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>UNE standards>UNE EN 4012:2025 - Aerospace series - Nut, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1 550 MPa (at ambient temperature)/425 °C (Endorsed by Asociación Española de Normalización in December of 2025.)
in stockReleased: 2025-12-01
UNE EN 4012:2025 - Aerospace series - Nut, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1 550 MPa (at ambient temperature)/425 °C (Endorsed by Asociación Española de Normalización in December of 2025.)

UNE EN 4012:2025

Aerospace series - Nut, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1 550 MPa (at ambient temperature)/425 °C (Endorsed by Asociación Española de Normalización in December of 2025.)

Material aeroespacial. Tuercas de cabeza bihexagonal, autofrenadas, en aleación a base de níquel resistente al calor NI-PH2601 (Inconel 718), revestimiento en MoS2. Clasificación: 1 550 MPa (a temperatura ambiente)/425 ºC (Ratificada por la Asociación Española de Normalización en diciembre de 2025.)

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Standard number:UNE EN 4012:2025
Pages:10
Released:2025-12-01
Status:Standard
DESCRIPTION

UNE EN 4012:2025

This document specifies the characteristics of self-locking bihexagonal nuts in NI-PH2601, MoS2 coated, for aerospace applications. Classification: 1 550 MPa1/ 425 °C2.