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ASD-STAN PREN 3434

Aerospace series - Nuts, hexagon, slotted/castellated, selflocking, in steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C

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Organization: ASD-STAN
Publication Date: 1 May 2019
Status: active
Page Count: 9
scope:

This standard specifies characteristics of self-locking hexagonal slotted/castellated nuts, in steel, cadmium plated, MoS2 lubricated, for aerospace applications.

Classification: 900 MPa1/235 °C2.

Document History

ASD-STAN PREN 3434
May 1, 2019
Aerospace series - Nuts, hexagon, slotted/castellated, selflocking, in steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C
This standard specifies characteristics of self-locking hexagonal slotted/castellated nuts, in steel, cadmium plated, MoS2 lubricated, for aerospace applications. Classification: 900 MPa1/235 °C2.
PREN 3434
December 31, 2010
Aerospace series Nuts, hexagon, slotted / castellated, self-locking, in steel, cadmium plated, MoS2 lubricated Classification : 900 MPa (at ambient temperature) / 235 °C
A description is not available for this item.
PREN 3434
August 1, 1998
Aerospace Series Nuts, Hexagon, Slotted / Castellated, Self-Locking, in Steel, Cadmium Plated, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature)/235 Degrees C
A description is not available for this item.
PREN 3434
September 30, 1997
Aerospace Series Nuts, Hexagon, Slotted/Castellated, Self-Locking, in Steel, Cadmium Plated, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature)/235 Degrees C
A description is not available for this item.
PREN 3434
March 1, 1991
Aerospace Series Nuts, Hexagon, Slotted, Self-Locking, in Steel, Cadmium Plated, MoS2 Lubricated Classification: 900 MPa (at Ambient Temperature)/235 Degrees C
A description is not available for this item.

References

This document references:
ASD-STAN TR 3791 - Aerospace Series Materials for Self-Locking Nuts, Threaded Inserts and Screw Thread Inserts of Temperature Classes Less Than or Equal to 425 Degrees Celsius
Published by ASD-STAN on January 1, 1999
A description is not available for this item.
This document references:
EN 2133 - Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
Published by CEN on December 1, 2020
This document specifies the electrolytic cadmium plating of parts and fasteners in steel of tensile strength UTS≤1 450 MPa, copper, copper alloys and nickel alloys, whose temperature in service does...
This document references:
EN 2367 - Split Pins in Steel EN 2573
Published by CEN on January 1, 1989
A description is not available for this item.
This document references:
EN 2424 - Aerospace series - Marking of aerospace products
Published by CEN on May 1, 2008
A description is not available for this item.
This document references:
EN 2491 - Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
Published by CEN on June 1, 2011
This European Standard defines the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion...
This document references:
EN 9100 - Quality Management Systems - Requirements for Aviation, Space and Defence Organizations
Published by CEN on May 1, 2018
This document includes EN ISO 9001:20152 quality management system requirements and specifies additional aviation, space and defence industry requirements, definitions and notes. It is emphasized...
This document references:
EN 9133 - Aerospace series - Quality Management Systems - Qualification Procedure for Aerospace Standard Products
Published by CEN on June 1, 2018
General This document defines a system for the qualification of standard products for aviation, space, and defenc applications. It defines the principles that shall be adhered to when carrying out...
This document references:
ISO 5855-2 - Aerospace - MJ Threads - Part 2: Limit Dimensions for Bolts and Nuts
Published by ISO on October 15, 1999
This part of ISO 5855 specifies limit dimensions of MJ threads for bolts and nuts of nominal diameter 1,6 mm to 39 mm for aerospace construction.
This document references:
ISO 5858 - Aerospace - Nuts, Self-Locking, with Maximum Operating Temperature Less Than or Equal to 425 Degrees Celsius - Procurement Specification
Published by ISO on November 15, 1999
This International Standard specifies the required characteristics for metric self-locking nuts, with MJ threads, for use in aerospace construction at a maximum temperature less than or equal to 425...
This document references:
ISO 8788 - Aerospace — Nuts, metric — Tolerances of form and position
Published by ISO on May 1, 2020
This document defines the tolerances of form and position of metric nuts meant for aerospace construction. These tolerances comply with ISO 1101, ISO 2692 and ISO 5459.
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