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Cleaner for Exterior Aircraft Surfaces Thickened or Gel-Type, Water-Base

AMS J Aircraft Maintenance Chemicals and Materials Committee
  • Aerospace Material Specification
  • AMS1523B
  • Current
Published 2019-06-03 by SAE International in United States
This specification covers a thickened, water-base, type cleaner in the form of a gel.
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Magnesium Alloy, Direct Chill Strand Cast, 2.8Nd - 1.4Gd - 0.4Zn - 0.6Zr (EV31A - T6), Solution and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4431
  • Current
Published 2019-05-14 by SAE International in United States

This specification covers a magnesium alloy in the form of direct chill strand cast round material up to 9.0 inch diameter and rectangular material up to 10 inch by 27.5 inch cross-section (see 8.4) for the purpose of machine from solid applications (see 8.2.1).

 

Minimizing Stress-Corrosion Cracking in Wrought High-Strength Aluminum Alloy Products

AMS D Nonferrous Alloys Committee
  • Aerospace Standard
  • ARP823F
  • Current
Published 2019-04-17 by SAE International in United States
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.
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Inspection Material, Penetrant

AMS K Non Destructive Methods and Processes Committee
  • Aerospace Material Specification
  • AMS2644G
  • Current
Published 2019-04-08 by SAE International in United States
This specification establishes the classification, technical requirements, tests, and test procedures for the qualification, approval, and quality verification of all materials used in the liquid penetrant methods of inspection with the exception of those excluded in the application section.
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Notch Plasticity and Fatigue Modelling of AZ31B-H24 Magnesium Alloy Sheet

FCA US LLC-Umesh Dighrasker
University of Waterloo-Lin Feng Victor Qian, Ali A. Roostaei, Grzegorz Glinka, Hamid Jahed
Published 2019-04-02 by SAE International in United States
Vehicle weight reduction through the use of components made of magnesium alloys is an effective way to reduce carbon dioxide emission and improve fuel economy. In the design of these components, which are mostly under cyclic loading, notches are inevitably present. In this study, surface strain distribution and crack initiation sites in the notch region of AZ31B-H24 magnesium alloy notched specimens under uniaxial load are measured via digital image correlation. Predicted strains from finite element analysis using Abaqus and LS-DYNA material types 124 and 233 are then compared against the experimental measurements during quasi-static and cyclic loading. It is concluded that MAT_233, when calibrated using cyclic tensile and compressive stress-strain curves, is capable of predicting strain at the notch root. Finally, employing Smith-Watson-Topper model together with MAT_233 results, fatigue lives of the notched specimens are estimated and compared with experimental results.
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Aluminum Alloy, Extrusions 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T4511 or T4510) Solution Heat Treated and Stress Relieved by Stretching

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4172G
  • Current
Published 2019-03-26 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
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Aluminum Alloy, Extrusions 4.4Cu – 1.5Mg – 0.60Mn (2024-T81) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4491
  • Current
Published 2019-03-08 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross sectional area of 32 in2 (206 cm2) maximum.
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Aluminum Alloy, Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T8510) Solution Heat Treated, Cold Worked, Stress-Relieved by Stretching, and Precipitation Heat Treated, Unstraightened

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4481
  • Current
Published 2019-03-01 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross sectional area of 32 in2 (206 cm2) maximum.
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Aluminum Alloy, Extrusions 4.4Cu – 1.5Mg – 0.60Mn (2024-T3511) Solution Heat Treated, Cold Worked, Stress-Relieved by Stretching, and Straightened

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4165J
  • Current
Published 2019-02-18 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross sectional area of 32 in2 (206 cm2) maximum.
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Protective Treatments Magnesium Alloys

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2475H
  • Current
Published 2019-02-13 by SAE International in United States
This specification establishes the requirements for chromate conversion coatings on magnesium alloys.
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