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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
Webbing, Woven Nylon Fabric 6000 Pounds (26,700 N), 1.8 Ounces/Yards (56 g/m)AMS3795/1B (Current)6/13/2016
This specification covers one strength and weight of nylon fabric in the form of webbing.
AMS P Polymeric Materials Committee
Glass Cloth, Chloroprene (Cr) CoatedAMS3783B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Tape and Webbing, Textile, Para-Aramid Intermediate Modulus 1-1/4 Inches (31 mm), 0.23 Ounces per Yard (7.1 g/m)AMS3793/6B (Current)9/11/2013
This specification covers one class of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
Tape and Webbing, Textile. Para-Aramid Intermediate Modulus ¾ Inch (19 mm), 0.11 to 0.60 Ounces per Yard (3.4 to 18.6 g/m)AMS3793/3D (Current)7/31/2018
This specification covers three classes of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
Nickel Alloy, Brazing Filler Metal, 92Ni 4.5Si 3.1B, 980 to 1040°C Solidus-Liquidus RangeMAM4778D (Current)3/12/2003
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder and procured in metric units. AMS 4778 is the inch/pound version of this MAM. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. Also may be used as a corrosion and oxidation resistant hard coating.
AMS F Corrosion and Heat Resistant Alloys Committee
FITTING END, 24° CONE, DESIGN STANDARD, METRICMA2095C (Current)4/27/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Sealing Compound, Polysulfide (T) Rubber, Fuel Resistant, Non-Chromated Corrosion Inhibiting for Intermittent Use to 360 °F (182 °C)AMS3265F (Current)9/9/2020
This specification covers polysulfide rubber sealing compounds containing only non-chromated corrosion inhibitors, supplied as a two-component system which cures at room temperature.
AMS G9 Aerospace Sealing Committee
Aluminum Alloy, Bars, Rods, and Wire, Rolled Or Cold-Finished 99.0a1, as FabricatedAMS4102G (Current)11/15/2001
This specification covers an aluminum alloy in the form of bars, rods, and wire. Primarily for parts requiring good formability and weldability in fabrications where strength is unimportant.
AMS D Nonferrous Alloys Committee
Elastomeric Tubing, Electrical Insulation Crosslinked Silicone, Pigmented, Flexible, Heat-Shrinkable 1.750 to 1 Shrink RatioAMS3625D (Current)2/23/2016
This specification covers an irradiated, thermally-stabilized, flame-resistant, modified silicone rubber in the form of heat shrinkable tubing.
AE-8D Wire and Cable Committee
Magnesium Alloy Castings, Sand, 8.7Al - 0.70Zn (AZ91C-T6), Solution Heat Treated and AgedAMS4437G (Current)6/17/2025
This specification covers a magnesium alloy in the form of sand castings (see 8.6).
AMS D Nonferrous Alloys Committee
Quality Assurance Sampling of Bolts and ScrewsAMS2373B (Current)7/1/1998
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of May, 1990.
AMS B Finishes Processes and Fluids 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
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 CAS4TINGS, SAND 4.5Cu (195-T4) Solution TreatedAMS4230C (Current)5/1/1995
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
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
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
Aluminum Alloy Bars, Rods, and Wire, Rolled, Drawn, or Cold Finished 4.5Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T6, -T651) Solution and Precipitation Heat TreatedAMS4121K (Current)11/22/2023
This specification covers an aluminum alloy in the form of bars, rods, and wire.
AMS D Nonferrous Alloys 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
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
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, 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
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 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
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, 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
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
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 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
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
Flame Resistant Properties for Aircraft MaterialsAMS3852A (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
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
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