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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
Compound, Corrosion Preventive Aircraft EngineAMS3072E (Current)4/5/2007
This specification covers a blend of corrosion-preventive compound concentrate and petroleum-base aircraft-engine lubricating oil in the form of a ready-to-use liquid.
AMS B Finishes Processes and Fluids Committee
Pressure Testing, 55 PsiAMS2605E (Current)2/10/2004
This specification provides requirements and procedures for air-pressure leak testing of parts.
AMS B Finishes Processes and Fluids Committee
Radiographic InspectionAMS2635D (Current)5/1/1999
This specification covers the procedures for radiographic inspection.
AMS K Non Destructive Methods and Processes Committee
Coating, Vapor Deposited Poly-Monochloro-Para-Xylylene for MicrocircuitsAMS2535B (Current)10/22/2015
This specification covers requirements for poly-monochloro-para-xylylene coatings.
AMS B Finishes Processes and Fluids Committee
Surface Texture, Roughness (Ra), Peak Count(Pc), and Mean Profile Spacing, (Rsm) Measurement of Metallic Coated and Uncoated Steel Sheet/Strip to be Formed and/or to be PaintedJ911_201704 (Current)4/3/2017
This SAE Recommended Practice describes a method for measuring Roughness Average (Ra) and Peak Count (PC) and other variables of the surface of metallic coated and uncoated steel sheet/strip.
Metals Technical Committee
Black Finishing Low Baking EnamelAMS2503G (Current)2/7/2017
This specification covers the engineering requirements for finishing aircraft parts and assemblies with a black enamel.
AMS B Finishes Processes and Fluids Committee
Gas Nitriding of Steel PartsAMS2756B (Current)6/3/2008
This specification covers a process for surface-hardening parts, made from appropriate low-alloy steels (See 8.4), by the introduction of nitrogen from ammonia.
AMS B Finishes Processes and Fluids Committee
Steel Sheet, Strip, and Plate, Low Alloy, Heat-Resistant 0.65Si - 1.25Cr - 0.50Mo - 0.25V (0.27 - 0.33C) [17-22A(S)] Aircraft QualityAMS6385N (Current)7/10/2025
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
Aircraft HumidificationAIR1609B (Current)1/14/2021
This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications.
AC-9 Aircraft Environmental Systems Committee
Boss, Straight Thread Gasket Seal, Standard Dimensions ForAS757 (Current)12/16/2002
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Nut, Sleeve Coupling, Flareless Tube, With Lockwire HolesAS1041 (Current)12/16/2002
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Steel Tubing, Welded, 0.50ni 0.55cr 0.20mo (0.28 0.33c) (SAE 8630)AMS6550J (Current)7/1/2001
Primarily for general use is light wall-thickness sections where minimum tensile strength up to 160,000 psi (1105 MPa) is required and parts may be welded during fabrication. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of April 19, 1988. It is recommended, therefore, that this specification not be specified for new designs.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings, and Tubing 1.2Cr - 2.0Ni - 0.45Mo (0.27 - 0.33C)AMS6407L (Current)10/22/2021
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
Rings, Flash Welded Carbon and Low-Alloy SteelsAMS7496K (Current)6/3/2022
This specification covers flash welded rings fabricated from carbon and low-alloy steels.
AMS E Carbon and Low Alloy Steels Committee
Alloy Sheet and Strip, Sintered Wire Mesh, Corrosion and Heat Resistant 30Fe - 1.5Mn - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0(Cb +Ta) - 0.15N PorousAMS7724D (Current)4/6/2017
This specification covers a corrosion and heat resistant iron alloy sintered wire mesh in the form of sheet and strip.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings, and Stock for Forgings or Rings 15Cr - 6.5Ni - 0.75Mo - 0.30Cb (Nb) - 1.5Cu Consumable Electrode Remelted, Solution Heat Treated, Precipitation HardenableAMS5773G (Current)9/7/2023
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, and flash welded rings in the solution heat-treated condition, 12 inches (305 mm) and under in nominal diameter, thickness or, for hexagons, least distance between parallel sides (thickness), and stock of any size for forging or flash welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
BOLTS AND SCREWS, CORROSION AND HEAT RESISTANT NICKEL ALLOY Upset Headed, Heat Treated, Roll Threaded 1950°F (1066°C) Solution Heat TreatedAMS7471F (Current)5/1/1995
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Bars, Forgings, and Tubing 1.45Cr (0.93 - 1.05C) (SAE 52100) Premium Aircraft-Quality, Consumable Electrode Vacuum RemeltedAMS6444P (Current)5/4/2021
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Cord, Aromatic Polyamide, Nonmelting 375 Pounds (1670 N), 230 Foot/Pound (155 M/Kg)AMS3853/2B (Current)10/1/1995
No scope available.
AMS P Polymeric Materials Committee
Webbing, Nylon, Aircraft Arresting 105,000 Pounds (467 kN)AMS3796/1B (Current)6/14/2016
This specification covers one type of nylon in the form of webbing.
AMS P Polymeric Materials Committee
Tow or Yarn, Carbon Fibers For Structural Composites GF (0X) 400 (2758) Tensile Strength, 40 (276) Tensile ModulusAMS3892/8B (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
Light Source Retention SystemJ567_201502 (Current)2/1/2015
This SAE Standard references the performance and functional requirements of the International Electrotechnical Commission (IEC) and its U.S. member, the American National Standards Institute (ANSI). By referring to IEC/ANSI and its standards concerning light source (bulb) sockets, light source (lamp) holders, and gages, this document recognizes the need for harmonized standards world-wide for what are typically commodity items. Additional requirements are noted.
Lighting Standard Practices Committee
Motorcycle and Motor Driven Cycle Electrical System Maintenance of Design VoltageJ392_202005 (Current)5/25/2020
This SAE Recommended Practice pertains to electrical systems of motorcycles both with and without batteries.
Motorcycle Technical Steering Committee
Steel Bars, Forgings, Rings and Stock for Forging and Flash-Welded Rings 0.95Cr - 0.20Mo (0.28 - 0.33C), (SAE 4130) Aircraft QualityAMS6370S (Current)5/3/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash-welded rings, and stock for forging or flash-welded rings.
AMS E Carbon and Low Alloy Steels Committee
Potting Compound, Epoxy, Unfilled General Purpose Room Temperature CureAMS3734B (Current)6/1/1996
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June, 1996, and has been supersed by AMS 3731 and /10.
AMS P Polymeric Materials Committee
POTTING COMPOUND, EPOXY, FILLED 15 – 20 GTE, 225 HDT Free MachiningAMS3740 (Current)12/1/1994
AMS P Polymeric Materials Committee
Tape, Nylon, Nonmelting, Reinforcing 2 (50) Wide, 1500 (6670 N) Breaking StrengthAMS3777/7B (Current)10/1/1995
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
AMS P Polymeric Materials Committee
Steel, Spring Wire 0.95Cr - 0.22V (0.48 - 0.53C) (SAE 6150) Annealed and Cold DrawnAMS6450L (Current)11/2/2022
This specification covers a low-alloy steel in the form of wire supplied as coils, spools, and straight lengths.
AMS E Carbon and Low Alloy Steels Committee
Steel, Welding Wire, 0.50Cr - 0.55Ni - 0.20Mo (0.33 0.38C) (SAE 8735) Vacuum Melted, Environment Controlled PackagingAMS6331B (Current)5/15/2003
This specification covers a low-alloy steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
Adhesion Promoter for Polysulfide Sealing Compounds Nonrestricted SolventAMS3100/2B (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 AMS3100B. The requirements of the latest issue of AMS3100B shall be fulfilled whenever reference is made to the cancelled AMS3100/2A. 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 AMS3100B.
AMS G9 Aerospace Sealing Committee
Interleaf Carrier Material, Composite Tape Differentially Coated Paper, Unperforated 0.0042 inch (0.107 mm)AMS3898/7A (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
Bolts and Screws, Steel, UNS S66286 1650 °F Solution Heat Treated Precipitation Heat Treated Before Roll ThreadedAS7479E (Current)8/27/2021
This specification covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, and of 130000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
E-25 General Standards for Aerospace and Propulsion Systems
Washer, Thermal Compensating, Metric SeriesAIR1754B (Current)2/18/2019
The purpose of this document is to define: - compensation washer application requirements - recommended materials - washer thickness determination - dimensioning
E-25 General Standards for Aerospace and Propulsion Systems
HOSE ASSEMBLY, 3000 PSI, PTFE, FLARED, STRAIGHT TO 45°, HEAVYWEIGHTAS628D (Current)11/27/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, 3000 PSI, PTFE, FLARED, 90° TO 90°, HEAVYWEIGHTAS632D (Current)11/27/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Emergency Vehicle SirensJ1849_202002 (Current)2/1/2020
This SAE Recommended Practice provides laboratory test procedures, requirements, and guidelines for electronic siren systems with a single loudspeaker, and electromechanical sirens for use on authorized emergency vehicles, which call for the right-of-way. Test procedures and performance requirements for individual system components are not included in this version. Results obtained for a siren system with a speaker array that is greater than 0.5 m in any dimension shall apply to the system only when the array is in the same spatial configuration as tested (i.e., the same speaker separation and orientation).
Emergency Warning Lights and Devices Standards Committee
IGNITION CABLE, HIGH TENSION Copper ConductorAMS3392 (Current)12/16/2002
AMS P Polymeric Materials Committee
GASKET, OIL RESISTINGAMS3230 (Current)12/16/2002
AMS CE Elastomers Committee
Adhesion Promoter for Polysulfide Sealing Compounds Nonhalogenated SolventAMS3100/1B (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 AMS3100B. The requirements of the latest issue of AMS3100B shall be fulfilled whenever reference is made to the cancelled AMS3100/1A. 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 AMS3100B.
AMS G9 Aerospace Sealing Committee
SEALING COMPOUND, LOW ADHESION, CORROSION INHIBITING 9,000 to 14,000 Poises (900 to 1400 Pas 1/2 Hour Application Time (B-1/2)AMS3267/2A (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
Webbing, Woven Nylon For Decelerators 1-23/32 (43) Wide, 8700 (38,700) Breaking StrengthAMS3718/4B (Current)6/14/2016
This specification covers one width and one strength of nylon webbing.
AMS P Polymeric Materials Committee
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