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
WL 1.4930-1:2012-10

WL 1.4930-1:2012-10

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Aerospace series - Stainless heat resisting chromium-cobalt steel casting with approx. 0,14 C - 13 Cr - 10 Co - 0,7 Mo - Part 1: Precision casting

€34.30

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WL 1.4930-100:2012-10

WL 1.4930-100:2012-10

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Aerospace series - Stainless heat resisting chromium-cobalt steel casting with approx. 0,14 C - 13 Cr - 10 Co - 0,7 Mo - Part 100: Precision casting - Notes for design and production, cross reference

€24.39

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WL 1.7736-1:2012-10

WL 1.7736-1:2012-10

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Aerospace series - Weldable hardened and tempered chromium-molybdenum-vanadium steel, with approx. 0,15 C - 1,4 Cr - 0,9 Mo - 0,25 V - Part 1: Remelted with consumable electrode - Plate

€34.30

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WL 1.7736-2:2012-10

WL 1.7736-2:2012-10

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Aerospace series - Weldable hardened and tempered chromium-molybdenum-vanadium steel, with approx. 0,15 C - 1,4 Cr - 0,3 Mo - 0,25 V - Part 2: Remelted with consumable electrode - Bar and forging

€34.30

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WL 1.7736-100:2012-10

WL 1.7736-100:2012-10

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Aerospace series - Weldable hardened and tempered chromium-molybdenum-vanaduim steel with approx. 0,15 C - 1,4 Cr - 0,9 Mo - 0,25 V - Part 100: Consumable elektrode remelted - Plate, bar and forging - Design and production data, cross-referencing

€41.78

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WL 1.7744-1:2012-10

WL 1.7744-1:2012-10

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Aerospace series - Weldable hardened and tempered cast chromium-molybdenum-vanadium steel with approx. 0,15 C - 1,4 Cr - 0,9 Mo - 0,25 V - Part 1: Sand and precision casting

€34.30

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WL 1.7784-2:2012-10

WL 1.7784-2:2012-10

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Aerospace series - Ultrahigh-strength chromium-molydenum-vanadium steel with approx. 0,4 C - 5 Cr - 1,3 Mo - 0,5 V - Part 2: Bar and forging

€34.30

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WL 1.7784-3:2012-10

WL 1.7784-3:2012-10

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Aerospace series - Ultrahigh-strength chromium-molybdenum-vanadium steel with approx. 0,4 C - 5 Cr - 1,3 Mo - 0,5 V - Part 3: Bar and wire for cold-or-hot-formed bolts and nuts

€34.30

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WL 1.7784-100:2012-10

WL 1.7784-100:2012-10

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Aerospace series - Ultrahigh-strength chromium-molybdenum-vanadium steel with approx. 0,4 C - 5 Cr - 1,3 Mo - 0,5 V - Part 100: Sheet, plate, bar, forging, bar and wire for cold-or-hot-formed bolts and nuts, tubing, filler metal - Design and production data, cross-referencing

€34.30

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WL 1.8544-1:2012-10

WL 1.8544-1:2012-10

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Aerospace series - Nitriding chromium-aluminium-molybdenum steel with approx. 0,34 C - 1,1 Cr - 1 Al - 0,2 Mo - Part 1: Bar and forging

€34.30

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WL 1.8544-100:2012-10

WL 1.8544-100:2012-10

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Aerospace series -Nitriding chromium-aluminium-molybdenum steel with approx. 0,34 C - 1,1 Cr - 1 Al - 0,2 Mo - Part 100: Bar and forging - Design and production data, cross-referencing

€34.30

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WL 1.8564-1:2012-10

WL 1.8564-1:2012-10

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Aerospace series - Nitriding chromium-molybdenum steel with approx. 0,3 C - 3 Cr - 0,4 Mo - Part 1: Bar and forging

€34.30

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WL 1.8564-100:2012-10

WL 1.8564-100:2012-10

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Aerospace series - Nitriding chromium-molybdenum steel with approx. 0,3 C - 3 Cr - 0,4 Mo - Part 100: Bar and forging - Design and production data, cross-referencing

€34.30

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WL 1.3514-1:2012-10

WL 1.3514-1:2012-10

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Aerospace series - Chromium ball and roller bearing steel with approx 1 C - 1,5 Cr, consumable electrode remelted - Part 1: Bar, wire and forging

€34.30

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DIN EN 3456:2012-10

DIN EN 3456:2012-10

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Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled - a 6 mm; German and English version EN 3456:2012

€56.17

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