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PREN 3724 : 200P1

Withdrawn

Withdrawn

View Superseded by

AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, MOS[2] COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)

Available format(s)

Hardcopy , PDF

Language(s)

English

Withdrawn date

12-14-2023

Superseded by

EN 3724:2004

US$74.41
Excluding Tax where applicable

1 Scope and field of application
2 References
3 Required characteristics
4 Designation
5 Marking
6 Technical specification

Specifies the characteristics of double hexagon headed bolts with relieved shank and long thread, in titanium alloy TI-P63, MoS[2] coated, for aerospace applications.

Committee
C8
DocumentType
Draft
Pages
7
ProductNote
Superseded by EN 3724:2004
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Withdrawn
SupersededBy

Standards Relationship
DIN EN 3724:2005-09 Identical

ISO 5855-2:1999 Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts
PREN 3813 : 200P2 AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AI-4V) - ANNEALED - BAR AND WIRE FOR FORGED FASTENERS - D[E] <= 50 MM
EN 2491:2011 Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
ISO 4095:1998 Aerospace — Bihexagonal drives — Wrenching configuration — Metric series
EN 3818:2004 Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
ISO 3353:1992 Aerospace — Rolled threads for bolts — Lead and runout requirements
EN 2424:2008 Aerospace series - Marking of aerospace products
PREN 3457 : 200P1 AEROSPACE SERIES - TITANIUM ALLOY TI-P63 NOT HEAT TREATED REFERENCE HEAT TREATMENT - SOLUTION TREATED AND AGED GRADE 2 FORGING STOCK FOR FASTENERS D &lt;= 25 MM

US$74.41
Excluding Tax where applicable