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BS 2S 119 64th Edition, January 31, 1964
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Specification for aircraft material. 1 1/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2 1/2 in)
Includes all amendments and changes through Amendment 1, January 1968
Additional Comments: W/D NO S/S
Page Count:4
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