BSI BS S 125:1964

Current Revision
Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

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BSI BS S 125:1964

Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

PUBLISH DATE 1964
BSI BS S 125:1964

SPECIFICATION FOR AIRCRAFT MAT

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