Aerospace - Bolts, with MJ threads, made of heat and corrosion resisting steel, strength class 1 100 MPa - Procurement specification
Edition 2024-04

Aerospace - MJ threads - Part 2: Limit dimensions for bolts and nuts (ISO 5855-2:1999); Text in German and English; Corrigendum 1
Edition 2020-01

Aerospace series - Bolts, with MJ threads, in titanium alloys, strength class 900 MPa and 1 100 MPa - Technical specification
Edition 2013-05

Aerospace series - Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286), MoS₂ coated - Classification: 1100 MPa (at ambient temperature)/425 °C - Technical specification; German and English version EN 3752:2004
Edition 2005-09

Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated - Classification: 1 550 MPa (at ambient temperature) / 650 °C - Technical specification; German and English version EN 3833:2019
Edition 2019-07

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

Aerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated or uncoated - Classification: 1210 MPa (at ambient temperature)/730 °C - Technical specification; German and English version EN 3005:2004
Edition 2005-09

Aircraft bolts and nuts - Nuts, hexagonal, plain, normal height, normal across flats, ISO M or ISO MJ threads, 4H tolerance class
Edition 2000-12-01

Aircraft bolts and nuts - Nuts, hexagonal, slotted/castellated, reduced height, ISO M or ISO MJ threads, 4H tolerance class
Edition 2000-12-01

Aircraft bolts and nuts - Nuts, hexagonal, slotted/castellated, normal height, ISO M or ISO MJ threads, 4H tolerance class
Edition 2000-12-01