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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
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
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
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
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)
Vehicle, Magnetic Particle Inspection Petroleum BaseAMS2641D (Current)9/12/2025
This specification covers two types of refined hydrocarbon compounds in the form of liquids. This specification only covers newly manufactured materials.
AMS K Non Destructive Methods and Processes Committee
Personal Watercraft - Display of Capacity InformationJ2566_202308 (Current)7/4/2023
This SAE Recommended Practice establishes uniform requirements and guidelines for the display of capacity information of personal watercraft.
Personal Watercraft Committee
EYE BOLT, A-286 CRES, 1000 °FAS4108/3B (Current)11/18/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
SCREW, MACHINE - HEXAGON HEAD, SLOTTED, FULL SHANK, ALLOY STEEL, UNS K14675, 135 KSI MIN, .1900-32 UNS-3AAS9316C (Current)9/14/2022
E-25 General Standards for Aerospace and Propulsion Systems
Standard Test Procedure and Limit Value for Shutoff Surge Pressure of Pressure Fuel Dispensing SystemsAS1284B (Current)7/17/2015
The test procedure and related limit value are intended to apply to fixed and mobile ground pressure fuel dispensing systems and to aerial refueling tankers.
AE-5C Aviation Ground Fueling Systems Committee
Logistics Product Data HandbookGEIAHB0007B (Current)2/10/2014
LCLS Life Cycle Logistics Supportability
Performance Testing for Aerospace and High Performance Electronic Interconnects Containing Pb-free Solder and FinishesGEIASTD0005_3A (Current)2/12/2018
This document defines: 1 A default method for those companies that require a pre-defined approach and 2 A protocol for those companies that wish to develop their own test methods. The default method (Section 4 of the document) is intended for use by electronic equipment manufacturers, repair facilities, or programs which, for a variety of reasons, may be unable to develop methods specific to their own products and applications. It is to be used when little or no other information is available to define, conduct, and interpret results from reliability, qualification, or other tests for electronic equipment containing Pb-free solder. The default method is intended to be conservative, i.e., it is biased toward minimizing the risk to users of AHP electronic equipment. The protocol (Section 5 of the document) is intended for use by manufacturers or repair facilities which have the necessary resources to design and conduct reliability, qualification, or process development tests that are
G-24 Pb-free Risk Management Committee for ADHP
Aluminum Alloy 2014, Bar, Rod, Shapes, Tube, and Wire, ExtrudedAMSQQA200/2B (Current)2/1/2014
This specification covers the specific requirements for aluminum alloy 2014 bar, rod, shapes, tube, and wire produced by extrusion.
AMS D Nonferrous Alloys Committee
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, Rings and Stock for Rings and Forging 45.5Ni - 25.5Cr - 3.2Mo - 3.2W - 18.5Fe (Alloy 333) Solution Heat TreatedAMS5717K (Current)2/25/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, flash-welded rings, and stock for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings and Forging Stock 18Cr - 11Ni - 0.60Cb(Nb) (347) Solution Heat TreatedAMS5646R (Current)12/13/2021
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
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Forging Stock 72Ni - 15.5Cr - 7.0Fe - 2.5Ti - 1.0Cb (Nb) - 0.70Al (X750) 2100 °F (1149 °C) Solution and Precipitation Heat TreatedAMS5668L (Current)6/10/2024
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, flash-welded rings 10.0 inches (254 mm) and under in nominal diameter or distance between parallel sides, and stock of any size for forging, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
Plastic Sheet and Strip, Modified Vinyl, Foamed Closed CellAMS3635E (Current)1/16/2012
This specification covers a modified vinyl plastic foam in the form of sheet and strip up to 1-1/2 inches (38.1 mm) in nominal thickness.
AMS P Polymeric Materials Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire 20.5Cr - 9.0Ni - 0.50Mo - 1.5W - 1.2Cb - 0.20Ti Vacuum Induction MeltedAMS5782J (Current)4/1/2024
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings and Stock for Forgings and Rings 60.5Ni - 23Cr - 14Fe - 1.4Al (Alloy 601) AnnealedAMS5715H (Current)1/22/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, and flash-welded rings 4.00 inches (101.6 mm) and under in diameter or least nominal cross-sectional dimension and stock of any size for forging or flash-welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant Seamless Tubing, 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750), Solution Heat Treated, Precipitation HardenableAMS5582H (Current)5/9/2024
This specification covers a precipitation hardenable, corrosion- and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD and 0.015 inch (0.38 mm) and over in nominal wall thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion Resistant, Seamless or Welded Tubing 19Cr - 9.5Ni (SAE 30304) Cold Drawn, 1/4 Hard TemperAMS5563D (Current)10/22/2021
This specification covers a corrosion-resistant steel in the form of seamless and drawn or welded and drawn tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Sheet Laminated, Edge BondedAMS5600G (Current)9/10/2024
This specification covers a corrosion-resistant steel in the form of laminated sheet.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.006B - 0.05Zr Consumable Electrode or Vacuum Induction Melted 1825 to 1900 °F Solution Heat TreatedAMS5706N (Current)8/4/2020
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings and Stock for Rings, Forgings, and Heading 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750) 1800 °F (982 °C) Solution Heat-Treated, Precipitation-HardenableAMS5670H (Current)9/28/2023
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, and flash-welded rings under 4.00 inches (101.6 mm) in nominal thickness or diameter, and stock of any size for forging, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
Powder, Plasma Spray 50 (88WC - 12Co) + 35 (70Ni - 16.5Cr - 4Fe - 4Si - 3.8B) + 15 (80Ni - 20Al) Three-Component MixtureAMS5792C (Current)4/1/2024
This specification covers a blend of tungsten carbide-cobalt aggregate, a nickel alloy, and a nickel aluminum aggregate in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 72Ni - 15.5Cr - 1.0Cb(Nb) - 2.4Ti - 0.70Al - 7.0FeAMS5778K (Current)10/18/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) (Alloy 625) Solution Heat TreatedAMS5869E (Current)7/14/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate up to 1.000 inch (25.40 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 29Fe - 22Cr - 21Ni - 18.5Co - 3.2Mo - 2.8W - 0.78Ta - 0.30Al - 0.05Zr - 0.05La - 0.20N (HS-556) Solution Heat TreatedAMS5874D (Current)10/16/2023
This specification covers a corrosion- and heat-resistant alloy in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Bars and Wire 18Cr - 9.0Ni (302) Solution Heat Treated, Cold Drawn and Stress Relieved 125 ksi (862 MPa) Tensile StrengthAMS5637K (Current)10/5/2023
This specification covers a corrosion-resistant steel in the form of bars and wire 0.75 inch (19 mm) and under in nominal diameter or distance between parallel sides (thickness).
AMS F Corrosion and Heat Resistant Alloys Committee
Powder, Plasma Spray 95Ni - 5AlAMS5793C (Current)4/1/2024
This specification covers a nickel-aluminum aggregate in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion and Heat-Resistant, Bars and Forgings and Forging Stock, 15.5Cr - 4.5Ni - 2.9Mo - 0.10N (AM 355®), Consumable Electrode Remelted, Heat Treated, 170 ksi (1172 MPa) Tensile StrengthAMS5744G (Current)9/18/2024
This specification covers a corrosion- and heat-resistant steel in the form of bars, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe 1800 °F (982 °C) Solution Heat Treated, Precipitation HardenableAMS5747E (Current)11/18/2022
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and flash welded rings up to 4.00 inches, including (101.6 mm, including) in nominal diameter or least distance between parallel sides, and stock of any size for forging or flash welded rings (see 8.5).
AMS F Corrosion and Heat Resistant Alloys Committee
Hose Assemblies, Metal, Medium Pressure, High TemperatureAS1424H (Current)4/7/2020
This SAE Aerospace Standard (AS) covers medium-pressure, high-temperature, flexible, metal-hose assemblies suitable for operation in pneumatic systems up to 800 °F with excursion to 1200 °F for Class “B” and “N” and primarily for use on jet aircraft power plants. See 1.2.1 for recommended usage.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
ADAPTER, ASSEMBLY - PORT CONNECTION RING LOCKED TO 24° FLARELESS TUBE END, METRICMA2112C (Current)4/18/2017
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Aluminum Alloy, Heat-Resistant, Castings 5.0Cu - 1.5Ni - 0.25Mn - 0.25Sb - 0.25Co - 0.20Ti - 0.20Zr (203.0-T6) Solution Heat Treated and Precipitation Heat TreatedAMS4225F (Current)5/14/2026
This specification covers an aluminum alloy in the form of castings.
AMS D Nonferrous Alloys Committee
TUBING, PLASTIC, FLEXIBLE, CONVOLUTED, ANNULAR POLYVINYLIDENE FLUORIDE (PVDF), THERMALLY STABILIZED, STANDARD CONVOLUTIONSAS81914/8C (Current)6/30/2025
AE-8C1 Connectors Committee
Plastic Extrusions and Moldings, Polycarbonate General PurposeAMS3628E (Current)11/7/2011
This specification covers a polycarbonate resin in the form of extrusions and moldings.
AMS P Polymeric Materials Committee
BOLTS AND SCREWS, CARBON STEELS, ALLOY STEELS OR CORROSION AND HEAT RESISTANT STEELS OR ALLOYS Roll ThreadedAMS7473E (Current)5/1/1995
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Castings, 7.0Si - 0.32Mg (356.0-T6), Solution and Precipitation Heat TreatedAMS4217K (Current)9/23/2025
This specification covers an aluminum alloy in the form of castings (see 8.6).
AMS D Nonferrous Alloys Committee
FABRIC, GLASS (182) (DECORATIVE GRADE)AMS3836 (Current)12/31/2012
AMS P Polymeric Materials Committee
Fluid, Hydraulic Fire ResistantAMS3150C (Current)7/1/1986
1. ACKNOWLEDGMENT: A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. 2. APPLICATION: , For use in commercial aircraft hydraulic systems. 3. COMPOSITION: There shall be no restrictions on the type of materials used in the fluid except those imposed by the technical requirements of this specification.
AMS B Finishes Processes and Fluids Committee
Studs, Steel, UNS S66286 Tensile Strength 130 ksi 1800 °F Solution Heat Treated, Aged Before Roll Threading Procurement SpecificationAS7482C (Current)10/28/2021
This specification covers studs made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
E-25 General Standards for Aerospace and Propulsion Systems
BOLTS AND SCREWS, CORROSION AND HEAT RESISTANT STEEL Upset Headed, Heat Treated, Roll Threaded 1800°F (982°C) Solution and Precipitation Heat TreatedAMS7477C (Current)5/1/1995
AMS F Corrosion and Heat Resistant Alloys Committee
INSERT, SCREW THREAD, HELICAL COIL, METRIC SERIES, SCREW LOCKING, CRES, UNCOATEDMA3329E (Current)2/27/2024
E-25 General Standards for Aerospace and Propulsion Systems
BOLTS AND SCREWS, WORK-STRENGTHENED ALLOY, CORROSION RESISTANT Forged Head, Roll Threaded After AgingAMS7468 (Current)5/1/1995
This specification covers aircraft-quality bolts and screws having UNJ (MIL-S-8879) thread form, made from a corrosion-resistant, work-strengthened cobalt-chromium-nickel alloy and aged to develop the specified properties.
AMS F Corrosion and Heat Resistant Alloys Committee
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