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 EN 3114-004:2006

BS EN 3114-004:2006

Active Most Recent

Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products sheet for superplastic forming

€201.00

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BS EN 3114-003:2006

BS EN 3114-003:2006

Active Most Recent

Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products plate

€281.00

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BS EN 3114-002:2007

BS EN 3114-002:2007

Active Most Recent

Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products bars, sections, forging stock and forgings

€281.00

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BS EN 3114-001:2006

BS EN 3114-001:2006

Active Most Recent

Aerospace series. Test method. Microstructure of (a + ß) titanium alloy wrought products General requirements

€172.00

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BS EN 3339:2006

BS EN 3339:2006

Active Most Recent

Aerospace series. Aluminium alloy AL-P7010-T76. Die Forgings. a = 200 mm

€172.00

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BS EN 3476:2006

BS EN 3476:2006

Active Most Recent

Aerospace series. Steel FE-PL1501 (30CrMo12). Air melted. Softened. Forging stock. a or D = 300 mm

€172.00

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BS EN 3479:2007

BS EN 3479:2007

Withdrawn Most Recent

Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Plate - 6 mm < a = 20 mm - 1070 MPa = Rm = 1220 MPa

€172.00

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BS EN 3490:2007

BS EN 3490:2007

Superseded Historical

Aerospace series. Steel FE-PM3901 (X15CrNi17-3). Air melted. Hardened and tempered. Bar for machining. De = 200 mm. 900 MPa = Rm = 1100 MPa

€172.00

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BS EN 3491:2006

BS EN 3491:2006

Active Most Recent

Aerospace series. Steel FE-PM3901 (X15CrNi17-3). Air melted. Hardened and tempered. Forgings. De = 100 mm. 900 MPa = Rm = 1100 MPa

€172.00

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BS EN 3527:2007

BS EN 3527:2007

Superseded Historical

Aerospace series. Steel FE-PL1504 (33CrMoV12). Air melted. Softened. Forging stock. a or D = 300 mm

€172.00

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BS EN 3531:2007

BS EN 3531:2007

Superseded Historical

Aerospace series. Steel FE-PM2701 (X2NiCoMo18-8-5). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Sheet and strip. a = 6 mm. 1750 MPa = Rm = 2000 MPa

€172.00

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BS EN 3532:2007

BS EN 3532:2007

Superseded Historical

Aerospace series. Steel FE-PM2701 (X2NiCoMo18-8-5).Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated.Plate. 6 mm < a = 40 mm. 1750 MPa = Rm = 2000 MPa

€172.00

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BS EN 3671:2007

BS EN 3671:2007

Active Most Recent

Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb). Non heat treated. Forging stock. a or D = 250 mm

€172.00

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BS EN 3683:2007

BS EN 3683:2007

Active Most Recent

Aerospace series. Test methods. Titanium alloy wrought products. Determination of primary a content. Point count method and line intercept method

€172.00

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BS EN 3684:2007

BS EN 3684:2007

Active Most Recent

Aerospace series. Test methods. Titanium alloy wrought products. Determination of ß transus temperature. Metallographic method

€172.00

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