EN 2752:1989
Current
Current
The latest, up-to-date edition.
Aerospace series - Nuts, anchor, self locking fixed, two lug, reduced series, with counterbore - Classification : 1100 MPa/235 degree C
Published date
20-03-1989
Publisher
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Brief history
1 Scope
2 Field of application
3 References
4 Required characteristics
5 Designation
6 Marking
7 Technical specification
This standard specifies the characteristics of self locking, two lug, fixed, reduced series anchor nuts, with counterbore.
| Committee |
ASD-STAN
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Standards | Relationship |
| NS EN 2752 : 1ED 1989 | Identical |
| NEN EN 2752 : 1989 | Identical |
| DIN EN 2752:1990-01 | Identical |
| PN EN 2752 : 2000 | Identical |
| I.S. EN 2752:1989 | Identical |
| NF EN 2752 : 1989 | Identical |
| NBN EN 2752 : 1993 | Identical |
| BS EN 2752:1990 | Identical |
| UNE-EN 2752:1992 | Identical |
| ISO 8788:2000 | Aerospace — Nuts, metric — Tolerances of form and position |
| ISO 5855-2:1999 | Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts |
| ISO 5855-1:1999 | Aerospace — MJ threads — Part 1: General requirements |
| EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
| ISO 5858:1999 | Aerospace — Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C — Procurement specification |
| EN 2133:2010 | Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys |
| EN 2000:1991 | Aerospace series - Quality assurance - EN aerospace products - Approval of the quality system of manufacturers |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| EN 2543:2009 | Aerospace series - Steel FE-PL1502 (25CrMo4) - Annealed - Sheet and strip - 0,3 mm ≤ a ≤ 2 mm - For prevailing torque nuts |
Summarise
Sorry this product is not available in your region.