This European Standard specifies the dimensions, mass and tolerances of the retaining grommet for use in fuselage interior equipment and non- structural or secondary structural area. This European Standard is to be used in conjunction with EN 4710-06 as described in EN 4710-02. The applicable temperature range is -55 °C to 85 °C.
Tämän julkaisun valmistelusta Suomessa vastaa SFS Suomen Standardit, puh. 09 149 9331.
EN 22768-1:1993 General tolerances - Part 1: Tolerances for linear and angular dimensions without individual tolerance indications (ISO 2768-1:1989)
EN 22768-2:1993 General tolerances - Part 2: Geometrical tolerances for features without individual tolerance indications (ISO 2768-2:1989)
EN 2424:2008 Aerospace series - Marking of aerospace products
EN 22768-1:1993 General tolerances - Part 1: Tolerances for linear and angular dimensions without individual tolerance indications (ISO 2768-1:1989)
EN 22768-2:1993 General tolerances - Part 2: Geometrical tolerances for features without individual tolerance indications (ISO 2768-2:1989)
EN 2424:2008 Aerospace series - Marking of aerospace products
EN 4710-01:2018 Aerospace series - Quick release fastening systems for non-structural applications - Part 01: Technical specification
EN 4710-02:2015 Aerospace series - Quick release fastening systems for non-structural applications - Part 02: Spring clamp stud combination
EN 4710-06:2015 Aerospace series - Quick release fastening systems for non-structural applications - Part 06: Stud - quick-release and locking