SIST EN 2148:2001
(Main)Aerospace series - Rivets, solid, universal head, in aluminium alloy 5056A, inch based series
General Information
- Abstract
This standard specifies the characteristics of solid rivets, with universal head, inch based series, in aluminium alloy, for maximum operating temperature 120 °C.
- Status
- Published
- Publication Date
- 31-Dec-2000
- Technical Committee
- SS SPL - Technical Board for the general field
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 01-Jan-2001
- Due Date
- 01-Jan-2001
- Completion Date
- 01-Jan-2001
Overview
SIST EN 2148:2001 is a European standard developed by CEN that specifies requirements for solid rivets used in aerospace applications. These rivets feature a universal head design and are manufactured from aluminium alloy 5056A. The standard covers an inch-based series and dictates the key characteristics to ensure reliable performance up to a maximum operating temperature of 120 °C. SIST EN 2148:2001 serves as a critical guideline for aerospace engineers and manufacturers seeking consistent quality and compatibility in fastening solutions.
Key Topics
- Rivet Type: Solid rivets with a universal head, designed for aerospace structural applications.
- Material Specification: Aluminium alloy 5056A, known for its strength, corrosion resistance, and suitability for aerospace environments.
- Dimensional Basis: Inch-based sizing series to align with legacy aerospace hardware and international interoperability.
- Operating Temperature: Rated for a maximum continuous operating temperature of 120 °C, ensuring reliability in typical aerospace conditions.
- Mechanical Properties: The standard ensures rivets meet strict mechanical strength and durability requirements to maintain structural integrity.
- Quality Control: SIST EN 2148:2001 includes provisions for manufacturing tolerances and testing to guarantee performance consistency.
Applications
SIST EN 2148:2001 rivets are widely used in the aerospace sector for:
- Aircraft Structural Assembly: Providing permanent mechanical fastening in fuselage panels, wing components, and interior frames.
- Maintenance and Repair: Preferred for high-quality replacements that match original rivet specifications.
- Spacecraft Manufacturing: Suitable for non-critical fastening points where aluminium alloy’s mass-to-strength ratio is advantageous.
- Defense Equipment: Utilized in military aircraft construction and refurbishment due to aluminium alloy's durability.
- General Engineering: Applicable in other transport industries requiring high-strength aluminium rivets with predictable performance.
Related Standards
- EN 2212 - Aluminium alloy rivets with different head styles for aerospace.
- EN 3306 - Solid rivets in magnesium alloys for lightweight aerospace applications.
- ISO 15998 - Mechanical fasteners for aerospace engineering, covering rivet testing methods.
- MIL-R-XXX series - U.S. military standards complementing EN 2148 for aerospace rivets.
- EN 1999 - Eurocode for aluminium structures, providing design guidelines complementary to the rivet standard.
By adhering to SIST EN 2148:2001, aerospace manufacturers and engineers ensure their fastening components meet stringent European safety, quality, and performance criteria, ultimately contributing to the reliability and longevity of aerospace assemblies.
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
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Frequently Asked Questions
SIST EN 2148:2001 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Rivets, solid, universal head, in aluminium alloy 5056A, inch based series". This standard covers: This standard specifies the characteristics of solid rivets, with universal head, inch based series, in aluminium alloy, for maximum operating temperature 120 °C.
This standard specifies the characteristics of solid rivets, with universal head, inch based series, in aluminium alloy, for maximum operating temperature 120 °C.
SIST EN 2148:2001 is classified under the following ICS (International Classification for Standards) categories: 49.025.20 - Aluminium; 49.030.60 - Rivets. The ICS classification helps identify the subject area and facilitates finding related standards.
SIST EN 2148:2001 has the following relationships with other standards: It is inter standard links to SIST EN 9100:2018, SIST EN 9133:2018, SIST EN 2117:2009, SIST EN 2424:2008. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 2148:2001 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Rivets, solid, universal head, in aluminium alloy 5056A, inch based seriesLuft- und Raumfahrt - Vollniete, mit Universalkopf, aus Aluminiumlegierung 5056A, Inch-ReiheSérie aérospatiale - Rivets ordinaires, a tete ronde aplatie, en alliage d'aluminium 5056A, série base inchesAer
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