BS 3S 79:1964

BS 3S 79:1964

Withdrawn Most Recent

Specification for aircraft material. '55' carbon steel (hardened and tempered) (55/65 tonf/sq in: limiting ruling section 1? in)

€165.00

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BS 2S 98:1964

BS 2S 98:1964

Superseded Historical

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

€165.00

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BS 2S 111:1964

BS 2S 111:1964

Withdrawn Most Recent

Specification for aircraft material. Nickel-chromium-tungsten valve steel

€95.00

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BS 2S 112:1964

BS 2S 112:1964

Withdrawn Most Recent

Specification for aircraft material. Semi-free cutting carbon steel, bright bars for machining (40-50 tonf/sq in: maximum size ½ inch diameter or minor sectional dimension) (primarily intended for the manufacture of nuts)

€95.00

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BS 2S 114:1964

BS 2S 114:1964

Withdrawn Most Recent

Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches)

€95.00

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BS 2S 116:1964

BS 2S 116:1964

Withdrawn Most Recent

Specification for aircraft material. '40' carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section ¾ inch) (primarily intended for the manufacture of machined bolts)

€95.00

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BS 2S 117:1964

BS 2S 117:1964

Withdrawn Most Recent

Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1? inch)

€165.00

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BS 2S 119:1964

BS 2S 119:1964

Withdrawn Most Recent

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

€95.00

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BS 2S 120:1964

BS 2S 120:1964

Withdrawn Most Recent

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

€165.00

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BS 2S 124:1964

BS 2S 124:1964

Withdrawn Most Recent

Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (free machining) (45/55 tonf/sq in: limiting ruling section 6 in)

€95.00

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BS S 125:1964

BS S 125:1964

Withdrawn Most Recent

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

€165.00

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BS S 126:1964

BS S 126:1964

Withdrawn Most Recent

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

€165.00

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BS S 127:1964

BS S 127:1964

Withdrawn Most Recent

Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

€165.00

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BS S 128:1964

BS S 128:1964

Withdrawn Most Recent

Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)

€165.00

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BS S 133:1965

BS S 133:1965

Withdrawn Most Recent

Specification for aircraft material. ¾ per cent nickel-chromium case-hardening steel

€95.00

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