Aerospace series - Unmanned Aircraft Systems (UAS) - Part 9: Requirements for Drone-Detection Systems
Edition 2025-04

Aerospace series - Fasteners in material 1.4534 - Nominal tensile strength 1250 MPa to 1550 MPa for temperatures up to 315 °C - Technical specification
Edition 2024-01

Aerospace series - Bolts, with MJ threads, in titanium alloys, strength class 900 MPa and 1 100 MPa - Technical specification
Edition 2023-10

Aircraft ground support equipment - General requirements - Part 2: Stability and strength requirements, calculations and test methods; German and English version prEN 1915-2:2025
Edition 2025-08

Aerospace series - Metallic materials - Test methods - Part 001: Tensile testing at ambient temperature; German version ASD-STAN prEN 2002-001:2025
Edition 2025-07

Aerospace series - Metallic materials - Test methods - Part 002: Tensile testing at elevated temperature; English version prEN 2002-002:2024
Edition 2024-11

Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys; German and English version prEN 2133:2025
Edition 2025-08

Aerospace series - Characteristics of aircraft electrical supplies; German and English version FprEN 2282:2022
Edition 2022-08

Aerospace series - Testing of aircraft wiring; German and English version prEN 2283:2025
Edition 2025-08

Aerospace series - Steel 31NiMoCr10-5-3 - 1230 MPa ≤ Rₘ ≤ 1420 MPa - Bars - Dₑ ≤ 40 mm; German version ASD-STAN prEN 2450:2025
Edition 2025-06