BS HR 506:1989

BS HR 506:1989

Superseded Historical

Nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy wire: softened (nickel base, Cr 19.5, Co 18, Ti 2.5, Al 1.5)

€165.00

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BS HR 208:1989

BS HR 208:1989

Superseded Historical

Specification for nickel-chromium-iron alloy sheet, strip and plate: annealed (Nickel base, Cr 15.5, Fe 8)

€165.00

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BS HR 205:1989

BS HR 205:1989

Superseded Historical

Nickel-copper alloy sheet and strip: annealed (Nickel base, Cu 31)

€165.00

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BS HR 209:1989

BS HR 209:1989

Superseded Historical

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

€165.00

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SAE AMS 5851D:2001-05-01

SAE AMS 5851D:2001-05-01

Withdrawn Most Recent

Nickel Alloy, Corrosion and Heat Resistant, Powder 55Ni 15Cr 17Co 5.0Mo 3.5Ti 4.0Al 0.025B, As Fabricated

€67.00

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SAE AMS 5851D:1989-07-01

SAE AMS 5851D:1989-07-01

Superseded Historical

Nickel Alloy, Corrosion and Heat Resistant, Powder 55ni 15cr 17co 5.0mo 3.5ti 4.0al 0.025b, as Fabricated

€77.00

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SAE AMS 2203K:1989-01-01

SAE AMS 2203K:1989-01-01

Withdrawn Most Recent

Tolerances, Aluminum Alloy Drawn Tubing

€68.00

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WL 5.5961:1988-12

WL 5.5961:1988-12

Withdrawn Most Recent

Aerospace; sealing compounds, two-component, polysulphide-polymer base, suitable for brush application, for temperatures from - 55 to 95 °C, corrosion inhibiting

€33.27

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WL 5.5963:1988-12

WL 5.5963:1988-12

Withdrawn Most Recent

Aerospace; sealing compounds, two-components, polysulphide polymer base, suitable for blow gun, spatula or roll application, for temperatures from - 55 to 95 °C, corrosion inhibiting

€40.56

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DIN EN 3219:1988-10

DIN EN 3219:1988-10

Superseded Historical

Aerospace series; heat resisting nickel base alloy (Ni-P100 HT); cold worked and softened; bar and wire for continuous forging or extrusion for fasteners 3 D 30 mm

€34.30

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DIN EN 3220:1988-10

DIN EN 3220:1988-10

Superseded Historical

Aerospace series; heat resisting nickel base alloy (Ni-P101 HT); cold worked and softened; bar and wire for continuous forging or extrusion for fasteners 3 D 30 mm

€34.30

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DIN EN 2959:1988-10

DIN EN 2959:1988-10

Superseded Historical

Aerospace series; heat resisting nickel base alloy (Ni-P101 HT); solution treated and cold worked; bar for hot upset forging for fasteners 3 D 30 mm

€34.30

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DIN EN 2960:1988-10

DIN EN 2960:1988-10

Withdrawn Most Recent

Aerospace series; heat resisting nickel base alloy (Ni-P101 HT); cold worked and solution treated; bar for machining for fasteners 3 D 50 mm

€34.30

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ASTM F1111-88(1998) (R2002)

ASTM F1111-88(1998) (R2002)

Superseded Historical

Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals

This product is not for sale, please contact us for more information

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SAE AMS 7223A:1987-07-01

SAE AMS 7223A:1987-07-01

Withdrawn Most Recent

Rivets, Aluminum Alloy, 4.5cu 1.5mg 0.6mn

€68.00

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