EN 3818:2004
Aerospace series - Bolts, MJ threads, in titanium alloy TIP64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification

Standard No.

EN 3818:2004

Release Date

2004

Published By

European Committee for Standardization (CEN)

Status

Be replaced 2019-05

Replace By

EN 3818:2019

Latest

EN 3818:2019

Replace

prEN 3818-2003

EN 3818:2004 Referenced Document

• EN 9133:2004 Aerospace series - Quality management systems - Qualification procedure for aerospace standard parts
• ISO 2859-1:1999 Sampling procedures for inspection by attributes - Part 1: Sampling schemes indexed by acceptance quality limit (AQL) for lot-by-lot inspection
• ISO 3452:1984 Non-destructive testing; Penetrant inspection; General principles
• ISO 4288:1996 Geometrical Product Specifications (GPS) - Surface texture: Profile method - Rules and procedures for the assessment of surface texture
• ISO 5855-2:1999 Aerospace - MJ threads - Part 2: Limit dimensions for bolts and nuts
• ISO 6892:1998 Metallic materials - Tensile testing at ambient temperature
• ISO 7961:1994 Aerospace; bolts; test methods

EN 3818:2004 history

• 2019 EN 3818:2019 Aerospace series - Bolts@ MJ threads@ in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
• 2004 EN 3818:2004 Aerospace series - Bolts, MJ threads, in titanium alloy TIP64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
• 2003 EN 3818:2003 Aerospace series - Bolts with MJ threads, in titanium alloy TI-P64001 - Classification: 1100 MPa (at ambient temperature) - Technical specification