This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for parts requiring high strength up to 500 φF (260 φC), but usage is not limited to such applications. Material may be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.
SAE AMS4613-2011 Referenced Document
ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 2024-04-19 Update
ASTM E1409-08 Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Technique*， 2024-04-19 Update
ASTM E1447-09 Standard Test Method for Determination of Hydrogen in Titanium and Titanium Alloys by the Inert Gas Fusion Thermal Conductivity/Infrared Detection Method*， 2024-04-19 Update
ASTM E1941-10 Standard Test Method for Determination of Carbon in Refractory and Reactive Metals and Their Alloys by Combustion Analysis*， 2024-04-19 Update
ASTM E2371-04 Standard Test Method for Analysis of Titanium and Titanium Alloys by Atomic Emission Plasma Spectrometry *， 2024-04-19 Update
ASTM E8-04 Standard Test Methods for Tension Testing of Metallic Materials*， 2024-04-19 Update
ASTM E8M-04 Standard Test Methods for Tension Testing of Metallic Materials [Metric] *， 2024-04-19 Update
SAE AMS2355 TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)