Inserts, thin wall, self-locking. Design standard

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-15-1998

Publisher

British Standards Institution

Defines the use and installation hole dimensions for EN standard, self-locking, thin wall inserts, for aerospace applications and provisions for component salvage.

Committee	ACE/12
DevelopmentNote	Supersedes 89/75828 DC. (08/2005)
DocumentType	Standard
Pages	16
PublisherName	British Standards Institution
Status	Current

Standards	Relationship
I.S. EN 3676:1998	Identical
NF EN 3676 : 1998	Identical
EN 3676:1998	Identical
NEN EN 3676 : 1998	Identical
NBN EN 3676 : 1998	Identical
UNI EN 3676 : 1998	Identical
UNE-EN 3676:1998	Identical
NS EN 3676 : 1ED 1998	Identical
DIN EN 3676:1998-02	Identical

ISO 5855-2:1999	Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
ISO 5855-1:1999	Aerospace MJ threads Part 1: General requirements
EN 3916:2008	Aerospace series - Insert, thin wall - Salvage procedure for components
EN 3236 : 1998	AEROSPACE SERIES - INSERTS, THIN WALL, SELF-LOCKING, SHORT, IN HEAT RESISTING NICKEL BASE ALLOY NI-P100HT (INCONEL 718), SILVER PLATED INTERNAL THREAD
EN 3237 : 1998	AEROSPACE SERIES - INSERTS, THIN WALL, SELF-LOCKING, LONG, IN HEAT RESISTING NICKEL BASE ALLOY NI-P100HT (INCONEL 718), SILVER PLATED INTERNAL THREAD
EN 3298:2008	Aerospace series - Inserts, thin wall, self-locking - Installation and removal procedure