PREN 4322 : 200P1
Withdrawn
View Superseded by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
English
12-19-2023
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Superseded by EN 4322:2004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Withdrawn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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