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BSI - BS G 262

Aircraft - Declaration of Design and Performance for Aircraft Equipment - Standard Form

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Organization: BSI
Publication Date: 15 May 1998
Status: active
Page Count: 12
ICS Code (Aircraft and space vehicles in general): 49.020

Document History

BS G 262
May 15, 1998
Aircraft - Declaration of Design and Performance for Aircraft Equipment - Standard Form
A description is not available for this item.

References

This document references:
ISO 2678 - Environmental Tests for Aircraft Equipment - Insulation Resistance and High Voltage Tests for Electrical Equipment
Published by ISO on May 15, 1985
A description is not available for this item.
This document references:
ISO 7137 - Aircraft - Environmental Conditions and Test Procedures for Airborne Equipment
Published by ISO on June 1, 1995
This International Standard lists the different environmental conditions and test procedures for airborne equipment and is primarily intended for civil and/or transport aircraft applications. This...
This document references:
ISO 2669 - Environmental Tests for Aircraft Equipment - Steady-State Acceleration
Published by ISO on April 15, 1995
This International Standard specifies two types of steady-state acceleration test and establishes five severity grades of acceleration forces used to simulate a gradually changing acceleration...
This document references:
ISO 2671 - Environmental Tests for Aircraft Equipment - Part 3.4: Acoustic Vibration First Edition
Published by ISO on January 1, 1982
A description is not available for this item.
This document is referenced by:
BS 3G 230 - Specification for General Requirements for Aircraft Electrical Cables (Second Series)
Published by BSI on May 15, 2000
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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