Heat Resistant Thermosetting, Inorganic BinderAMS3126D (Current)7/22/2013
This specification covers a corrosion and heat resistant aluminum coating material supplied as a liquid of suitable consistency for coating parts after being thoroughly mixed.
AMS G8 Aerospace Organic Coatings Committee
PLASTIC SHEET, COPPER FACED, GTN Glass Fabric Reinforced PolytetrafluoroethyleneAMS3598D (Current)5/1/1995
This specification covers polytetrafluoroethylene-impregnated glass laminates in the form of sheet clad on one or both sides with electrolytically deposited copper foil.
AMS P Polymeric Materials Committee
Chloroprene (CR) Rubber Flame Resistant 65 - 75AMS3244H (Current)9/23/2011
This specification covers a chloroprene (CR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
AMS CE Elastomers Committee
Fire Resistant Properties for Aircraft MaterialsAMS3851A (Current)1/1/1987
AMS CE Elastomers Committee
Core, Honeycomb Fibrous, Aramid Base, Phenolic CoatedAMS3711E (Current)7/16/2013
This specification covers expanded honeycomb core made of fibrous aramid paper sheets and supplied in the form of blocks, slices, and ordered shapes.
AMS P17 Polymer Matrix Composites Committee
Conversion Coating of Titanium Alloys Fluoride-Phosphate TypeAMS2486F (Current)1/16/2024
This specification establishes the requirements for a chemical conversion coating on titanium alloys.
AMS B Finishes Processes and Fluids Committee
Enamel, Glyceryl Phthalate Black BakingAMS3120H (Current)1/16/2012
This specification covers a gloss, black baking enamel based on a glyceryl phthalate resin.
AMS G8 Aerospace Organic Coatings Committee
Aluminum Alloy, Welding Wire 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti for Welding A206.0 Type AlloysAMS4244D (Current)8/9/2022
This specification covers an aluminum alloy in the form of two types of welding wire.
AMS D Nonferrous Alloys Committee
ALUMINUM ALLOY CAS4TINGS, SAND 4.5Cu (195-T4) Solution TreatedAMS4230C (Current)5/1/1995
AMS D Nonferrous Alloys Committee
Aluminum Alloy Extrusions 2.7Cu - 2.2Li - 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat TreatedAMS4232E (Current)9/9/2024
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles up to 0.499 inches (12.67 mm) in nominal diameter, or least thickness, and under 10 in2 (65 cm2) in cross-sectional area.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate, 1.6Cu - 2.2Mg - 0.22Cr - 5.7Zn (7475-T7651), Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat TreatedAMS4089G (Current)2/25/2025
This specification covers an aluminum alloy in the form of plate 0.250 to 1.500 inches (6.35 to 38.10 mm), inclusive, in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
Dimer, Dichloro 2, 2 Para-CyclophaneAMS2517B (Current)2/11/2019
This specification covers the properties of a mixed dimer.
AMS B Finishes Processes and Fluids Committee
Plating, Gold, for Thermal ControlAMS2425G (Current)9/23/2025
This specification covers the requirements for gold deposited on metal surfaces and the properties of the deposit.
AMS B Finishes Processes and Fluids Committee
Aluminum Alloy, Drawn Seamless Tubing, 1.2Mn - 0.12Cu (3003-O), AnnealedAMS4065K (Current)7/13/2007
This specification covers an aluminum alloy in the form of drawn seamless tubing.
AMS D Nonferrous Alloys Committee
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, Drawn Seamless Round Tubing, (1100-H14), Strain HardenedAMS4062J (Current)7/13/2007
This specification covers an aluminum alloy in the form of drawn seamless round tubing.
AMS D Nonferrous Alloys Committee
Yarn, Organic Fiber (Para-Aramid) Intermediate Modulus 1500 Denier (1670 Dtex), 0.9% FinishAMS3904/5C (Current)8/1/2016
This specification covers one type of organic (para-aramid) 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
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
Filler Metal, Aluminum Brazing, 12SiAMS4185G (Current)3/12/2026
This specification covers an aluminum alloy in the form of wire, sheet, foil, pig, grains, shot, and chips (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Castings, Permanent Mold, 5.0Si - 1.2Cu - 0.5Mg (355.0-T71), Solution Heat Treated and OveragedAMS4280K (Current)9/23/2025
This specification covers an aluminum alloy in the form of permanent mold castings (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Tubing, Seamless, Drawn, 4.4Cu - 1.5Mg - 0.60Mn (2024-O), AnnealedAMS4087K (Current)2/25/2025
This specification covers an aluminum alloy in the form of seamless drawn tubing having nominal wall thickness of 0.018 to 0.500 inch (0.46 to 12.70 mm), inclusive (see 8.4).
AMS D Nonferrous Alloys Committee
Filler Metal, Aluminum Brazing 10Si - 4.0Cu (4145)AMS4184H (Current)11/10/2023
This specification covers an aluminum alloy in the form of wire, sheet, foil, pig, grains, shot, and chips (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate 4.5 Cu - 1.5 Mg - 0.60 Mn (2024-T36) Width 48 In. and UnderAMS4097 (Current)12/16/2002
AMS D Nonferrous Alloys Committee
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
Aluminum Alloy, Sheet and Plate 3.5mg 0.25crAMS4018C (Current)1/1/1989
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate 4.5cu 1.5mg 0.60mn (2024-T36) Width 30 In. and UnderAMS4103 (Current)12/16/2002
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
Structural Examination of Titanium Alloys Etch-Anodize Inspection ProcedureAMS2642F (Current)11/3/2021
This specification covers a procedure, typically referred to as Blue Etch Anodize, for revealing the macrostructure and microstructure of selected titanium alloys.
AMS B Finishes Processes and Fluids Committee
Yarn, Organic Fiber (Para-Aramid) Intermediate Modulus 400 Denier (440 Dtex), 1.0% FinishAMS3904/2C (Current)8/1/2016
This specification covers one type of organic (para-aramid) 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
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