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EN 3818:2004

EN 3818:2004

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification

Superseded date

05-15-2019

Published date

11-10-2004

Publisher

Comite Europeen de Normalisation

Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Quality assurance
  4.1 Qualification
  4.2 Acceptance
5 Requirements

This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in TI-P64001.Strength class: 1 100 MPaIt is applicable whenever referenced.

Committee
ASD-STAN
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Superseded
SupersededBy

Standards Relationship
DIN EN 3818:2018-12 (Draft) Identical
SN EN 3818:2005 Identical
UNE-EN 3818:2004 Identical
I.S. EN 3818:2019 Identical
NF EN 3818 : 2005 Identical
I.S. EN 3818:2005 Identical
DIN EN 3818:2005-09 Identical
UNI EN 3818:2019 Identical
BS EN 3818:2019 Identical
NEN EN 3818 : 2006 Identical
ONORM EN 3818 : 2006 Identical
NS EN 3818 : 2ED 2005 Identical
PN EN 3818 : 2006 Identical
SN EN 3818 : 2003 Identical
UNI EN 3818 : 2006 Identical
BS EN 3818:2004 Identical
NBN EN 3818 : 2005 Identical
NEN-EN 3818:2019 Identical

PREN 3724 : 200P1 AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, MOS[2] COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)
BS EN 3725:2004 Aerospace series. Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature)
I.S. EN 3725:2005 AEROSPACE SERIES - SCREWS, PAN HEAD, SIX LOBE RECESS, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, ANODIZED, MOS[2] COATED - STRENGTH CLASS: 1100 MPA (AT AMBIENT TEMPERATURE)
I.S. EN 4322:2005 AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD WITH LOCKWIRE HOLES, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, ANODIZED, MOS[2] COATED - STRENGTH CLASS: 1100 MPA (AT AMBIENT TEMPERATURE)
I.S. EN 3907:2005 AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, MOS[2] COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/350 DEGREE C
I.S. EN 4323:2005 AEROSPACE SERIES - SCREWS, 100 DEGREE COUNTERSUNK HEAD, SIX LOBE RECESS, THREADED TO HEAD, IN TITANIUM ALLOY TI-P64001, ANODIZED, MOS[2] COATED - CLASSIFICATION: 900 MPA (AT AMBIENT TEMPERATURE)/350 DEGREE C
BS EN 3724:2004 Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS<sub>2</sub> coated. Strength class: 1100 MPa (at ambient temperature)
I.S. EN 3724:2005 AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P64001, MOS[2] COATED - STRENGTH CLASS: 1100 MPA (AT AMBIENT TEMPERATURE)
BS EN 3907:2004 Aerospace series. Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS<sub>2</sub> coated. Classification: 1100MPa (at ambient temperature)/350°C
EN 3725:2004 Aerospace series - Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1 100 MPa (at ambient temperature)
EN 3907:2004 Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1 100 MPa (at ambient temperature) / 350 °C
EN 4323:2004 Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature) / 350 °C
EN 3724:2004 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Strength Class: 1 100 MPa (at ambient temperature)
BS EN 4323:2004 Aerospace series. Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS<sub>2</sub> coated. Classification. 900 MPa (at ambient temperature) / 350°C

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 3452:1984 Non-destructive testing — Penetrant inspection — General principles
ISO 7961:1994 Aerospace Bolts Test methods
PREN 9133 : 200P1 AEROSPACE SERIES - QUALITY MANAGEMENT SYSTEMS - QUALIFICATION PROCEDURE FOR AEROSPACE STANDARD PRODUCTS

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