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BSI - BS EN 2127

Aluminium Alloy AL-P7075-T73511 Extruded Bars and Sections a or D Less Than or Equal to 100 mm

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Organization: BSI
Publication Date: 15 November 1992
Status: active
Page Count: 12
ICS Code (Aluminium): 49.025.20

Document History

BS EN 2127
November 15, 1992
Aluminium Alloy AL-P7075-T73511 Extruded Bars and Sections a or D Less Than or Equal to 100 mm
A description is not available for this item.

References

This document references:
BS EN 2048 - Aerospace Series - Extruded L-Section, in Aluminium Alloys - Dimensions
Published by BSI on September 15, 2001
A description is not available for this item.
This document references:
BS EN 2134 - Round Bars, Extruded in Aluminium and Aluminium Alloys - Diameter 10 mm Less Than or Equal to D Less Than or Equal to 220 mm - Dimensions
Published by BSI on January 4, 2002
A description is not available for this item.
This document references:
BS EN 2047 - Aerospace Series - Beaded L-Section Extruded, in Aluminium Alloys - Dimensions
Published by BSI on September 15, 2001
A description is not available for this item.
This document references:
BS EN 2050 - Aerospace series - Extruded T-section, in aluminium alloys - dimensions
Published by BSI on September 15, 2001
A description is not available for this item.
This document is referenced by:
DEF STAN 00-970: PART 0 - Certification Specifications for Airworthiness Part 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Published by MODUK on March 14, 2021
Part 0 provides guidance and content information, together with definitions of terms used throughout this Standard.
This document is referenced by:
DEF STAN 00-970: PART 5 - Certification Specifications for Airworthiness Part 5: LARGE TYPE AIR SYSTEMS
Published by MODUK on March 14, 2021
Where CS 25 makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
This document is referenced by:
DEF STAN 00-970: PART 9 - Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
Published by MODUK on September 28, 2017
(a) The mandatory requirements set out in this Standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services based on the requirements...
This document is referenced by:
DEF STAN 00-970: PT7 SEC1 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Section 1: Introduction
Published by MODUK on July 13, 2015
This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Rotorcraft Aircraft for UK Military operation.
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