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BSI - BS G 217

Specification for General Requirements for Cockpit Lighting Controllers

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Organization: BSI
Publication Date: 31 January 1975
Status: active
Page Count: 12
ICS Code (On-board equipment and instruments): 49.090

Document History

BS G 217
January 31, 1975
Specification for General Requirements for Cockpit Lighting Controllers
A description is not available for this item.

References

This document references:
BS 3G 100-4.1.1 - Specification for General requirements for equipment for use in aircraft - Part 4: Electrical equipment - Section 1: Construction and general - Subsection 1.1: Electrical insulation tests
Published by BSI on November 30, 1982
Specifies requirements for a test to determine the electrical insulation resistance of equipment for use in aircraft together with a high voltage test.
This document is referenced by:
DEF STAN 00-970: PT1 SEC6 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
Published by MODUK on September 19, 2016
INTRODUCTION This Clause specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
This document is referenced by:
DEF STAN 00-970: PART 1 - Certification Specifications for Airworthiness Part 1: FIXED WING COMBAT AIR SYSTEMS
Published by MODUK on August 28, 2020
Note 1 Where CS 25 and CS 23 make reference to ‘the Agency’, this should be considered to mean the certifying authority.
This document is referenced by:
DEF STAN 00-970 PT7: VOL1 - Installations Chapter 711 on
Published by MODUK on March 10, 1998
This chapter states the design requirements for the installation of armament equipment in all aeroplanes. Armament Equipment, for the purpose of these requirements , comprises the weapon...
This document is referenced by:
DEF STAN 00-970:PT7:S2 S6 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Supplement 6: Equipment (Subpart F)
Published by MODUK on July 13, 2015
A description is not available for this item.
This document is referenced by:
DEF STAN 00-970: V2 P7 - Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 3 (Parts 7 to 10) Part 7: Installations
Published by MODUK on March 10, 1998
INTRODUCTION The requirements of this Chapter are applicable to the design and construction of all turbine engine propulsion system installations including all the equipment and sub-systems necessary...
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