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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
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
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
FITTING, ADAPTER, FLARED TUBE, .375 BULKHEAD TO BOSS FOR SEAL RINGAS4318B (Current)5/12/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
JAUS Environment Sensing Service SetAS6060A (Current)5/11/2026
This document defines a set of standard application layer interfaces called JAUS Environment Sensing Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned systems to communicate and coordinate their activities. The Environment Sensing Services represent typical environment sensing capabilities commonly found across all domains and types of unmanned systems in a platform-independent manner. At present, twelve services are defined in this document: Range Sensor: Determine the proximity of objects in the platform’s environment Visual Sensor: Provides common configuration and setup for different types of imaging systems Digital Video: A type of Visual Sensor that manages digital video Analog Video: A type of Visual Sensor that manages analog video Still Image: A type of Visual Sensor that manages and encodes individual digital images Digital Audio Sensor: Provides common configuration and setup for different types of audio streams
AS-4JAUS Joint Architecture for Unmanned Systems Committee
Compound, Cleaning Gel for Aircraft SurfacesAMS79_015 (Current)5/11/2026
This SAE Standard specifies requirements for a gelled compound for cleaning the soiled exterior of service aircraft. The cleaning gel may be applied by pressure pump as a thixotropic liquid, by brushing or by swabbing. The surfaces to be cleaned may be unpainted metal or surfaces painted with glossy or matt schemes, including strippable acrylic paint complying with DTD 5599. This Standard includes tests to limit specific forms of corrosion that affect aircraft structural materials.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Ultrasonic Inspection, Thin Wall Metal TubingAMS2634D (Current)5/11/2026
This specification covers procedures for ultrasonic inspection of thin wall metal tubing of titanium, titanium alloy, and corrosion- and heat-resistant steels and alloys having nominal OD over 0.1875 inch (4.762 mm) with OD to wall thickness ratio of 8 or greater and wall thickness variation not exceeding ±10% of nominal.
AMS K Non Destructive Methods and Processes Committee
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings and Stock for Forging, Flash-Welded Rings or Heading, 13Cr - 2.0Ni - 3.0W (Greek Ascoloy), AnnealedAMS5616P (Current)5/11/2026
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, flash-welded rings, or heading.
AMS F Corrosion and Heat Resistant Alloys Committee
Contractile Strain Ratio Testing of Titanium Hydraulic TubingAS4076A (Current)5/11/2026
This SAE Aerospace Standard establishes the requirements and procedures for Contractile Strain Ratio (CSR) testing of cold-worked and stress-relieved titanium tubing such as Ti-3AI-2.5V tubing per AMS 4944.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Compound, Cleaning, Foaming, for Aircraft SurfacesAMS79_017 (Current)5/11/2026
This SAE Standard specifies requirements for a foaming liquid cleaning compound which, when diluted with water 1:9 v/v, is suitable for cleaning the soiled exterior of Service aircraft. The cleaning compound may be applied by spraying, either as foam or liquid, by brushing or by swabbing. The surfaces to be cleaned may be unpainted metal or surfaces painted with glossy or matt schemes, including strippable acrylic paint complying with DTD 5599. This Standard includes tests to limit specific forms of corrosion that affect aircraft structural materials.
AMS J Aircraft Maintenance Chemicals and Materials Committee
CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS)AS39029/83C (Current)5/11/2026
AE-8C1 Connectors Committee
SLEEVE, CHAFE-PROTECTION, WRAP-AROUND, SELF-CLOSING (-55° TO +260°C)AS60491/2 (Current)5/6/2026
AE-8D Wire and Cable Committee
SLEEVE, CHAFE-PROTECTION, EXPANDABLE (-55 TO +200 °C)AS60491/3 (Current)5/6/2026
AE-8D Wire and Cable Committee
BOLT, SHEAR - DOUBLE HEX HEAD, UNS N07718 - 185 KSIAS3574C (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
WIRE - STEEL, CORROSION AND HEAT RESISTANT, SAFETY, 1800 °FAS9226B (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 3 - Purchasing Specification for Unidirectional Carbon Fiber Tape Epoxy Repair PrepregAMS6885/3 (Current)5/7/2026
This Purchasing Specification, AMS6885/3, specifies the batch release and delivery requirements for unidirectional carbon fiber tape epoxy prepreg used for repair. This specification is applicable only when the unidirectional carbon fiber tape epoxy prepreg is used as part of the repair system defined in AMS6885 and AMS6885/1. This specification also defines the procedure and requirements for storage life extension of materials purchased against this specification. It is only applicable for materials qualified against AMS6885 (refer to PRI-QPL-AMS6885) and shall be carried out within the responsibility of the purchaser and under control of its Quality organisation.
AMS CACRC Commercial Aircraft Composite Repair Committee
Safety Cable Kit Procurement Specification and Requirement for UseAS4536D (Current)5/4/2026
This procurement specification covers aerospace quality safety cable kits consisting of safety cables and ferrules made from the same corrosion and heat resistant steels and a nickel base alloy of the type identified under the Unified Numbering System as follows: a. UNS S30400 - Corrosion resistant steel (AMS5697, AMS5560) b. UNS S32100 - Corrosion and heat resistant steel (AMS5689, AMS5570) c. UNS N06600 - Nickel base alloy (AMS5687, AMS5580) d. UNS N06625 - Nickel alloy, corrosion resistant (AMS5666, AMS5581) The requirements for installation practices are also specified.
E-25 General Standards for Aerospace and Propulsion Systems
NUT, SELF-LOCKING, DOUBLE HEXAGON, SOLID FILM LUBRICATED, EXTENDED WRENCH PAD, 160 KSI, 800 °F, UNS S66286AS3563E (Current)5/5/2026
E-25 General Standards for Aerospace and Propulsion Systems
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 5 - Material Specification for Unidirectional Carbon Fiber Tape Epoxy Prepreg for Repair and Film Adhesive for Repair, 120 to 145 °C (250 to 290 °F) CuringAMS6885/5 (Current)5/7/2026
AMS6885/5 is the Material Specification (MS) which defines the requirements of a unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. It also defines the requirements of an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
AMS CACRC Commercial Aircraft Composite Repair Committee
INSERT, SCREW THREAD, NON-LOCKING, LOCKED IN, KEY LOCKED, EXTRA HEAVY-DUTY, SELF-BROACHING KEYS, UNS S66286AS3573B (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
Heat Treatment of Steel Raw MaterialsAMS2761 (Current)7/8/2020
This specification establishes general requirements for the heat treatment of steel raw material (see 8.2.1) by producers or for producers.
AMS E Carbon and Low Alloy Steels Committee
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, Nitriding, 1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C) (32CrMoNiV5), Aircraft-Quality for Bearing ApplicationsAMS6496C (Current)3/13/2026
This specification covers a nitriding grade of aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6497 and AMS6498 cover UNS K23280 having other quality levels.
AMS E Carbon and Low Alloy Steels Committee
Chord Method of Evaluating Surface Microstructural CharacteristicsARP1820C (Current)5/19/2021
This practice provides a method for evaluating microhardness and microstructure very close (0.002 inch (0.051 mm) or less) to the surface of a disk specimen. Specific accept/reject criteria for partial decarburization (3.7.1), inadvertent carburization/nitriding (3.7.3), total decarburization/intergranular oxidation (3.8), and other characteristics evaluated are to be found in the applicable specification where this ARP is referenced.
AMS E Carbon and Low Alloy Steels Committee
Steel Bars, Forgings, and Tubing 1.0Cr - 3.2Ni - 0.2Mo (0.12 - 0.17C) Premium Aircraft-Quality Double Vacuum MeltedAMS6549A (Current)6/3/2018
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
Steel, Bars, Wire, and Forgings 10.5Mo - 6W - 3.75Cr - 2V (1.25 - 1.40C) Powder Metallurgy Product Hot Isostatically PressedAMS6558A (Current)5/16/2023
This specification covers a premium aircraft-quality, high-alloy steel gas-atomized and HIP-consolidated in the form of bars, wire, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Rings, Piston, Cast Iron As CastAMS7310M (Current)3/3/2026
This specification covers piston rings fabricated from cast iron.
AMS E Carbon and Low Alloy Steels Committee
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 1.7Cr - 3.8Ni - 0.3Mo (0.32 - 0.38C), Aircraft-QualityAMS6539B (Current)1/16/2024
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
Tolerances Carbon and Alloy Steel TubingAMS2253F (Current)2/24/2018
This specification covers established inch/pound manufacturing tolerances applicable to carbon and alloy tubing ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range.
AMS E Carbon and Low Alloy Steels Committee
Steel, Maraging, Investment Castings 17Ni - 10Co - 4.6Mo - 0.30Ti - 0.06Al Vacuum Melted Homogenized, Overaged, and Solution Heat TreatedAMS5339H (Current)6/2/2022
This specification covers an alloy steel in the form of investment castings.
AMS E Carbon and Low Alloy Steels Committee
Tubing, Carbon Steel (1025) (Aircraft Quality)AMST5066B (Current)7/1/2020
This specification covers carbon steel (1025) tubing of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
Steel, Sheet, Strip, and Plate 1.8Ni - 0.80Cr - 0.25Mo (0.38 - 0.43C) (SAE 4340) Vacuum Consumable Electrode RemeltedAMS6454G (Current)8/30/2023
This specification covers a premium-aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings, and Forging Stock 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) (H-11) Consumable Electrode Vacuum Re-MeltedAMS6487M (Current)11/23/2021
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Steel, Sheet and Strip, 0.15 Carbon, Maximum (SAE 1010), Half Hard TemperAMS5044L (Current)12/3/2024
This specification covers a carbon steel in the form of sheet and strip.
AMS E Carbon and Low Alloy Steels Committee
Steel, Maraging, Bars, Forgings, Mechanical Tubing, Rings, and Forging Stock 18Ni - 7.8Co - 4.9Mo - 0.40Ti - 0.10Al Consumable Electrode Vacuum Melted, AnnealedAMS6512J (Current)9/8/2022
This specification covers a premium aircraft-quality, maraging alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings up through 10.000 inches (254.00 mm), inclusive, in diameter or least distance between parallel sides and stock of any size for forging or flash welded rings.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings and Forging Stock 3.5Cr - 9.5Ni - 18Co - 1.1Mo (0.13 - 0.17C) (Ferrium® C61) Premium Aircraft Quality, Double Vacuum Melted, Normalized, AnnealedAMS6517C (Current)8/1/2025
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings, and Mechanical Tubing 0.50Cr - 0.55Ni - 0.20Mo (0.18 - 0.23C) (SAE 8620)AMS6274S (Current)7/23/2021
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
Steel, Bars, Forgings and Forging Stock, 0.80Cr - 1.8Ni - 0.25Mo (0.35 - 0.40C) (4337), Aircraft QualityAMS6412R (Current)9/23/2025
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
Steel Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Aircraft QualityAMS6350R (Current)12/18/2024
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
Steel, Sheet, Strip, and Plate 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130) Aircraft Quality, SpheroidizedAMS6351M (Current)12/18/2024
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
Steel, Bars and Forgings, and Forging Stock 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C) Vacuum Melted, Normalized and Overaged Precipitation HardenableAMS6532L (Current)6/26/2024
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings 100 square inches (645 cm2) and under in cross-sectional area, and forging stock of any size.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars 0.90 - 1.03CAMS5132M (Current)1/28/2022
This specification covers a high-carbon steel in the form of bars.
AMS E Carbon and Low Alloy Steels Committee
Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and HigherAMS2759/2K (Current)7/7/2021
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of low-alloy steel parts to minimum ultimate tensile strengths of 220 ksi (1517 MPa) and higher. Parts are defined in AMS2759. The requirements for heat treatment of alloy Aermet100 are no longer part of this specification and can be found in AMS2759/3. Due to the limited hardenability of these materials, size limits have been added to this specification.
AMS E Carbon and Low Alloy Steels Committee
Steel, Nitriding, Bars, Forgings, Mechanical Tubing, and Stock for Forging, 1.6Cr - 0.35Mo - 1.13Al (0.38 - 0.43C) (135 Mod), Premium Aircraft Quality, Consumable Electrode Vacuum RemeltedAMS6471K (Current)12/26/2023
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
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 1.5Si - 1.25Cr - 3.8Ni - 0.50Mo - 0.30V (0.40C), Vacuum Remelted, AnnealedAMS6482C (Current)7/23/2024
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
Steel Bars 1.0Cr - 0.20Mo - 0.45Se (0.39 - 0.48C) (4142H Modified) Die-Drawn, 130 ksi (896 MPa) Yield Strength Free MachiningAMS6378J (Current)12/18/2024
This specification covers a free-machining, low-alloy steel in the form of round bars 3.50 inches (88.9 mm) and under in nominal diameter produced by a die-drawing process.
AMS E Carbon and Low Alloy Steels Committee
Steel, Bars, Forgings, Mechanical Tubing and Forging Stock, 0.80Cr - 0.85Ni - 0.20Mo - 0.003B (0.35 - 0.40C) (Modified 98B37), Aircraft QualityAMS6421J (Current)9/12/2025
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
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 0.92Cr - 0.75Ni - 0.52Mo - 0.003B - 0.04V (98BV40), Aircraft QualityAMS6423K (Current)10/23/2025
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
Steel Tubing, Seamless 0.31 - 0.38C (SAE 1035) Stress RelievedAMS5082J (Current)8/30/2023
This specification covers a carbon steel in the form of seamless tubing up through 1.500 inches (38.10 mm), inclusive, outer diameter.
AMS E Carbon and Low Alloy Steels Committee
Steel, Sheet and Strip 0.08 - 0.13C, Aluminum Killed (SAE 1010) Deep Forming GradeAMS5047G (Current)2/15/2017
This specification covers an aluminum-killed carbon steel in the form of sheet and strip.
AMS E Carbon and Low Alloy Steels Committee
Steel Bars, Forgings, Forging Stock, and Mechanical Tubing 1.6Si - 0.82Cr - 1.8Ni - 0.40Mo - 0.08V (0.40 - 0.44C) Consumable Electrode Vacuum Remelted Normalized and TemperedAMS6257G (Current)10/26/2022
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
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