Browse Topic: Wrought alloys

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Nickel-Aluminum-Bronze, Martensitic, Sand, Centrifugal and Continuous Castings, 78Cu - 11Al - 5.1Ni - 4.8Fe, Quench Hardened and Temper AnnealedAMS4881E (Current)11/25/2025
This specification covers a nickel-aluminum bronze alloy in the form of sand, centrifugal or continuous castings.
AMS D Nonferrous Alloys Committee
Aluminum Bronze Alloy, Centrifugal and Continuous-Cast Castings, 81.5Cu - 10.3Al - 5.0Ni - 2.8Fe, Quench Hardened and Temper Annealed (TQ50)AMS4880E (Current)11/25/2025
This specification covers an aluminum bronze alloy in the form of centrifugal and continuous-cast castings.
AMS D Nonferrous Alloys Committee
Aluminum Bronze, Centrifugal and Chill Castings 85Cu - 11Al - 3.6Fe As CastAMS4870G (Current)11/25/2025
This specification covers an aluminum bronze alloy in the form of centrifugal and chill castings.
AMS D Nonferrous Alloys Committee
Test Publishing DocumentARP090824B (Current)10/13/2025
Test Publishing Document6667
A-6 Aerospace Actuation, Control and Fluid Power Systems
test 03/01auto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testSAE-PP-078071/3/2023
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Mutagaana, Festo
abc test 30/12auto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testauto testSAE-PP-0780612/30/2022
Mutagaana, F., "QE Testing 11/2-10 jms edit," SAE MobilityRxiv™ Preprint, submitted November 2, 2022, https://doi.org/10.47953/SAE-PP-07790.
Mutagaana, Festo
Test Method and Limits for Bow Height of Aluminum Sheet Samples After Chemical MillingAS6507 (Current)11/2/2021
The results of this test are intended to be a useful indication of the resistance to distortion of bare or two-side Alclad, flat sheet aluminum used in chemical milling applications.
AMS D Nonferrous Alloys Committee
Disposition of Landing Gear Components Involved in Accidents/IncidentsARP4915B (Current)8/5/2021
This document establishes a procedure for disposition of landing gear components that have been involved in accidents/incidents. The recommendations in this document apply to components made of ferrous and non-ferrous alloys. The recommendations in this document do not apply to components made of non metallic composite materials.
A-5B Gears, Struts and Couplings Committee
Disposition of Landing Gear Components Involved in Accidents/IncidentsARP4915B-TEST-REC (Historical)8/5/2021
This document establishes a procedure for disposition of landing gear components that have been involved in accidents/incidents. The recommendations in this document apply to components made of ferrous and non-ferrous alloys. The recommendations in this document do not apply to components made of non metallic composite materials.
A-5B Gears, Struts and Couplings Committee
Inspection, Ultrasonic, Wrought Metals, Process forAMSSTD2154E (Current)7/15/2021
The purpose of this standard is to provide uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
AMS K Non Destructive Methods and Processes Committee
Inspection, Ultrasonic, Wrought Metals, Process forAMSSTD2154E-TEST-REC (Historical)7/15/2021
The purpose of this standard is to provide uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
AMS K Non Destructive Methods and Processes Committee
Aluminum Alloy Forgings and Rolled or Forged Rings and Forging Stock 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally AgedAMS4146H (Current)7/7/2021
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy Forgings and Rolled or Forged Rings and Forging Stock 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally AgedAMS4146H-TEST-REC (Historical)7/7/2021
This specification covers an aluminum alloy in the form of die forgings up to 4 inches (102 mm), hand forgings up to 8 inches (203 mm), rolled or forged rings up to 2.5 inches (63.5 mm) in thickness, and forging stock (see 8.6).
AMS D Nonferrous Alloys Committee
Fittings, 24 Degree Cone Flareless, Fluid Connection, 3000 psiAS18280H (Current)5/26/2021
This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fittings, 24 Degree Cone Flareless, Fluid Connection, 3000 psiAS18280H-TEST-REC (Historical)5/26/2021
This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fittings, 37 Degree Internal Flare, Fluid Connection, Procurement SpecificationAS4841D (Current)4/14/2021
This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose, and seal ring fittings in all types of aerospace fluid systems (see Section 6).
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Connector Accessories, Electrical General Specification forAS85049F (Current)4/14/2021
This specification covers connector accessories for use with electrical connectors; see 6.8.
AE-8C1 Connectors Committee
Connector Accessories, Electrical General Specification forAS85049F-TEST-REC (Historical)4/14/2021
This specification covers connector accessories for use with electrical connectors; see 6.8.
AE-8C1 Connectors Committee
Fittings, 37 Degree Internal Flare, Fluid Connection, Procurement SpecificationAS4841D-TEST-REC (Historical)4/14/2021
This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose, and seal ring fittings in all types of aerospace fluid systems (see Section 6).
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fittings, Straight Threaded Boss or Flanged, Fluid Connection, Procurement SpecificationAS4875B (Current)3/9/2021
This SAE Aerospace Standard (AS) establishes the requirements for straight threaded boss or flanged fluid connection fittings (see Section 6) for use in all types of fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fittings, Straight Threaded Boss or Flanged, Fluid Connection, Procurement SpecificationAS4875B-TEST-REC (Historical)3/9/2021
This SAE Aerospace Standard (AS) establishes the requirements for straight threaded boss or flanged fluid connection fittings (see Section 6) for use in all types of fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fittings and Bosses, Pipe Threaded, Fluid Connection, Procurement SpecificationAS4842B (Current)3/8/2021
This SAE Aerospace Standard (AS) establishes the requirements for pipe threaded fluid connection fittings (see Section 6) for use in all types of fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Fittings and Bosses, Pipe Threaded, Fluid Connection, Procurement SpecificationAS4842B-TEST-REC (Historical)3/8/2021
This SAE Aerospace Standard (AS) establishes the requirements for pipe threaded fluid connection fittings (see Section 6) for use in all types of fluid systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Editorial21AVEP01_011/1/2021
I vividly remember a high-level engineer for a global automaker telling me a couple of years ago that he was more than a little miffed when he saw the figures for what the company planned to invest in “self-driving technology” in the coming year. “Somebody needs to figure out what's reality and what's R&D,” he griped. I think that's becoming clearer. Almost by the day.
Visnic, Bill
Minimizing Stress-Corrosion Cracking in Wrought Titanium Alloy ProductsARP982D (Current)9/21/2020
Primarily to provide recommendations concerning minimizing stress-corrosion cracking in wrought titanium alloy products.
AMS G Titanium and Refractory Metals Committee
Heat Treatment of Wrought Aluminum Alloy PartsAMS2770R (Current)8/20/2020
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (see 8.6.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (see 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2195, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, and 7475.
AMS D Nonferrous Alloys Committee
Heat Treatment of Wrought Aluminum Alloy PartsAMS2770R-TEST-REC (Historical)8/20/2020
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (see 8.6.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (see 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2195, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, and 7475.
AMS D Nonferrous Alloys Committee
Metal Injection Molding Offers OEMs Edge and Safety with DisposablesTBMG-371176/1/2020
Medical instruments used in surgery today often require more elaborate features and added functionality than they did in the past, largely due to the growth in minimally invasive surgery. For this reason, greater attention to detail is critical in product design and development. To meet the demand for small, complex, lightweight surgical products, medical device original equipment manufacturers (OEMs) are increasingly opting for disposable surgical tools and product offerings, which provide flexible, off-the-shelf single-use sterile solutions to surgeons and hospitals.
Uphill Quenching of Aluminum Alloy ProductAMS2767A (Current)5/7/2020
This specification establishes engineering requirements for the uphill quenching process. Uphill quenching immerses product in liquid nitrogen followed by exposure to a high pressure/velocity steam blast or boiling water.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extruded Rod, Bar, and Profiles (7055-T76511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress-Relieved, and OveragedAMS4336B (Historical)4/28/2020
This specification covers an aluminum alloy procured in the form of extruded bars, rods, and profiles (shapes) with nominal thickness up to 3.000 inch (76.20 mm), inclusive, and having a cross-sectional area of 12 square inches (77 square centimeters) maximum and circle size of 10 inches (254 mm) maximum (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extruded Rod, Bar, and Profiles (7055-T76511) 8.0Zn - 2.3Cu - 2.0Mg - 0.16Zr Solution Heat Treated, Stress-Relieved, and OveragedAMS4336B-TEST-REC (Historical)4/28/2020
This specification covers an aluminum alloy procured in the form of extruded bars, rods, and profiles (shapes) with nominal thickness up to 3.000 inch (76.20 mm), inclusive, and having a cross-sectional area of 12 square inches (77 square centimeters) maximum and circle size of 10 inches (254 mm) maximum (see 8.6).
AMS D Nonferrous Alloys Committee
Innovative Additive Manufacturing Process for Successful Production of 7000 Series Aluminum Alloy Components Using Smart Optical Monitoring System2020-01-13004/14/2020
Aircraft components are commonly produced with 7000 series aluminum alloys (AA) due to its weight, strength, and fatigue properties. Auto Industry is also choosing more and more aluminum component for weight reduction. Current additive manufacturing (AM) methods fall short of successfully producing 7000 series AA due to the reflective nature of the material along with elements with low vaporization temperature. Moreover, lacking in ideal thermal control, print inherently defective products with such issues as poor surface finish alloying element loss and porosity. All these defects contribute to reduction of mechanical strength. By monitoring plasma with spectroscopic sensors, multiple information such as line intensity, standard deviation, plasma temperature or electron density, and by using different signal processing algorithm, AM defects have been detected and classified. For composition analysis, the ratio of the maximum intensities of Mg(I)/Al(I) shows a strong trend with the
Choi, Jay, Mazumder, Jyoti, Rice, Alex
Inspection, Ultrasonic, Wrought Metals, Process forAMSSTD2154D (Historical)4/3/2020
The purpose of this standard is to provide uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
AMS K Non Destructive Methods and Processes Committee
Inspection, Ultrasonic, Wrought Metals, Process forAMSSTD2154D-TEST-REC (Historical)4/3/2020
The purpose of this standard is to provide uniform methods for the ultrasonic inspection of wrought metals and wrought metal products.
AMS K Non Destructive Methods and Processes Committee
Fittings, 37 Degree Internal Flare, Fluid Connection, Procurement SpecificationAS4841C (Historical)3/10/2020
This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose, and seal ring fittings in all types of aerospace fluid systems (see Section 6).
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Titanium Alloy, Round Bar and Wire 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Cold DrawnAMS4957G (Current)1/14/2020
This specification covers a titanium alloy in the form of round bar and wire, 0.625 inch (15.88 mm) and under in nominal diameter or thickness.
AMS G Titanium and Refractory Metals Committee
Anodic Treatment of Aluminum Alloys Sulfuric Acid Process, Dyed CoatingsAMS2472H (Current)1/13/2020
This specification establishes the requirements for dyed anodic coatings on aluminum alloys.
AMS B Finishes Processes and Fluids Committee
Aluminum Alloy, Alclad Sheet 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-O) Annealed, Fine GrainAMS4274B (Current)12/17/2019
This specification covers an aluminum alloy in the form of sheet 0.009 to 0.126 inch (0.23 to 3.20 mm) inclusive, in nominal thickness, alclad.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extrusion 3.7Cu - 1.15Li - 0.5Zn - 0.45Ag - 0.4Mg - 0.3Mn - 0.1Zr (2055-T84) Solution Heat Treated, Stress Relieved by Stretching 2% to 5% and AgedAMS4257 (Current)11/12/2019
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles.
AMS D Nonferrous Alloys Committee
Investigation of Dry Sliding Wear Behavior of AA8011 Reinforced with Zirconium Oxide and Aluminium Oxide Hybrid Composites Processed through Multi-Direction Forging2019-28-005710/11/2019
The Cardinal goal of this research work is to fabricate hybrid composites of AA8011 with reinforcement particles of Zr2O3 and Al2O3 which was taken in equal (5wt%) weight percentage. The hybrid composites were cast in a square shape (50x50x50 mm size) under the optimal stir casted process parametric condition, further, it was taken for the forging process. The prepared specimens were induced for uni-direction (x), bi-direction (x and y) and multi-direction (x,y, and z) forging route and the response of microhardness of 53, 68, 81 and 96 VHN were obtained respectively due to microstructural phase changes with an even distribution of particles in the matrix. Thus, the tribological properties of prepared specimens were tested using pin-on-disc Tribometer at room temperature under dry sliding condition of load 5,10,15,20 N and by adjusting the sliding speed as 266 and 531 rpm respectively. The outcomes uncovered all the specimens that the wear rate increments with an increase in load and
Kuppuraj, Sathishkumar, Ranganathan, Soundararajan, Aruchamy, Sathishkumar, Gopal, Shanthosh
Aluminum Alloy, Extruded Profiles (2043-T85) 2.8Cu - 1.65Li - 0.35Mg - 0.1Zr Solution Heat Treated, Stress Relieved by Stretching, and AgedAMS4450 (Current)7/3/2019
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) produced with thickness between 0.040 and 2.500 inches (1.02 to 38.10 mm) in thickness, and having a maximum cross sectional area of 23 in2 (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 16 inches (406 mm) (see 8.4.1).
AMS D Nonferrous Alloys Committee
Minimizing Stress-Corrosion Cracking in Wrought High-Strength Aluminum Alloy ProductsARP823F (Current)4/17/2019
The purpose of this recommended practice is to provide the aerospace industry with recommendations concerning minimizing stress-corrosion cracking (SCC) in wrought high-strength aluminum alloy products.
AMS D Nonferrous Alloys Committee
Heat Treatment of Wrought Aluminum Alloy PartsAMS2770P (Historical)4/8/2019
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (see 8.6.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (see 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2014, 2017, 2024, 2098, 2117, 2124, 2195, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, 7475
AMS D Nonferrous Alloys Committee
Properties and Limitation of an Oxide Coated Aluminum Brake Rotor2018-01-187710/5/2018
The electrification of the powertrain and the thereto related recuperation of the electric engine saves the energy in the battery and thus reduces the thermally dissipated brake energy, which leads to lower brake rotor temperatures compared to combustion engine vehicles (ICEVs). These new conditions enable to reconsider brake disc concepts. Including lightweight design in heavy battery electric vehicles (BEVs) and the increasingly reliant corrosion resistance of brake rotors, Aluminum is a promising approach for new brake disc concepts. In the past, Aluminum brake disc concepts have already been deployed. For instance Aluminum Metal-Matrix Composite (Al-MMC) concepts in the Lotus Elise S1 and on the rear axle of the Volvo V40 [1]. The presented concept is a different approach and separates the friction system from the bulk Aluminum brake disc, achieved by coating of the friction rings. By locally reinforcing the friction rings, the good machinability and ductility of the base body is
Gulden, Florian, Gramstat, Sebastian, Stich, Anton, Hoppel, Heinz Werner, Tetzlaff, Ulrich
Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked (8%) and Naturally Aged (2219 -T37)AMS4600A (Historical)8/2/2018
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 5.000 inches (0.51 to 127.00 mm) in nominal thickness (see 8.5).
AMS D Nonferrous Alloys Committee
New High-Performance Materials Tailored Specifically For Additive Manufacturing ProcessesF-0074-2018-128145/14/2018
ABSTRACT Integrated Computational Materials Engineering (ICME) technologies have served an integral role in understanding, evaluating and designing material microstructures and heat treatments specifically tailored for the unique processing conditions of Additive Manufacturing (AM). Applying their Materials by Design® methodologies, QuesTek Innovations has expanded their ICME framework under US Army Small Business Innovation Research (SBIR) funding to adapt their high performance Ferrium® C64® gear steel to AM processes, demonstrating printability across multiple systems, achievement of AMS minimum tensile properties, and positive response to heat treatment. Under Office of Naval Research and US Navy SBIR funding, QuesTek has designed and is developing high performance, aluminum alloys that are both printable and demonstrate properties of wrought 6000 and 7000 series alloys. AM builds and testing to date have demonstrated crack-free printability, high strength and good corrosion
Grabowski, Jeff, Kozmel, Tom
Shim Stock, LaminatedAMSDTL22499B (Current)5/7/2018
This specification covers the requirements for surface bonded laminated shim stock.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by StretchingAMS4338B (Current)4/3/2018
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) with a maximum cross-sectional area of 25 in2 (161 cm2), a maximum circle size of 12 inches (305 mm) and a nominal thickness up to 3.250 inch (82.54 mm), inclusive.
AMS D Nonferrous Alloys Committee
Cobalt Alloy, Corrosion and Heat-Resistant, Strip 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Vacuum Induction Plus Consumable Electrode Remelted Solution Heat Treated and Cold RolledAMS5876E (Historical)3/23/2018
This specification covers a corrosion and heat-resistant cobalt alloy in the form of strip 0.100 inch (2.54 mm) and under in specified thickness and 4.000 inches (101.60 mm) and under in specified width (see 8.6).
AMS F Corrosion Heat Resistant Alloys Committee
Cobalt Alloy, Corrosion and Heat-Resistant, Strip 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Vacuum Induction Plus Consumable Electrode Remelted Solution Heat Treated and Cold RolledAMS5876E-TEST-REC (Historical)3/23/2018
This specification covers a corrosion and heat-resistant cobalt alloy in the form of strip 0.100 inch (2.54 mm) and under in specified thickness and 4.000 inches (101.60 mm) and under in specified width (see 8.6).
AMS F Corrosion Heat Resistant Alloys Committee
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