UNLIMITED FREE
ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Select Your Free Newsletters

Industry Newsletters

Select Your Free Product Alerts

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

BSI - BS 2G 134

Specification for D.C. generators

active, Most Current
Buy Now
Organization: BSI
Publication Date: 23 October 1970
Status: active
Page Count: 14
ICS Code (Aerospace electric equipment and systems): 49.060

Document History

BS 2G 134
October 23, 1970
Specification for D.C. generators
A description is not available for this item.

References

This document references:
BS 3G 100-2.3.1 - Specification for General Requirements for Equipment for Use in Aircraft - Part 2: All Equipment - Section 3: Environmental Conditions - Subsection 3.1: Vibration
Published by BSI on December 31, 1969
A description is not available for this item.
This document references:
BS 3G 100-2.3.2 - Specification for General requirements for equipment in aircraft - Part 2: All equipment - Section 3: Environmental conditions - Subsection 3.2: Temperature - pressure requirements
Published by BSI on October 28, 1970
A description is not available for this item.
This document references:
BS G 102 - Specification for General requirements for rotating electrical machinery
Published by BSI on April 23, 1971
A description is not available for this item.
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: 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...
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 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: 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.
View Less
View All

Related Products

Searching for related products...

Advertisement