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BS EN 4710-07:2015

BS EN 4710-07:2015

Current

Current

The latest, up-to-date edition.

Aerospace series. Quick release fastening systems for non-structural applications Retaining grommet

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-10-2015

Publisher

British Standards Institution

European foreword
1 Scope
2 Normative references
3 Requirements
4 Designation
5 Marking
6 Technical specification

Defines the dimensions, mass and tolerances of the retaining grommet for use in fuselage interior equipment and non-structural or secondary structural area.

Committee
ACE/12
DevelopmentNote
Supersedes 11/30247482 DC. (10/2015)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current
Supersedes

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.

Standards Relationship
EN 4710-07 : 2015 Identical

EN 22768-2:1993 General tolerances - Part 2: Geometrical tolerances for features without individual tolerance indications (ISO 2768-2:1989)
EN 4710-02:2015 Aerospace series - Quick release fastening systems for non-structural applications - Part 02: Spring clamp stud combination
ISO 2768-2:1989 GENERAL TOLERANCES - PART 2: GEOMETRICAL TOLERANCES FOR FEATURES WITHOUT INDIVIDUAL TOLERANCE INDICATIONS
EN 4710-06 : 2015 AEROSPACE SERIES - QUICK RELEASE FASTENING SYSTEMS FOR NON-STRUCTURAL APPLICATIONS - PART 06: STUD - QUICK-RELEASE AND LOCKING
EN 22768-1:1993 General tolerances - Part 1: Tolerances for linear and angular dimensions without individual tolerance indications (ISO 2768-1:1989)
EN 2424:2008 Aerospace series - Marking of aerospace products
EN 4710-01:2015 Aerospace series - Quick release fastening systems for non-structural applications - Part 01: Technical specification

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