PREN 4322 : 200P1
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
View Superseded by
AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD WITH LOCKWIRE HOLES, RELIEVED SHANK, LONG THREAD, IN TITANIUM ALLOY TI-P63, ANODIZED, MOS[2] COATED - STRENGTH CLASS: 1100 MPA (AT AMBIENT TEMPERATURE)
Hardcopy , PDF
12-19-2023
English
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1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification
Gives the characteristics of double hexagon headed bolts with lockwire holes, relieved shank and long thread in TI-P63, anodized, MoS[2] coated, for aerospace applications.
| Committee |
C8
|
| DocumentType |
Draft
|
| Pages |
8
|
| ProductNote |
Superseded by EN 4322:2004
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 4322:2006-03 | 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 |
| 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 <= 25 MM |
| PREN 3818 : 200P1 | AEROSPACE SERIES - BOLTS, MJ THREADS, IN TITANIUM ALLOY TI-P64001 - STRENGTH CLASS: 1100 MPA (AT AMBIENT TEMPERATURE) - TECHNICAL SPECIFICATION |
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