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 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Superseded Historical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Superseded Historical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Withdrawn Most Recent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Superseded Historical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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DIN 65426-2:1989-06

DIN 65426-2:1989-06

Withdrawn Most Recent

Aerospace; aromatic polyamide (aramid); woven filament fabric prepreg from high-modulus filament yarn and epoxy resin; technical specification

€91.03

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L17-411 (05/1989)

L17-411 (05/1989)

Superseded Historical

Aerospace series. Unidirectional laminates carbon-thermosetting resin. Flexural test.

€47.00

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L17-412 (05/1989)

L17-412 (05/1989)

Superseded Historical

Aerospace series. Unidirectional laminates carbon-thermosetting resin. Test method. Determination of apparent interlaminar shear strength.

€47.00

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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Withdrawn Most Recent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Withdrawn Most Recent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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BS 4S 99:1976

BS 4S 99:1976

Superseded Historical

Specification for 2.5% nickel-chromium-molybdenum (high carbon) steel billets, bars, forgings and parts (1230-1420 MPa: limiting ruling section 150 mm)

€165.00

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NF L17-102 (11/1988)

NF L17-102 (11/1988)

Superseded Historical

Industrie aérospatiale - Élastomères - Marquage et repérage des produits

€28.00

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NF L17-162 (11/1988)

NF L17-162 (11/1988)

Superseded Historical

Industrie aérospatiale - Élastomères halogénocarbonés classe 62 - Caractéristiques.

€28.00

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NF L17-163 (11/1988)

NF L17-163 (11/1988)

Superseded Historical

Industrie aérospatiale - Élastomères fluorosilicones - Classe 63 - Caractéristiques.

€28.00

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NF L17-103 (11/1988)

NF L17-103 (11/1988)

Superseded Historical

Industrie aérospatiale - Élastomères - Produits non montés - Conditions d'emballage et de stockage.

€25.00

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