BSI BS 2S 119:1964

Current Revision
Specification for aircraft material. 1½ per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2½ in)

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BSI BS 2S 119:1964

Specification for aircraft material. 1½ per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2½ in)

PUBLISH DATE 1964
BSI BS 2S 119:1964

SPECIFICATION FOR AIRCRAFT MAT

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