Material Specifications - SAE Mobilus

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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
Material Specification
Steel Bars, Forgings, Tubing, and Forging Stock, 1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C), Electroslag Remelted or Consumable Electrode Vacuum Remelted, Premium Aircraft QualityAMS6493C (Current)12/18/2024
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
Material Specification
Aluminum Alloy, Alclad Sheet, 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (Alclad 7050-T76), Solution Heat Treated and OveragedAMS4243D (Current)12/18/2024
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.187 inch (1.02 to 4.75 mm), inclusive, in nominal thickness (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
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
Material Specification
Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740), Heat Treated, 105 ksi (724 MPa) Tensile StrengthAMS6325M (Current)12/18/2024
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings
AMS E Carbon and Low Alloy Steels Committee
Material Specification
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
Material Specification
Iron-Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate, 44Fe - 18.5Cr - 35Ni - 1.15Si (Alloy 330), Solution Heat TreatedAMS5592H (Current)12/18/2024
This specification covers a corrosion- and heat-resistant iron-nickel alloy in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Molybdenum Disulfide Coating, Thin Lubricating Film, Impingement AppliedAMS2526E (Current)12/18/2024
This specification covers requirements for a coating consisting of finely powdered molybdenum disulfide in a heat resistant inorganic binder applied to parts
AMS B Finishes Processes and Fluids Committee
Material Specification
Automated Gaseous Nitriding Controlled by Nitriding PotentialAMS2759/10D (Current)12/18/2024
This document specifies the procedure and requirements for nitriding steel parts in a process automatically controlled by the nitriding potential (see 2.3.6
AMS B Finishes Processes and Fluids Committee
Material Specification
Steel, Sheet and Strip, 0.25 Carbon, Maximum (SAE 1020), Hard TemperAMS5045L (Current)12/18/2024
This specification covers a carbon steel in the form of sheet and strip
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Coating, Plasma Spray DepositionAMS2437E (Historical)12/18/2024
This specification covers the engineering requirements for applying coatings to parts by the plasma spray process and the properties of such coatings
AMS B Finishes Processes and Fluids Committee
Material Specification
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, Plate and Foil, 48Ni - 20Cr - 20Co - 5.9Mo - 2.2Ti - 0.45Al (Alloy 263), Consumable Electrode Remelted or Vacuum Induction Melted, Solution Heat TreatedAMS5872G (Historical)12/18/2024
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 19Cr - 9.5Ni (304L), Solution Heat TreatedAMS5511L (Current)12/12/2024
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Beryllium Bars, Rods, Tubing, and Shapes, High Ductility GradeAMS7904F (Current)12/10/2024
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot pressed powder
AMS G Titanium and Refractory Metals Committee
Material Specification
Aluminum Alloy, Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn; (2024-T81 Sheet, -T851 Plate), Solution Heat Treated, Cold Worked and Artificially AgedAMS4268B (Current)12/10/2024
This specification covers an aluminum alloy in the form of sheet and plate 0.010 to 1.500 inches (0.254 to 38.07 mm), inclusive, in thickness, supplied in the -T81/-T851 temper (see 8.5
AMS D Nonferrous Alloys Committee
Material Specification
Beryllium Near-Net Preforms, Standard Grade, Cold Isostatic Pressed, SinteredAMS7910E (Current)12/10/2024
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from impact-ground beryllium powder consolidated by cold isostatic pressing (CIP) and sintering
AMS G Titanium and Refractory Metals Committee
Material Specification
Aluminum Alloy, Plate (7065-T7451), 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr, Solution Heat Treated, Stress-Relieved, and OveragedAMS4361B (Current)12/10/2024
This specification covers an aluminum alloy in the form of plate
AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Plate (7065-T7651), 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr, Solution Heat Treated, Stress-Relieved, and OveragedAMS4351B (Current)12/10/2024
This specification covers an aluminum alloy in the form of plate
AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Extruded Profiles (2043-T85), 2.8Cu - 1.65Li - 0.35Mg - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching, and AgedAMS4450A (Current)12/10/2024
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) produced with thicknesses 0.040 to 2.500 inches (1.02 to 38.10 mm), inclusive, having a maximum cross-sectional area of 23 square inches (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 16 inches (406 mm) (see 2.4.1 and 8.7
AMS D Nonferrous Alloys Committee
Material Specification
Steel, Sheet, Strip, and Plate, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft Quality, Normalized or Otherwise Heat TreatedAMS6345F (Current)12/10/2024
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate up to and including 1.500 inches (38.10 mm) in thickness
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum-Beryllium Alloy, Sheet and Plate, 38Al - 62BeAMS7913E (Current)12/10/2024
This specification covers an aluminum-beryllium alloy in the form of sheet and plate consolidated from powder by extrusion and then rolled (see 8.5
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Sheet, Strip, and Plate, 6Al - 4V, Solution Heat TreatedAMS4903E (Current)12/10/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 2.000 inches (50.80 mm), inclusive (see 8.6
AMS G Titanium and Refractory Metals Committee
Material Specification
Aluminum Alloy, Extrusions, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73, 7075-T73511, 7075-T73510), Solution Heat Treated, Stress Relieved by Stretching when required, and OveragedAMS4617B (Current)12/10/2024
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing 0.040 to 4.499 inches (1.01 to 114.27 mm), inclusive, in nominal diameter or least thickness and with areas up to 32 square inches (206 cm2), inclusive (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes, 4Al - 2.5V -1.5 Fe, AnnealedAMS6948C (Current)12/10/2024
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, drawn shapes 5.000 inches (127.00 mm) and under, and stock for forging or flash-welded rings of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Bars, Wire, Forgings, Rings, and Drawn Shapes, 4Al - 2.5V -1.5 Fe, Annealed, Heat TreatableAMS6947C (Current)12/10/2024
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, and drawn shapes 4.000 inches (101.60 mm) and under and stock for forging, heading, or flash-welded rings of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
Material Specification
Beryllium Bars, Rods, Tubing, and Shapes, Instrument GradeAMS7907E (Current)12/10/2024
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot pressed powder
AMS G Titanium and Refractory Metals Committee
Material Specification
Chemical Check Analysis Limits, Titanium and Titanium AlloysAMS2249K (Current)12/10/2024
This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer
AMS G Titanium and Refractory Metals Committee
Material Specification
Tolerances, Low-Alloy Steel BarsAMS2251K (Current)12/10/2024
This specification covers established manufacturing tolerances applicable to low-alloy steel bars ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term “exclusive” is used to apply only to the higher figure of the specified range
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7451), Solution Heat Treated, Stress Relieved, and OveragedAMS4354B (Current)12/10/2024
This specification covers an aluminum alloy in the form of plate from 1.000 to 6.000 inches (25.40 to 152.40 mm) in thickness (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Flash-Welded Rings, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73), Solution and Precipitation Heat TreatedAMS4174F (Current)12/05/2024
This specification covers an aluminum alloy in the form of flash-welded rings 0.062 to 4.499 inches (1.57 to 114.27 mm), inclusive, in radial thickness with cross-sectional areas up to 32 square inches (206 cm2) (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C), Aircraft QualityAMS6492C (Current)12/05/2024
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
Material Specification
Plating, Silver, Nickel Strike, High BakeAMS2410M (Current)12/05/2024
This specification covers the requirements for electrodeposited silver on other metals, usually with a nickel strike between the basis metal and the silver
AMS B Finishes Processes and Fluids Committee
Material Specification
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings and Forging Stock 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted, 1800 °F (982 °C) Solution Heat Treated, Precipitation Hardenable (X750AMS5671J (Current)12/05/2024
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 (101.6 mm), exclusive, in least distance between parallel sides (thickness) or diameter, and stock of any size for forging or flash-welded rings
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Nickel Alloy, Corrosion- and Heat-Resistant, Welded Tubing, 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 2.9Ti - 1.4Al - 0.006B - 0.08Zr (Waspaloy), Consumable Electrode Remelted or Vacuum Induction Melted, AnnealedAMS5586J (Current)12/05/2024
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welded and drawn 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
Material Specification
Nickel - Copper Alloy, Corrosion-Resistant, Bars, Forgings and Forging Stock, 67Ni - 30Cu - 0.04S, Free MachiningAMS4674J (Current)12/05/2024
This specification covers a corrosion-resistant nickel-copper alloy in the form of bars up to 3.00 inches (76.2 mm), inclusive, in thickness and forgings and forging stock of any size
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Plating, Cadmium, Low Hydrogen Embrittlement ProcessAMS2401L (Current)12/05/2024
This specification covers the engineering requirements for cadmium deposited on ferrous and nonferrous metals using a low hydrogen embrittlement (LHE) electroplating process
AMS B Finishes Processes and Fluids Committee
Material Specification
Magnetic Particles, Fluorescent, Wet Method, Oil Vehicle, Aerosol PackagedAMS3046J (Current)12/05/2024
This specification covers one type of fluorescent magnetic particles in the form of a mixed, ready-to-use suspension in an odorless, inspection oil vehicle and packaged in aerosol cans
AMS K Non Destructive Methods and Processes Committee
Material Specification
Cold Spray Additive Manufacturing (CSAM) ProcessAMS7057 (Current)12/05/2024
This specification establishes process controls for the repeatable implementation of the CSAM process for the manufacturing of metallic and metal-nonmetal blend components
AMS AM Additive Manufacturing Metals
Material Specification
Performance Specification Anti-Seize Thread Compound, High Temperature – ‘Copper+Graphite+Aluminum’ OnlyAMS3050/7A (Current)12/04/2024
The foundation specification (AMS3050) and this category specification (AMS3050/7) cover anti-seize greases conforming to the requirements, but using the anti-seize ingredient Copper+Graphite+Aluminum only
AMS M Aerospace Greases Committee
Material Specification
Aluminum Alloy, Alclad Sheet and Plate, 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti, Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked, Alclad 2219-T351; Plate, Solution Heat Treated and Stress RelievedAMS4095F (Current)12/04/2024
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 0.499 inch (0.51 to 12.67 mm), inclusive, in nominal thickness alclad two sides (see 8.5
AMS D Nonferrous Alloys Committee
Material Specification
Magnesium Alloy, Extrusions, 4.0Y - 2.25Nd - 0.5Zr (WE43C - T5), Precipitation Heat TreatedAMS4485B (Current)12/04/2024
AMS D Nonferrous Alloys Committee
Material Specification
Performance Specification Anti-Seize Thread Compound, High Temperature – Molybdenum Disulphide; Graphite OnlyAMS3050/4A (Current)12/04/2024
The foundation specification (AMS3050) and this category specification (AMS3050/4) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Molybdenum Disulphide; Graphite only
AMS M Aerospace Greases Committee
Material Specification
Performance Specification Anti-Seize Thread Compound, High Temperature – Nickel OnlyAMS3050/3A (Current)12/04/2024
The foundation specification (AMS3050) and this category specification (AMS3050/3) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Nickel only
AMS M Aerospace Greases Committee
Material Specification
Elevated Temperature Tensile Properties of CastingsAMS2361F (Current)12/04/2024
This specification establishes a procedure for designating minimum elevated temperature tensile property requirements of castings by means of this AMS number and a series of dash numbers
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Performance Specification Anti-Seize Thread Compound, High Temperature - ‘Graphite+Calcium Fluoride’ OnlyAMS3050/9A (Historical)12/04/2024
The foundation specification (AMS3050) and this category specification (AMS3050/9) cover anti-seize greases conforming to the requirements, but using the anti-seize ingredient Graphite+Calcium Fluoride only
AMS M Aerospace Greases Committee
Material Specification
Room Temperature Tensile Properties of CastingsAMS2360F (Current)12/04/2024
This specification establishes a procedure for designating minimum room temperature tensile property requirements of castings by means of this AMS number and a series of dash numbers
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Performance Specification Anti-Seize Thread Compound, High Temperature – Aluminum OnlyAMS3050/2A (Current)12/04/2024
The foundation specification (AMS3050) and this category specification (AMS3050/2) cover anti-seize greases conforming to the requirements, but using the anti-seize ingredient Aluminum only
AMS M Aerospace Greases Committee
Material Specification
Aluminum Alloy, Extrusions, 4.4Cu - 1.5Mg - 0.60Mn (2024-T8510), Solution Heat Treated, Cold Worked, Stress-Relieved by Stretching, and Precipitation Heat Treated, UnstraightenedAMS4481A (Current)12/04/2024
AMS D Nonferrous Alloys Committee
Material Specification
Performance Specification Anti-Seize Thread Compound, High Temperature - PTFE OnlyAMS3050/5A (Current)12/04/2024
The foundation specification (AMS3050) and this category specification (AMS3050/5) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient PTFE only. For use only below 600 °F / 315 °C
AMS M Aerospace Greases Committee
Material Specification
Performance Specification Anti-Seize Thread Compound, High Temperature - ‘Nickel+Graphite’ OnlyAMS3050/6A (Current)12/04/2024
The foundation specification (AMS3050) and this category specification (AMS3050/6) cover anti-seize greases conforming to the requirements but using the anti-seize ingredient Nickel and Graphite only
AMS M Aerospace Greases Committee
Material Specification
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