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 2L 504:1973

BS 2L 504:1973

Withdrawn Most Recent

Specification for sheet and strip of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6)

€165.00

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BS 2L 505:1973

BS 2L 505:1973

Withdrawn Most Recent

Specification for bars and extruded sections of magnesium-3% zinc-zirconium alloy (not exceeding 100 mm diameter or minor sectional dimension) (Zn 3.0, Zr 0.6)

€165.00

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BS 2L 508:1973

BS 2L 508:1973

Withdrawn Most Recent

Specification for bars and extruded sections of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (not exceeding 50 mm diameter or minor sectional dimension) (Zn 1.25, Zr 0.6)

€165.00

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BS 2L 509:1973

BS 2L 509:1973

Withdrawn Most Recent

Specification for tube of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6)

€165.00

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BS L 512:1973

BS L 512:1973

Withdrawn Most Recent

Specification for bars and extruded sections of magnesium-6% aluminium-zinc alloy (not exceeding 150 mm diameter or minor sectional dimension) (Al 6.0, Zn 1.0)

€165.00

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BS L 514:1973

BS L 514:1973

Withdrawn Most Recent

Specification for forging stock and forgings of magnesium-3% zinc-zirconium alloy (Zn 3.0, Zr 0.6)

€165.00

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BS L 515:1973

BS L 515:1973

Withdrawn Most Recent

Specification for sheet and strip of magnesium-1¼% zinc-zirconium alloy (suitable for welding by inert-gas shielded arc techniques) (Zn 1.25, Zr 0.6)

€165.00

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BS 5S 21:1964

BS 5S 21:1964

Withdrawn Most Recent

Specification for aircraft material. '20' carbon steel (suitable for welding) (25/35 tonf/sq in: maximum size 6 inches diameter or minor sectional dimension)

€81.00

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BS 3S 61:1964

BS 3S 61:1964

Withdrawn Most Recent

Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (35/45 tonf/sq in: limiting ruling section 6 in)

€165.00

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BS 3S 62:1964

BS 3S 62:1964

Withdrawn Most Recent

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

€95.00

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BS 3S 70:1964

BS 3S 70:1964

Withdrawn Most Recent

Specification for aircraft material. '55' carbon steel (normalized) (45/55 tonf/sq in: limiting ruling section 4 in)

€165.00

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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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