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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
Anodic Treatment of Magnesium Alloys Acid Type, Full CoatAMS2478F (Current)12/13/2023
This specification establishes the engineering requirements for producing an acid-type, anodic coating on magnesium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
Compound, Hot Carbon and Paint Remover Aircraft Turbine Engine ComponentsAMS1385A (Current)6/23/2025
This specification covers a solvent-based compound in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Disposition of Wheels Which Have Been OverheatedAIR811C (Current)2/9/2006
The development and use of brakes with high temperature capabilities has resulted in instances of tire and wheel failures which were attributed to excessive brake heat. These instances have led to the establishment of more stringent wheel requirements and the addition of heat shields, safety devices, auxiliary cooling devices, brake temperature and low tire pressure indication systems. This SAE Aerospace Information Report (AIR) has been prepared to assist those who are concerned with the removal, inspection, and disposition of magnesium and aluminum wheels which may have been subjected to excessive temperatures.
A-5A Wheels, Brakes and Skid Controls Committee
FLUORESCENT PENETRANT INSPECTIONAMS2645K (Current)2/1/1995
AMS K Non Destructive Methods and Processes Committee
Investigation of PTFE "Melt" Phenomenon for High Pressure HosesAIR4092B (Current)3/16/2021
To provide information regarding a unique failure mode and alternate solutions for consideration by application designers.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Skin Protective Compound, Chemical BarrierAMS1725C (Current)7/25/2005
This specification covers three types of semi-solid skin protective compounds in the form of barrier creams.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Chloroprene (CR) Rubber Sheet, Nylon Cloth Reinforced Weather ResistantAMS3273F (Current)8/25/2011
This specification covers nylon-cloth-reinforced chloroprene (CR) rubber in the form of sheet.
AMS P Polymeric Materials Committee
Silicone Potting Compound, Elastomeric Two-Part, General Purpose 80 to 180 Poise (8 to 18 Pa·s) ViscosityAMS3358C (Current)1/17/2012
This specification covers a room-temperature-vulcanizing, elastomeric silicone compound.
AMS G9 Aerospace Sealing Committee
Elastomer: Silicone (VMQ) Rubber Sheet, Glass Cloth Reinforced Heat and Weather Resistant 60 to 80 Type “A” Durometer HardnessAMS3320J (Current)5/10/2019
This specification covers a silicone (VMQ) elastomer, reinforced with glass cloth, in the form of sheet.
AMS CE Elastomers Committee
Cloth, Knitted Nylon Stretch Polychloroprene CoatedAMS3271B (Current)8/25/2011
This specification covers a polychloroprene-coated, one side only, nylon knit in the form of cloth.
AMS P Polymeric Materials Committee
Importance of Physical and Chemical Properties of Aircraft Hydraulic FluidsAIR81E (Current)10/2/2019
This document discusses the relative merits of the physical and chemical properties of hydraulic fluids in relation to the aerospace hydraulic system design, and the related materials compatibility. The discussion in this report applies both to hydrocarbon and phosphate ester based aircraft hydraulic fluids. In some cases, numerical limits are suggested, but, in general, the significance and effect of a property is noted qualitatively.
A-6C1 Fluids and Contamination Control Committee
Cleaner, Transparent PlasticAMS1535D (Current)9/28/2018
This specification covers a cleaner for plastics in the form of a liquid.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Oxide Conditioner, Alkaline Permanganate Aircraft Turbine Engine ComponentsAMS1383B (Current)7/23/2020
This specification covers an alkaline permanganate oxide conditioner in the form of a water-soluble powder or a liquid for dilution with water.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Steel, Maraging, Bars, Forgings, Mechanical Tubing, Flash-Welded Rings, and Stock for Forging and Flash-Welded Rings, 19Ni - 3.0Mo - 1.4Ti - 0.10Al (Alloy T250), Premium Aircraft Quality, Double Vacuum Melted, AnnealedAMS6519F (Current)8/1/2024
This specification covers a premium aircraft-quality, maraging steel in the form of bars, forgings, mechanical tubing, flash-welded rings up to 10.0 inches (254 mm) in diameter or least distance between parallel sides (thickness), and stock of any size for forging or flash-welded rings (see 8.6).
AMS E Carbon and Low Alloy Steels Committee
Elastomer: Fluorosilicone Rubber (FVMQ) High Temperature, High Modulus, Fuel and Oil Resistant 70 - 80 Shore A Hardness For Products in Fuel Systems/Lubricating OilsAMS3327E (Current)2/27/2019
This specification covers a fluorosilicone (FVMQ) elastomer that can be used to manufacture product in the form of sheet, strip, and molded shapes. This specification should not be used for molded rings, compression seals, O-ring cord, and molded in place gaskets for aeronautical and aerospace applications without complete consideration of the end use prior to the selection of this material.
AMS CE Elastomers Committee
Primer, Ocher PhenolicAMS3108G (Current)9/23/2011
This specification covers an ocher-pigmented primer.
AMS G8 Aerospace Organic Coatings Committee
Felt, Back Check, White 100% WoolAMS3285F (Current)8/25/2011
This specification covers felted wool fibers in the form of sheets and rolls.
AMS P Polymeric Materials 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
Piston Rings, Centrifugally-Cast IronAMS7312H (Current)1/13/2016
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings.
AMS E Carbon and Low Alloy Steels Committee
Steel Sheet, Strip, and Plate, Maraging, 19ni 3.0mo 1.4ti 0.10al Double Vacuum Melted, Solution Heat TreatedAMS6518C (Current)3/12/2004
This specification covers a premium aircraft-quality maraging steel in the form of sheet, strip, and plate. Primarily for parts such as pressure vessels, and other components requiring through-hardening, without quenching, to a yield strength of 245,000 psi (1690 MPa) or higher.
AMS E Carbon and Low Alloy Steels Committee
Steel, Corrosion-Resistant, Sheet and Strip 18Cr - 9.0Ni (302) Cold Rolled, 3/4 Hard, 175 ksi (1207 MPa) Tensile StrengthAMS5905D (Current)3/27/2024
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Hose, Aircraft Fueling, Acrylonitrile Butadiene (NBR) Rubber Single Wire Braid Reinforced, Chloroprene Covered, NoncollapsingAMS3388E (Current)4/30/2019
This specification covers a synthetic rubber in the form of a non-rigid, smooth bore, noncollapsing-type hose.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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, Corrosion-Resistant, Sheet and Strip 18Cr - 8Ni (SAE 301) Cold Rolled, 3/4 Hard, 175 ksi (1207 MPa) Tensile StrengthAMS5902E (Current)7/16/2025
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Rings, Sealing, Fluorocarbon Rubber High Temperature-Fluid-Resistant, 70-80AMS7278F (Current)5/1/1995
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of 10/17/90. Use AMS 7276 or 7280
AMS CE Elastomers Committee
Alloy Billets and Preforms, Corrosion and Heat Resistant, 59.5ni 12cr 10co 3.0mo 6.0w 3.0ti 1.5ta 4.5al 0.015b 0.10zr (0.30-0.35c), Powder-Metallurgy ProductAMS5856B (Current)10/1/1998
This specification covers a corrosion and heat resistant nickel alloy powder-metallurgy product in the form of billets and preforms for forgings. Primarily for parts requiring high strength up to 1500 degrees F (815 degrees C) and corrosion and oxidation resistance up to 1700 degrees F (925 degrees C). This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of October 16, 1986. It is recommended that this specification not be specified for new designs.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion and Heat Resistant, Seamless and Welded Hydraulic Tubing 17Cr - 12Ni - 1.5Mo - 0.03C max Cold Drawn, 1/8 Hard TemperAMS5584B (Current)1/14/2022
This specification covers a corrosion and heat resistant steel in the form of two types of thin-wall, close-tolerance tubing 0.125 to 2.00 inches (3.18 to 50.8 mm), inclusive, in nominal OD.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Bars, Wire, Forgings, Mechanical Tubing and Forging Stock, Corrosion Resistant 14Cr - 2.1Mo - 0.30Cb (Nb) - 1.0V (1.05 - 1.15C) Premium Aircraft Quality for Bearing Applications, Double Vacuum Melted, AnnealedAMS5900D (Current)2/25/2025
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 17Cr - 0.52Mo (0.95 - 1.20C) (SAE 51440C) for Bearing ApplicationsAMS5880F (Current)5/1/2024
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Elastomer: Fluorosilicone (FVMQ) Rubber Fuel and Oil Resistant 45 - 55 Shore A Hardness For Products in Fuel Systems/Lubricating OilsAMS3330D (Current)8/16/2023
This specification covers a fluorosilicone (FVMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, molded O-ring cord, and molded in place gaskets for aeronautical and aerospace applications.
AMS CE Elastomers Committee
Steel, Corrosion-Resistant, Bars and Wire 19Cr - 10Ni (304) High Yield Strength, Solution Heat Treated and Cold WorkedAMS5857E (Current)6/30/2025
This specification covers a corrosion-resistant steel in the form of cold-worked bars and wire up to 1.750 inches (44.45 mm), inclusive, in nominal diameter or least distance between parallel sides.
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
CONNECTOR ACCESSORIES, ELECTRICAL, RING, POTTING BOOT, CATEGORY 5 (MIL-DTL-27599 CONNECTORS)AS85049/61C (Current)5/26/2021
AE-8C1 Connectors Committee
CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, ENVIRONMENTAL, 90°, SHIELD TERMINATION, CATEGORY 2B, NONSELF-LOCKING (MIL-DTL-38999 SERIES III AND IV CONNECTORS)AS85049/79C (Current)5/21/2021
AE-8C1 Connectors Committee
Titanium Alloy Welding Wire, 6Al - 4V, Extra Low Interstitial, Environment Controlled PackagingAMS4956J (Current)5/14/2026
This specification covers a titanium alloy in the form of wire for welding filler metal (see 8.5).
AMS G Titanium and Refractory Metals Committee
Titanium Alloy, Bars and Rods 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Centerless Ground or Peeled and PolishedAMS4958F (Current)11/2/2022
This specification covers a titanium alloy in the form of bars and rods 1.00 inch (25.4 mm) and under in nominal diameter.
AMS G Titanium and Refractory Metals Committee
Alloy, Corrosion- and Heat-Resistant, Bars and Forgings 53Ni - 15Cr - 18.5Co - 5.0Mo - 3.2Ti - 4.2Al - 0.03B Double Vacuum Melted Solution, Stabilization, and Precipitation Heat TreatedAMS5846D (Current)2/7/2022
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Sheet and Strip 15cr 8.4ni 2.2mo 1.1al Vacuum Induction Melted, Solution Heat TreatedAMS5603E (Current)5/1/2001
This specification covers a corrosion-resistant, precipitation-hardenable steel in the form of sheet and strip.
AMS F Corrosion and Heat Resistant Alloys Committee
Oxygen Systems for General AviationAIR822C (Current)7/11/2014
This SAE Aerospace Information Report (AIR) provides a general overview of oxygen systems for general aviation use. Included are a brief review of the factors and effects of hypoxia, system descriptions, and mission explanations for system or component selection, and techniques for safe handling of oxygen distribution systems.
A-10 Aircraft Oxygen Equipment 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
CONTACTS, ELECTRICAL CONNECTOR, PIN CRIMP REMOVABLE (FOR AS81511 SERIES 3 AND 4 CONNECTORS)AS39029/18D (Current)3/13/2026
AE-8C1 Connectors 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
Aluminum Alloy, Sheet and Plate, Alclad 4.3zn 3.3mg 0.6cu 0.20mn 0.17crAMS4199A (Current)4/1/1991
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Foil 2.5Mg - 0.25Cr (5052-H191) Strain HardenedAMS4004E (Current)12/3/2015
This specification covers an aluminum alloy in the form of foil.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Drawn, Round Seamless Tubing Close Tolerance 2.5Mg - 0.25Cr (5052-O) AnnealedAMS4069G (Current)9/21/2023
This specification covers an aluminum alloy in the form of drawn, round seamless tubing 0.010 to 0.450 inch (0.25 to 11.43 mm), inclusive, in wall thickness (see 8.5).
AMS D Nonferrous Alloys Committee
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