Results

This specification establishes the requirements for an expanded polytetrafluoroethylene (EPTFE) in the form of sealing tape, gaskets, or sheets requiring no mixing or curing

AMS G9 Aerospace Sealing Committee

Cleaning and Preparation of Metal Surfaces

AMS03_2C (Current)

02/25/2020

This SAE Standard specifies processes for the cleaning of metal surfaces to remove any extraneous or undesirable material or deposits at any stage of manufacture, storage or service and for the preparation of these surfaces for further treatment. Any necessary stress-relieving treatments are also included. This Standard does not override special preparatory procedures specified in individual Defence Standards, Defence Specifications, DTD Process Specifications, DG Ships Specifications and Naval Defence Standards. It also does not cover cleaning operations associated with the maintenance of internal combustion engines, the preliminary removal of heavy deposits of oil, grease, or dirt accumulated during operational service, preparations for welding and the cleaning of electrical contacts

AMS B Finishes Processes and Fluids Committee

Plastic Moldings, Laminated, Thermosetting Resin Glass Cloth Reinforced Heat Resistant

AMS3642E (Current)

01/16/2012

This specification covers a glass-cloth-reinforced thermosetting resin in the form of laminated, pressure-bag or matched-die moldings

AMS P Polymeric Materials Committee

Plastic Sheet and Strip, Modified Vinyl, Foamed Closed Cell

AMS3635E (Current)

01/16/2012

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

ALUMINUM ALLOY CAS4TINGS, SAND 4.5Cu (195-T4) Solution Treated

AMS4230C (Current)05/01/1995

AMS D Nonferrous Alloys Committee

Magnetic Rubber Inspection

AMS2308A (Current)04/25/2005

This specification covers the procedural requirements necessary for the performance of magnetic rubber inspection

AMS K Non Destructive Methods and Processes Committee

Aluminum Alloy, Bar, Rod, and Wire, Rolled, Drawn, or Cold Finished, 1100

AMSQQA225/1B (Current)04/13/2007

This specification covers the specific requirements for 1100 aluminum alloy bar, rod, and wire produced by rolling, drawing, or cold finishing

AMS D Nonferrous Alloys Committee

Packing, Preformed, Petroleum Hydraulic Fluid Resistant, 160°F

AMSP5516A (Current)11/30/2010

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of November 2010. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Materials Specifications indicating that it has been "CANCELLED". This specification covers two classes of preformed packings for use where resistance to hydraulic fluid conforming to specification MIL-M-5606 is required at temperatures from -65° to 160°F

AMS CE Elastomers Committee

Steel, Corrosion-Resistant, Bars and Forgings 0.14S - 18Cr - 9.5Ni - 0.50Mo - 0.80Al (303MA) Free-Machining; Swaging or Upsetting Solution Heat Treated

AMS5638G (Current)

05/04/2021

This specification covers a free-machining, corrosion-resistant steel in the form of bars, forgings, and forging stock

AMS F Corrosion and Heat Resistant Alloys Committee

Steel, Corrosion and Heat Resistant, Seamless Tubing 23Cr - 13.5Ni (309S) Solution Heat Treated

AMS5574F (Current)07/31/2019

This specification covers a corrosion and heat resistant steel in the form of seamless tubing

AMS F Corrosion and Heat Resistant Alloys Committee

Sealing Compound, Polythioether Nonchromated, Corrosion Inhibiting for Intermittent Use to 360°F (182°C

AMS3259B (Current)07/25/2005

This specification covers a polythioether sealing compound with nonchromated corrosion inhibitors supplied as a two-component system which cures at room temperature. The compound has been used typically for faying surface sealing and for wet-installation of fasteners in aircraft structural joints, but usage is not limited to such applications. This compound is also suitable for fillet sealing and overcoating fasteners in nonfuel areas. The sealing compounds are usable from -65 to +320 degrees F (-54 to +160 degrees C) with short term (six hour) exposures up to 36 degrees F (182 degrees C

AMS G9 Aerospace Sealing Committee

Electroless Nickel Plating Low Phosphorus

AMS2405E (Current)10/16/2013

This specification covers the engineering requirements for electroless deposition of low-phosphorus nickel on various materials and the properties of the deposit

AMS B Finishes Processes and Fluids Committee

Paint System, Fluorescent, Removable, for Aircraft Application

AMSP21600B (Current)

10/28/2019

This specification establishes the requirements for a high visibility, durable, exterior fluorescent coating system consisting of a pigmented fluorescent coating with a clear protective overcoat containing a weathering stabilizer. This coating system is capable of being removed without softening the permanent undercoats

AMS G8 Aerospace Organic Coatings Committee

Sealing Compound, Low Adhesion, Corrosion Inhibiting, 200 to 600 Poises (20 to 60 Pa⋅s), 2 Hour Application Time (A-2

AMS3267/3B (Current)02/18/2011

This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system. This product has been used typically for sealing aircraft access doors and accessories where gaskets are required, but usage is not limited to such applications. Compound is classified as an A-2 sealing compound; the compound being suitable for brush application with a minimum of two hours application time after mixing

AMS G9 Aerospace Sealing Committee

COMPOUND, SILICONE RUBBER REMOVER Aircraft Turbine Engine Components Room Temperature Application

AMS1386 (Current)

08/10/2011

This specification covers a silicone-rubber-remover compound in liquid form supplied as a ready-to-use product

AMS J Aircraft Maintenance Chemicals and Materials Committee

Titanium Alloy, Welding Wire 8Al - 1Mo - 1V

AMS4955J (Current)

04/02/2020

This specification covers a titanium alloy in the form of welding wire

AMS G Titanium and Refractory Metals Committee

Titanium Alloy Welding Wire 6Al - 4V, Extra Low Interstitial Environment Controlled Packaging

AMS4956H (Current)

04/02/2020

This specification covers a titanium alloy in the form of wire for welding filler metal

AMS G Titanium and Refractory Metals Committee

Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0(Cb+Ta) - 0.15N - 32Fe Solution Heat Treated

AMS5769G (Current)04/02/2020

This specification covers a corrosion and heat-resistant alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading

AMS F Corrosion and Heat Resistant Alloys Committee

Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Extra Low Interstitial Annealed

AMS6932C (Current)

08/06/2018

This specification covers a titanium alloy in the form of bars up through 3.000 inches (76.20 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 3.000 inches (76.20 mm), inclusive, with bars and forgings having a maximum cross-sectional area of 16 in2 (103.23 cm2), and stock for forging of any size

AMS G Titanium and Refractory Metals Committee

Peening Media Hardened Steel Peening Balls

AMS2431/5B (Current)02/25/2018

The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS2431

AMS B Finishes Processes and Fluids Committee

Aluminum Alloy 6063, Bar, Rod, Shapes, Tube, and Wire, Extruded

AMSQQA200/9A (Current)08/24/2007

AMS D Nonferrous Alloys Committee

Aluminum 7075, Plate and Sheet, Alclad 7011

AMSQQA250/26B (Current)06/18/2007

This specification covers the specific requirements for aluminum alloy, 7011 alclad, 7075 plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy 7075 core with thin layers of a 7011 aluminum alloy anodic to the core and of approximately equal thickness, bonded to both surfaces

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Bar, Rod, and Wire, Rolled, Drawn, or Cold Finished, 2011

AMSQQA225/3A (Current)06/18/2007

This specification covers the specific requirements for aluminum alloy 2011 bar, rod, and wire produced by rolling, drawing, or cold finishing

AMS D Nonferrous Alloys Committee

Aluminum Alloy 3003, Plate and Sheet

AMSQQA250/2A (Current)04/13/2007

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Structural Shapes, Extruded, 6061

AMSQQA200/16A (Current)06/27/2007

AMS D Nonferrous Alloys Committee

Steel, Corrosion and Heat Resistant, Investment Castings 13Cr - 2.0Ni - 3.0W Hardened and Tempered to 32 - 38 HRC

AMS5354G (Current)

11/03/2023

This specification covers a corrosion and moderate heat resistant steel in the form of investment castings

AMS F Corrosion and Heat Resistant Alloys Committee

Peening of Metals

AMSP81985A (Current)12/15/2004

This specification covers procedures and requirements for dry peening the surfaces of metals by impingement of metallic shot or glass beads for the purpose of increasing the fatigue strength and resistance to stress corrosion cracking by inducing residual compressive stresses in specified surfaces

AMS B Finishes Processes and Fluids Committee

Rotary Flap Peening of Metal Parts

AMSR81841A (Current)12/15/2004

This specification covers procedures and requirements for peening of metal parts with portable bonded-shot rotary flap wheels (see 6.1

AMS B Finishes Processes and Fluids Committee

Steel, Corrosion and Heat-Resistant, Investment Castings 19.5Cr - 10.5Ni - 0.65Cb (Nb) (CF-8C) Solution Heat Treated

AMS5364D (Current)

11/03/2023

This specification covers a corrosion and heat-resistant steel in the form of investment castings

AMS F Corrosion and Heat Resistant Alloys Committee

Primer, Anodic Electrodeposition for Aircraft Applications

AMS3144A (Current)

10/17/2019

This specification establishes the requirements for a waterborne, corrosion inhibiting, chemical and solvent resistant, anodic electrodeposition epoxy primer capable of curing at 200 to 210 °F (93 to 99 °C

AMS G8 Aerospace Organic Coatings Committee