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EN 3308 : 1996

Current

Current

The latest, up-to-date edition.

AEROSPACE SERIES - SCREWS, NORMAL HEXAGONAL HEAD, THREADED TO HEAD, IN TITANIUM ALLOY, ANODIZED, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREE C

Published date

21-08-1996

Foreword
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification

This standard specifies the characteristics of bolts, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS2 lubricated.

DevelopmentNote
Supersedes PREN 3308 (11/2003)
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Current
Supersedes

Standards Relationship
NF EN 3308 : 1997 Identical
NS EN 3308 : 1ED 1997 Identical
PN EN 3308 : 2001 Identical
UNI EN 3308 : 1997 Identical
NEN EN 3308 : 1996 Identical
BS EN 3308:1996 Identical
NBN EN 3308 : 1996 Identical
I.S. EN 3308:1997 Identical
SNV DIN EN 3308 : 1996 Identical
UNE-EN 3308:1997 Identical
DIN EN 3308:1996-09 Identical

ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
EN 2491:2011 Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
TR 4070 : 1 AEROSPACE SERIES - MOLYBDENUM DISULPHIDE COATINGS - LIST OF COMMERCIAL PRODUCTS
ISO 9152:1998 Aerospace Bolts, with MJ threads, in titanium alloys, strength class 1 100 MPa Procurement specification
ISO 3353:1992 Aerospace — Rolled threads for bolts — Lead and runout requirements
EN 2000:1991 Aerospace series - Quality assurance - EN aerospace products - Approval of the quality system of manufacturers
EN 2424:2008 Aerospace series - Marking of aerospace products
TR 3775 : 4 AEROSPACE SERIES - BOLTS AND PINS - MATERIALS
ISO 7913:1994 Aerospace Bolts and screws, metric Tolerances of form and position

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