AMS QQA 200/3 2024
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DATA SHEET TYPICAL APPLICATIONS Aerospace Components Defence Components High Technology Applications Very Good Resistance to Atmospheric Attack Poor A high strength 3.8 to 4.9% Copper alloy in extruded bar and profile form. Solution heat-treated and controlled stretched to achieve the T3511 condition, produced to the American Standard. General Engineering Euronorm - EN 573 / 755 AECMA Euronorm - BS EN 2318, 2633 SURFACE TREATMENT STOCK RANGE Anodising Protective Bright Hard Colour Plating Very Good Fair Variable Good Fair (Dark Colours Only) Vitreous Enamelling Unsuitable Flat & Squares WELDABILITY Brazing & Soldering Oxygen Inert Gas Resistance, Spot, Beam Not Recommended Not Recommended Not Recommended Excellent CUT TO SIZE SAWN BLANKSPRODUCTION TOLERANCES Cut to Length + 1.0mm - NIL Manufacturing limits are as stated in the Tables 11.2 to 11.14 of U.S. Aluminium Standards & Data. For further assistance please contact our Sales Dept / Laboratory. Our resident team of qualified metallurgists and engineers will be pleased to assist further on any technical topic. Smiths Advanced Metals Stratton Business Park, London Road, Biggleswade, Bedfordshire SG18 8QB United Kingdom Tel: +44 (0) 1767 604 710 Fax: +44 (0)1767 315 340 Email: info@smithsadvanced.com Website: www.smithsadvanced.com All information in this data sheet is based on approximate testing and is stated to the best of our knowledge and belief. It is presented apart from contractual obligations and does not constitute any guarantee of properties or of processing or application possibilities in individual cases. Our warranties & liabilities are stated exclusively in our terms of trading. © Smiths Advanced Metals 2014