49.025 : Materials for aerospace construction

49.025.01

Materials for aerospace construction in general

49.025.05

Ferrous alloys in general

49.025.10

Steels

49.025.15

Non-ferrous alloys in general

49.025.20

Aluminium

49.025.30

Titanium

49.025.40

Rubber and plastics

49.025.50

Adhesives

49.025.60

Textiles

49.025.99

Other materials
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Withdrawn Most Recent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Withdrawn Most Recent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Withdrawn Most Recent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Withdrawn Most Recent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Withdrawn Most Recent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Withdrawn Most Recent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Withdrawn Most Recent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Withdrawn Most Recent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Withdrawn Most Recent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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BS S 138:1967

BS S 138:1967

Withdrawn Most Recent

Specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum remelted - air hardening) (157 kgf/mm2 (100 tonf/in2): limiting ruling section 30 mm (1? in))

€165.00

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BS S 139:1968

BS S 139:1968

Withdrawn Most Recent

Specification for 1½ per cent nickel-chromium-molybdenum steel (110/130 kgf/mm2 (70/83 tonf/in2): limiting ruling section 70 mm (2¾ in))

€95.00

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BS S 141:1968

BS S 141:1968

Withdrawn Most Recent

Specification for 12 per cent chromium corrosion-resisting steel (60/80 kgf/mm2 (38/51 tonf/in2): limiting ruling section 150 mm (6in))

€165.00

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BS 2S 144:1976

BS 2S 144:1976

Superseded Historical

Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (1130-1330 MPa)

€165.00

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