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BS EN 2752:1990

Current
Current

The latest, up-to-date edition.

Specification for nuts, anchor, self locking fixed, two lug, reduced series, with counterbore. Classification: 1100 MPa/235°C
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

06-29-1990

Publisher

British Standards Institution

Cooperating organizations
National foreword
Brief history
1 Scope
2 Field of application
3 References
4 Required characteristics
5 Designation
6 Marking
7 Technical specification
National appendix A
National appendix B

Characteristics of nuts for use in aircraft assemblies subjected principally to shear loading.

Committee
ACE/12
DevelopmentNote
Supersedes 88/72139 DC (10/2005)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current

Standards Relationship
EN 2752:1989 Identical
NS EN 2752 : 1ED 1989 Identical
NEN EN 2752 : 1989 Identical
DIN EN 2752:1990-01 Identical
NF EN 2752 : 1989 Identical
NBN EN 2752 : 1993 Identical
UNI EN 2752 : 1989 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

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