DIN 65160 PDF

Published Date: 02/01/2018

Aerospace series - Screws in material 1.4534 - Nominal tensile strength 1 220 MPa, 1 400 MPa and 1 550 MPa for temperatures up to 315 °C - Technical specifications

Published Date: 07/01/2017

Draft Document - Aerospace series - Screws in material 1.4534 - Nominal tensile strength 1220 MPa, 1400 MPa and 1550 MPa for temperatures up to 315 °C - Technical specifications

Published Date: 01/01/2013

Aerospace series - Screws in material 1.4534 - Nominal tensile strength 1550 MPa - Technical specifications

Published Date: 01/01/2011

Draft Document - Aerospace - Screws in material 1.4534 - Nominal tensile strength 1 550 MPa - Technical specifications

Published Date: 01/01/1989

Aerospace; studs with MJ thread, ring locked, steel; nominal tensile strength 900 MPa, for temperatures up to 235 °C

Published Date: 10/01/2009

Aerospace series - Bolts, normal bi-hexagonal head, stepped shank, long thread, in titanium alloy, anodized, MoS<(Index)2> lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C; German and English version EN 4137:2009

Published Date: 03/01/2006

Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS<(Index)2> coated - Strength class: 1100 MPa (at ambient temperature): German and English version EN 4322:2004

Published Date: 06/01/1995