DIN 65265:1998 Aerospace - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 °C
This document contains specifications pertinent to manufacture and use such as dimensions and designation, material, surface treatment, marking and technical specifications.#,,#
DIN 65265:1998 history
2020DIN 65265:2020-03 Aerospace series - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1 100 MPa, for temperatures up to 315 °C; Text in German and English
2020DIN 65265:2020 Aerospace series - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1 100 MPa, for temperatures up to 315 °C; Text in German and English
1970DIN 65265 E:2019-03 Aerospace series - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1 100 MPa, for temperatures up to 315 °C
2019DIN 65265 E:2019 Draft Document - Aerospace series - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 °C; Text in German and English
1998DIN 65265:1998 Aerospace - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 °C