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>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.10 Steels>BS EN 3532:2025 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa
immediate downloadReleased: 2025-09-17
BS EN 3532:2025 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa

BS EN 3532:2025

Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa

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Standard number:BS EN 3532:2025
Pages:12
Released:2025-09-17
ISBN:978 0 539 32127 2
Status:Standard
DESCRIPTION

BS EN 3532:2025


This standard BS EN 3532:2025 Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Plates. 6 mm < a ≤ 40 mm. 1 750 MPa ≤ Rm ≤ 2 000 MPa is classified in these ICS categories:
  • 49.025.10 Steels
This document specifies the requirements relating to: Steel X2NiCoMo18-8-5 (1.6359) Vacuum induction melted and vacuum arc remelted Solution treated and precipitation treated Plates 6 mm < a ≤ 40 mm 1 750 MPa ≤ Rm ≤ 2 000 MPa for aerospace applications. W.nr: 1.6359 ASD-STAN designation: FE-PM2701
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