BS EN 4424:2006
Current
The latest, up-to-date edition.
Aerospace series. Rod-ends, adjustable single fork and threaded shank with engagement: 1,5 x thread diameter in titanium alloys. Dimensions and loads
Hardcopy , PDF
English
30-06-2006
Foreword
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification
Describes the characteristics of rod-ends for flight control rods. - a single fork; - a threaded shank comprising; - a circumferential groove to identify engagement; - an optional longitudinal groove for locking purpose. These rod-ends are intended for use with control rods or rods for aircraft structures.
| Committee |
ACE/12
|
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
This standard specifies the characteristics of rod-ends for flight control rods. a single fork; a threaded shank comprising; a circumferential groove to identify engagement; an optional longitudinal groove for locking purpose. These rod-ends are intended for use with control rods or rods for aircraft structures.
| Standards | Relationship |
| I.S. EN 4424:2006 | Identical |
| NBN EN 4424 : 2006 | Identical |
| DIN EN 4424:2007-03 | Identical |
| EN 4424:2006 | Identical |
| NS EN 4424 : 1ED 2006 | Identical |
| NF EN 4424 : 2006 | Identical |
| NEN EN 4424 : 2006 | Identical |
| UNE-EN 4424:2006 | Equivalent |
| 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 2601:1996 | Aerospace series - Fork ends, adjustable - Technical specification |
| PREN 3315 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM |
| TR 3775 : 4 | AEROSPACE SERIES - BOLTS AND PINS - MATERIALS |
| PREN 3353 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63 - SOLUTION TREATED AND AGED - R[M] >= 1100 MPA - BAR AND WIRE FOR FASTENERS MACHINED - D[E] <= 25 MM |
| ISO 3353-1:2002 | Aerospace — Lead and runout threads — Part 1: Rolled external threads |
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