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BSI BS 2S 120:1964

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 2½ in)
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BSI BS 2S 120:1964

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 2½ in)

PUBLISH DATE 1964
BSI BS 2S 120:1964

SPECIFICATION FOR AIRCRAFT MAT

SDO BSI: British Standards Institution
Document Number 2S 120
Publication Date Jan. 31, 1964
Language en - English
Page Count
Revision Level
Supercedes
Committee ACE/61/-/15
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