CTN ACE : Aerospace

BS 2HR 209:2011

BS 2HR 209:2011

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Specification for nickel-chromium-cobalt-molybdenum- titanium-aluminium heat-resisting alloy plate, sheet and strip (Nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)

€165.00

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BS 2HR 240:2011

BS 2HR 240:2011

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Specification for cobalt-chromium-tungsten-nickel-manganese heat-resisting alloy plate, sheet and strip (Cobalt base, Cr 20, W 15, Ni 10, Mn 1.5)

€165.00

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BS 3HR 401:2011

BS 3HR 401:2011

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Specification for nickel-chromium-titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Ti 2.2, Al 1.4)

€165.00

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BS 2HR 402:2011

BS 2HR 402:2011

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Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)

€165.00

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BS 2HR 403:2011 (R2016)

BS 2HR 403:2011 (R2016)

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Specification for nickel-chromium-titanium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Ti 0.4)

€165.00

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BS 2HR 404:2011 (R2016)

BS 2HR 404:2011 (R2016)

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Specification for nickel-cobalt-chromium-molybdenum- titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)

€165.00

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BS 3HR 501:2011 (R2016)

BS 3HR 501:2011 (R2016)

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Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)

€165.00

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BS 3HR 502:2011 (R2016)

BS 3HR 502:2011 (R2016)

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Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn and solution treated wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)

€165.00

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BS 3HR 503:2011

BS 3HR 503:2011

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Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy wire for thread inserts (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5) (0.45 mm to 2 mm diameter)

€165.00

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BS 3HR 504:2011

BS 3HR 504:2011

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Specification for nickel-chromium-titanium heat-resisting alloy bar and wire for rivets and rivets (Maximum diameter or minor sectional dimension 20 mm) (Nickel base, Cr 19.5, Ti 0.4)

€165.00

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BS EN 4658:2010

BS EN 4658:2010

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Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 1520 MPa

€165.00

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BS EN 4659:2010

BS EN 4659:2010

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Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 1650 MPa

€165.00

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BS EN 3197:2010

BS EN 3197:2010

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Aerospace series. Design and installation of aircraft electrical and optical interconnection systems

€404.00

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BS 2A 241:2005+A2:2011

BS 2A 241:2005+A2:2011

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General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greater. Specification

€316.00

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BS 2HR 650:2011 (R2016)

BS 2HR 650:2011 (R2016)

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Specification for high expansion heat-resisting steel bar and wire for the manufacture of bolts, studs, set screws and nuts (Ni 25.5, Cr 15, Ti 2, Mn 1.5, Mo 1.25, Si 0.7, V 0.3) (limiting ruling section 50 mm)

€165.00

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