PREN 4446 : 200P1
Current
The latest, up-to-date edition.
AEROSPACE SERIES - NUTS, ELLIPTICAL CLINCH, SELF-LOCKING - INSTALLATION ADN REMOVAL PROCEDURE
Hardcopy , PDF
English
31-10-2000
1 Scope
2 Normative references
3 Countersinking of installation hole
4 Installation
5 Disassembly - Repair
Gives the manufacturing requirements of recesses, the conditions of installation and removal of self-locking elliptical clinch nut defined by EN standards, for aerospace applications.
| Committee |
C8
|
| DocumentType |
Draft
|
| Pages |
6
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Current
|
| Standards | Relationship |
| DIN EN 4446:2001-05 (Draft) | Identical |
| PREN 4444 : 200P1 | AEROSPACE SERIES - NUTS, ELLIPTICAL CLINCH, SELF-LOCKING, IN HEAT RESISTING STEEL FE-PA2601 (A286), MOS[2] COATED - CLASSIFICATION: 900 MPA (AT AMBIENT TEMPERATURE)/425 DEGREES C - TECHNICAL SPECIFICATION |
| PREN 4445 : 200P1 | AEROSPACE SERIES - NUTS, ELLIPTICAL CLINCH, SELF-LOCKING - DESIGN STANDARD |
| ISO 5855-2:1999 | Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts |
| PREN 4444 : 200P1 | AEROSPACE SERIES - NUTS, ELLIPTICAL CLINCH, SELF-LOCKING, IN HEAT RESISTING STEEL FE-PA2601 (A286), MOS[2] COATED - CLASSIFICATION: 900 MPA (AT AMBIENT TEMPERATURE)/425 DEGREES C - TECHNICAL SPECIFICATION |
| ISO 3161:1999 | Aerospace — UNJ threads — General requirements and limit dimensions |
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