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Deoxidizer, Acidic, for Magnesium AlloysAMS1538B (Current)07/09/2012
This specification covers an acidic deoxidizer in the form of a liquid
AMS J Aircraft Maintenance Chemicals and Materials Committee
Material Specification
Steel Sheet, Strip, and Plate, Low Alloy, Heat-Resistant 0.65Si - 1.25Cr - 0.50Mo - 0.25V (0.27 - 0.33CAMS6385L (Current)04/28/2020
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
Material Specification
Interior Decorative Clear Coating for Metal SurfacesAMS7200 (Current)02/10/2020
This specification establishes requirements for an interior decorative clear coating for wear protection of metal substrates
AMS G8 Aerospace Organic Coatings Committee
Material Specification
Castings, Leaded Bronze, Sand and Centrifugal 80Cu - 10Sn - 9.5Pb As CastAMS4842F (Current)09/07/2018
This specification covers a leaded bronze in the form of sand and centrifugal castings
AMS D Nonferrous Alloys Committee
Material Specification
Insulation Sleeving, Electrical, Heat Shrinkable, Polyolefin, Semi-Rigid, CrosslinkedAMSDTL23053/6B (Current)12/07/2018
The requirements for acquiring the sleeving described herein shall consist of this specification sheet and the issue of the following specification listed in that issue of the Department of Defense Index of Specifications and Standards (DODISS) specified in the solicitation: MIL-DTL-23053
AE-8D Wire and Cable Committee
Material Specification
Steel, Corrosion Resistant, Wire 18Cr - 9.0Ni (302) Spring TemperAMS5688M (Current)01/02/2019
This specification covers a corrosion resistant steel in the form of wire
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Steel, Investment Castings 0.50Cr - 0.55Ni - 0.20Mo (0.25 - 0.35C) (SAE 8630 Mod) Normalized and TemperedAMS5334J (Current)01/19/2024
This specification covers a low-alloy steel in the form of investment castings
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Wire, Steel Welding 2.0Cr - 10Ni - 8.0Co - 1.0Mo - 0.02Al - 0.06V (0.10 - 0.14C) (HY-180) Vacuum Melted, Environment Controlled PackagingAMS6465E (Current)08/02/2017
This specification covers a low-alloy steel in the form of welding wire
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Rings, Piston, Cast Iron As CastAMS7310L (Current)09/21/2020
This specification covers piston rings fabricated from cast iron
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum Alloy, Die and Hand Forgings, Rolled Rings, and Forging Stock 2.3Cu - 1.6Mg - 1.1Fe - 1.0Ni - 0.18Si - 0.07Ti (2618-T61) Solution and Precipitation Heat TreatedAMS4132H (Current)01/02/2019
This specification covers an aluminum alloy in the form of die forgings, hand forgings, and rolled rings 4 inches (102 mm) and under in nominal thickness, and forging stock of any size (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
SYNCHRO CONTROL TRANSMITTER, TYPE 31CX6aAS20708/139B (Current)05/22/2017
AE-7A Generators and Controls Motors and Magnetic Devices
Technical Standard
Leakage, Requirements and Test Methods, for Fuel Couplings, Pneumatic Couplings, Hydraulic Fittings, Quick Disconnects, and Hose AssembliesARP4785A (Current)09/01/1999
This SAE Aerospace Recommended Practice (ARP) establishes the suggested requirements and test methods for the evaluation, qualification testing, and/or acceptance testing of fuel and pneumatic couplings, quick disconnects, hydraulic fittings, and hose assemblies. The paragraphs noted herein are general words and may be modified to fit specific hardware, materials, and usage which will appear in procurement specifications
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Recommended Practice
AS9000 Audit Summary and Supplier Profile InstructionsAS9000-APPNDX1A (Current)12/19/2003
To assure customer satisfaction, aerospace industry manufacturers must produce world class quality products at the lowest possible cost. AS9000 standardizes, to the greatest extent possible, the quality system requirements of the aerospace industry. Standardization of compliance requirements results in cost savings due to the elimination or reduction of unique requirements developed for each different customer. AS9000 Appendix 1, AS9000 Audit Summary and Supplier Profile Instructions, facilitates the standardization of this process
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Technical Standard
Flight Deck Tire Pressure Monitoring System (TPMSARP4102/3 (Current)01/03/2017
This document recommends design criteria for a Flight Deck Tire Pressure Monitoring System. The requirements arise from operational experience of incidents, which have led to considerable damage to aircraft systems and structures caused by tire debris and wheel fragments
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
Recommended Practice
Plain Bearing Bond Integrity - Peelable Woven Fabric PTFE LinersARP5448/4 (Current)08/13/2018
This test method outlines a recommended procedure for performing bond integrity tests of bonded peelable woven fabric reinforced polytetrafluoroethylene (PTFE) liners, hereafter referred to within this document as "PTFE liner" or "liner". The data from these tests shall be used to determine if the product meets the "bond integrity" requirements of the applicable specifications
ACBG Plain Bearing Committee
Recommended Practice
Blackening Solution for Steel Touch-Up MethodAMS2484C (Current)01/04/2019
This specification covers the requirements for an inorganic blackening solution for steel, applied at room temperature
AMS B Finishes Processes and Fluids Committee
Material Specification
Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 73Ni - 0.14C - 13Cr - 4.5Mo - 2.3Cb (Nb) - 0.75Ti - 6.0Al - 0.010B - 0.10Zr Vacuum Cast, As-CastAMS5391H (Current)07/30/2019
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T76511) Solution Heat Treated, Stress Relieved, Straightened, and OveragedAMS4159F (Current)07/08/2020
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing with a nominal diameter or least thickness (wall thickness of tubing) up to 5.000 inches (127 mm), inclusive (see 8.4
AMS D Nonferrous Alloys Committee
Material Specification
Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 53.3Ni - 16.5Cr - 17Mo - 4.5W - 5.8Fe - 0.40V (CW-12MW) As-CastAMS5388K (Current)07/30/2019
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Steel Bars, Forgings, and Tubing, Nitriding 1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C) Double Vacuum Melted Premium Aircraft-Quality for Bearing ApplicationsAMS6498B (Current)01/04/2019
This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6496 and AMS6497 cover UNS K23280 with other quality levels
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Magnesium Alloy, Sand Castings 3.2 Rare Earths - 2.5Zn - 0.70Zr (EZ33A-T5) Precipitation Heat TreatedAMS4442H (Current)01/04/2019
This specification covers a magnesium alloy in the form of sand castings
AMS D Nonferrous Alloys Committee
Material Specification
Scale Conditioner, Alkaline Aircraft Turbine Engine ComponentsAMS1380B (Current)07/29/2020
This specification covers a strongly alkaline scale conditioner in the form of a liquid or a water-soluble powder
AMS J Aircraft Maintenance Chemicals and Materials Committee
Material Specification
Steel, Corrosion Resistant, Seamless and Welded Aircraft Tubing 19Cr - 9.5Ni (304) Cold Drawn, 1/2 Hard TemperAMS5868C (Current)01/02/2019
This specification covers a corrosion-resistant steel in the form of two types of aircraft tubing
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Universal Turnover Build-Up Stand for Small Propulsion Units Requiring Vertical AssemblyARP863B (Current)12/05/2012
This recommended practice covers a stand that may be used for assembly, disassembly, and maintenance. The stand incorporates the following design criteria: complete interchangeability of any and all components, collapsible frame construction, envelope dimensions (marked with an asterisk on the attached drawings), attachment pad configuration, and gearbox and caster specifications
AGE-2 Air Cargo
Recommended Practice
Aluminum Alloy, Investment Castings 7.0Si - 0.32Mg (356.0-T6) Solution and Precipitation Heat TreatedAMS4260G (Current)10/01/2014
This specification covers an aluminum alloy in the form of castings
AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy Powder 10.0Si - 0.35MgAMS7018 (Current)05/11/2020
This specification covers an aluminum alloy in the form of pre-alloyed powder
AMS AM Additive Manufacturing Metals
Material Specification
Steel, Corrosion and Heat-Resistant, Bars and Forgings 15.5Cr - 4.5Ni - 2.9Mo - 0.10N Consumable Electrode Remelted Solution Heat Treated, Sub-Zero Cooled, Equalized, and Over-TemperedAMS5743K (Current)05/11/2020
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
Material Specification
Steel, Corrosion-Resistant, Sheet, Strip, and Plate 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu Consumable Electrode Remelted, Solution Heat Treated Precipitation-HardenableAMS5862M (Current)07/20/2017
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 4.0 inches (102 mm) and under in nominal thickness (see 8.5
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Magnesium Alloy, Sand Castings 2.5Ag - 2.1Di - 0.70Zr (QE22A-T6) Solution and Precipitation Heat TreatedAMS4418J (Current)12/27/2018
This specification covers a magnesium alloy in the form of sand castings
AMS D Nonferrous Alloys Committee
Material Specification
Steel, Corrosion and Moderate Heat-Resistant, Investment Castings 12.5Cr (410) Hardened and TemperedAMS5350K (Current)11/18/2022
This specification covers a corrosion and moderate heat-resistant steel in the form of investment castings
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Castings, Sand - Aluminum Bronze 85cu 11.2al 3.6fe, as CastAMS4872C (Current)07/01/1990
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of January 1990
AMS D Nonferrous Alloys Committee
Material Specification
Plating, Brush, Nickel Low Stress, Hard DepositAMS2451/2B (Current)10/20/2022
This specification covers the requirements and process controls for brush plating of hard, low stress nickel by electrodeposition
AMS B Finishes Processes and Fluids Committee
Material Specification
BOLT, MACHINE - STEEL, CADMIUM PLATED, HEXAGON HEAD, UNS G87400, 125 KSI MIN, .7500-16 UNJF-3AAS9526C (Current)07/23/2015
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, BUSSING MODULES, FEEDBACK TYPE, SIZE 12, SERIES IAS81714/4A (Current)07/13/2022
AE-8C2 Terminating Devices and Tooling Committee
Technical Standard
Installation of Window Anti-Icing, De-Greasing, and Washing Systems (General SpecificationAS18259 (Current)08/01/1997
This specification covers the general requirements for the design and installation of fluid anti-icing, de-greasing, and washing systems installed in military aircraft
Aerospace Council
Technical Standard
Silicon Bronze Tubing, Seamless 96cu 3.2si, AnnealedAMS4665B (Current)09/01/1996
Primarily for hydraulic pressure lines. This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: C65500 UNS Number: C65500
AMS D Nonferrous Alloys Committee
Material Specification
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 23Cr - 13.5Ni (309S) Solution Heat TreatedAMS5650G (Current)11/18/2022
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
Material Specification
Lubricant, Dry Film, Heat Cured, For Fasteners Polysulfide Sealant CompatibleAMS3090B (Current)09/23/2011
This specification covers a dry film lubricant in the form of lubricating solids dispersed in a resin binder and suitable solvents to produce a sprayable liquid
AMS G9 Aerospace Sealing Committee
Material Specification
Steel, Welding Wire 0.30Cr - 1.8Ni - 0.40Mo - (0.23-0.28C) Vacuum Melted, Environment Controlled PackagingAMS6453D (Current)03/04/2018
This specification covers a low-alloy steel in the form of welding wire
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum Alloy 5454, Bar, Rod, Shapes, Tube, and Wire, ExtrudedAMSQQA200/6C (Current)12/07/2017
This specification covers the specific requirements for aluminum alloy 5454 bar, rod, shapes, tube, and wire produced by extrusion
AMS D Nonferrous Alloys Committee
Material Specification
Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities High Strength, for Intermittent Use to 360 °F (182 °CAMS3269C (Current)09/23/2011
This specification covers three classes of fuel-resistant polysulfide (T) sealing compound with high strength and temperature characteristics, supplied as a two-component system which cures at room temperatures
AMS G9 Aerospace Sealing Committee
Material Specification
Sheet, Polyether Urethane (EU) Elastomer Foam Shock AbsorbingAMS3568B (Current)08/25/2011
This specification and its supplementary detail specifications cover a chemically or mechanically expanded polyether urethane (EU) elastomeric foam material in the form of ready-to-use sheet
AMS P Polymeric Materials Committee
Material Specification
Foam, Polyether Urethane (EU) Elastomer, Shock Absorbing 20 Pounds/Cubic Foot (320 kg/m3) DensityAMS3568/3B (Current)08/25/2011
This specification covers a chemically or mechanically expanded polyether urethane (EU) elastomeric foam material in the form of ready-to-use sheet
AMS P Polymeric Materials Committee
Material Specification
Heat Treatment of Aluminum Alloy CastingsMAM2771B (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 AMS2771. The requirements of the latest issue of AMS2771 shall be fulfilled whenever reference is made to the cancelled MAM2771. 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 AMS2771
AMS D Nonferrous Alloys Committee
Material Specification
Detail Requirements for 4,000 & 5,000 Psi Aircraft Hydraulic SystemsARP578 (Current)07/01/1994
The purpose of this document is to outline and publish the criteria applicable to design and installation for types I and II, classes 4000 and 5000 psi aircraft hydraulic systems
A-6A2 Military Aircraft Committee
Recommended Practice
Standard Electrical and Logical Interface for Airborne Fuzing SystemsAS5716A (Current)12/03/2012
This interface standard applies to fuzes/fuzing systems (referred to as fuzing system hereafter) in airborne weapons that use a MIL-STD-1760 type interface. It defines the powers, the discrete signals and the serial data interface for the communications at the interface between the fuzing system and the remainder of the weapon, including the weapon control unit. The Class 1 interface is an electrical only interface that facilitates use of MIL-STD-1760 type platform store interfaces for the fuze to monitor intentional release and defines the fuze interface bus communications protocol to allow sending and receiving data from fuzing systems. Class 2 interfaces add a defined connector and additional interfaces to facilitate the exchange of compatible fuzing systems. Class 3 interfaces add further interface definitions to facilitate the exchange of AS5680A compatible fuzing systems components. The bus communications protocol provides a means by which the weapon may set mission parameters
AS-1B Aircraft Store Integration Committee
Technical Standard
COVER - TYPE XVI, XVII-C, D, E, AND F ENGINE ACCESSORY DRIVEAS3542A (Current)06/20/2018
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
SCREW - OVAL FILLISTER, DRILLED HEAD, CADMIUM PLATED, STEEL UNS K00802, .1120-40 UNC - 2AAS116913C (Current)06/20/2018
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
BRACKET, ANGLE, 90°, CRES UNS S41000, .190 X .250 BOLTAS9601B (Current)06/20/2018
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Sealing Compound, Silicone Rubber, Two-Part, Electrically Conductive and Corrosion Resistant (Nonchromated) for Use from -67 to 500 °F (-55 to 260 °CAMS3262A (Current)09/23/2011
This specification covers a silicone, electrically conductive and corrosion-inhibiting sealing compound
AMS G9 Aerospace Sealing Committee
Material Specification
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