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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.
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
SCOPE IS UNAVAILABLE.
E-25 General Standards for Aerospace and Propulsion Systems
WASHER, KEY - 90°, LOCKING, CRES, UNS S32100AS9581D (Current)6/3/2026
SCOPE IS UNAVAILABLE.
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
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
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
Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted, AnnealedAMS5544L (Current)7/14/2020
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Wire, Steel 0.18 - 0.23C (SAE 1020) AnnealedAMS5032J (Current)9/18/2024
This specification covers a low-carbon steel in the form of wire up to 0.249 inch (6.32 mm), inclusive, supplied as coils of wire or, when specified, as straight lengths.
AMS E Carbon and Low Alloy Steels Committee
Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification forAS85720C (Current)9/30/2022
This specification covers the design requirements and test procedures for separable beam seal fittings which include end fittings (see 2.4.2), connectors (see 2.4.3), and boss fittings for use in aerospace fluid systems. Design requirements are for Class 5000 and 8000 in titanium, and corrosion resistant steel (CRES). Definition of fittings and related terms are defined in 2.4.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Titanium Alloy Sheet 6Al - 4V Driver SheetAMS4932E (Current)8/23/2024
This specification covers a titanium alloy in the form of sheet.
AMS G Titanium and Refractory Metals Committee
Bearings, Leaded Copper 70Cu – 28.5Pb Steel BackAMS4820F (Current)4/19/2018
This specification covers bearings of leaded copper cast on one or both faces of a steel backing.
AMS D Nonferrous Alloys Committee
Brass Forgings, Free Cutting 60Cu - 2.0Pb - 37.5Zn As Forged (M10)AMS4614J (Current)9/30/2022
This specification covers one type of brass in the form of forgings and forging stock.
AMS D Nonferrous Alloys Committee
Adhesive, Electrically Nonconductive, Moderately Rapid CureAMS3703B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P17 Polymer Matrix Composites Committee
Webbing, Woven Nylon For Decelerators 3/4 (19) Wide, 3000 (13,350) Breaking StrengthAMS3718/1B (Current)6/14/2016
This specification covers one width and one strength of nylon webbing.
AMS P Polymeric Materials Committee
Titanium Alloy Sheet, Strip, and Plate 6Al - 2Sn - 4Zr - 2Mo - 0.08Si Duplex AnnealedAMS4919K (Current)4/1/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate 0.025 to 3.000 inches (0.64 to 76.20 mm), inclusive, in nominal thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
Coating Material, Fluorocarbon (FKM) Elastomeric, Anti-Static Topcoating, Color MatchedAMS3138/6C (Current)4/14/2009
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. 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 AMS3138D. Cancelled specifications are available from SAE.
AMS G8 Aerospace Organic Coatings Committee
SEALING COMPOUND, LOW ADHESION, CORROSION INHIBITING 9,000 to 14,000 Poises (900 to 1400 Pa·s), 2 Hour Application Time (B-2)AMS3267/4A (Current)4/1/1992
This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system.
AMS G9 Aerospace Sealing Committee
Tape, Nylon, Nonmelting, Reinforcing 1 (25) Wide, 525 (2335 N) Breaking StrengthAMS3777/5B (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, Nylon, Nonmelting, Reinforcing 3/4 (19) Wide, 400 (1780 N) Breaking StrengthAMS3777/1B (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, Nylon, Nonmelting, Reinforcing 1 (25) Wide, 1000 (4450 N) Breaking StrengthAMS3777/3B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Webbing, Woven Nylon For Decelerators 1 (25) Wide, 4000 (17,800) Breaking StrengthAMS3718/2B (Current)6/14/2016
This specification covers one width and one strength of nylon webbing.
AMS P Polymeric Materials Committee
Coating, Abrasion Resistant for Polycarbonate PartsAMS3510B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Coating Material, Fluorocarbon (FKM) Elastomeric, Anti-Static Topcoating, WhiteAMS3138/5C (Current)4/14/2009
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. 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 AMS3138D. Cancelled specifications are available from SAE.
AMS G8 Aerospace Organic Coatings Committee
Asbestos and Synthetic Rubber Sheet, Hot Oil ResistantAMS3232N (Current)9/2/2009
AMS CE Elastomers Committee
Cloth, Upholstery, Flame Resistant Novoloid/Aramid, Waffle Type WeaveAMS3856/1B (Current)6/24/2016
This specification covers one weight and one weave of novoloid/aramid cloth.
AMS P Polymeric Materials Committee
Tape, Nylon, Nonmelting, Reinforcing 1-1/2 (38) Wide, 1500 (6670 N) Breaking StrengthAMS3777/4B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Tow or Yarn, Carbon Fibers For Structural Composites GF (0X) 400 (2758) Tensile Strength, 33 (228) Tensile ModulusAMS3892/7B (Current)12/15/2016
This specification covers one type of continuous multifilament carbon fibers in the form of a tow or yarn (when twisted). The weight per unit length of the tow or yarn is governed by the filament count which is identified by the supplier's grade or material designation.
AMS P17 Polymer Matrix Composites Committee
Interleaf Carrier Material, Composite Tape Differentially Coated Paper, Unperforated 0.0035 inch (0.081 mm)AMS3898/6A (Current)4/13/2022
This specification covers a paper, coated on both sides and with different release characteristics on each side (i.e., differentially coated), supplied in the form of rolls of sheeting or reels of unperforated tape of the width specified.
AMS P17 Polymer Matrix Composites Committee
Interleaf Carrier Material, Composite Tape/Broadgoods Kraft, Differentially Coated Paper, Unperforated 0.0050 inch ± 0.0005 (0.127 mm ± 0.013)AMS3898/9A (Current)4/13/2022
This specification covers a kraft paper, coated on both sides and with different release characteristics on each side (i.e., differentially coated), supplied in the form of rolls of sheeting or reels of unperforated tape of the width specified.
AMS P17 Polymer Matrix Composites Committee
Tape, Nylon, Nonmelting, ReinforcingAMS3777B (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 1/2 Inch (12.5 mm), 0.06 to 0.56 Ounces per Yard (1.9 to 17.4 g/m)AMS3793/1B (Current)9/11/2013
This specification covers four classes 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 1-1/2 Inches (37.5 mm), 0.12 to 0.47 Ounces per Yard (3.7 to 14.6 g/m)AMS3793/7B (Current)9/11/2013
This specification covers three classes of para-aramid tape and webbing of a single width and with varying weights.
AMS P Polymeric Materials Committee
Diglycidyl Ester ResinAMS3296B (Current)7/1/1993
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Potting Compound, Epoxy, Filled 25 - 30 Cte, 175 Hdt Room Temperature CureAMS3736B (Current)6/1/1996
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996, and has been supersed by AMS 3731 & /7.
AMS P Polymeric Materials Committee
Tape, Nylon, Nonmelting, Reinforcing 5/16 (8) Wide, 350 (1555 N) Breaking StrengthAMS3777/6B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Epoxy Resin, Polyfunctional SolidAMS3706B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P17 Polymer Matrix Composites Committee
Tape, Nylon, Nonmelting, Reinforcing 9/16 (14) Wide, 500 (2225 N) Breaking StrengthAMS3777/2B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Core, Polyurethane Foam (Polyether) 2.0 Pounds Per Cubic Foot (32 kg/m3) DensityAMS3725/1B (Current)11/10/2016
This specification covers a rigid cellular polyurethane or polyisocyanurate (polyether only) foam in the form of board or block.
AMS P17 Polymer Matrix Composites Committee
Potting Compound, Epoxy, Unfilled 35 - 40 Cte, 160 Hdt Room Temperature CureAMS3737B (Current)6/1/1996
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 1996, and has been superseded by AMS 3731 & /1.
AMS P Polymeric Materials Committee
Cloth, Nylon, Metallized, Water Repellent TreatedAMS3848/2B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Webbing, Woven Nylon Fabric 12,000 Pounds (53,400 N), 3.3 Ounces/Yards (102.5 g/m)AMS3795/3B (Current)6/13/2016
This specification covers one strength and weight of nylon fabric in the form of webbing.
AMS P Polymeric Materials Committee
Silicon Bronze Bars, Rods, Forgings, and Tubing 92Cu - 3.2Si - 2.8Zn - 1.5Fe Stress RelievedAMS4616H (Current)2/1/2024
This specification covers one type of bronze in the form of bars, rods, forgings, tubing, and forging stock (see 8.5).
AMS D Nonferrous Alloys Committee
Steel, Welding Wire 0.95Cr - 0.20Mo (0.38 - 0.43C) Vacuum Melted, Environment Controlled PackagingAMS6452E (Current)12/7/2017
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Steel, Welded Tubing, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft QualityAMS6373K (Current)5/27/2025
This specification covers an aircraft-quality, low-alloy steel in the form of welded tubing.
AMS E Carbon and Low Alloy Steels Committee
Castings, Alloy-Investment, 61ni 16cr 8.5co 1.8mo 2.6w 0.8cb 3.4ti 1.8ta 3.4al 0.010b 0.06zr (0.03-0.08c), Vacuum Melted, Vacuum Cast, as CastAMS5409A (Current)8/21/2002
This specification covers a corrosion and heat resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, and Stock for Forgings, 18Cr - 13Ni - 2.1Mo (316FM) Free Machining Solution Heat TreatedAMS5649J (Current)3/1/2024
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
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