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BSI - BS 4C 14

Specification for Aircraft pressure refuelling connectors

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Organization: BSI
Publication Date: 30 August 1991
Status: active
Page Count: 10
ICS Code (Ground service and maintenance equipment): 49.100
scope:

Basic dimensions and access clearance.

Document History

BS 4C 14
August 30, 1991
Specification for Aircraft pressure refuelling connectors
Basic dimensions and access clearance.
BS 3C 14
October 29, 1982
Specification for Coupling Requirements for Aircraft Pressure Fuelling Connection
Specifies basic design requirements for connections on aircraft to ensure coupling to pressure fuelling equipment on the ground and the access clearance to permit coupling of the hose unit to the...

References

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: PT1 SEC5 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 5: Powerplant
Published by MODUK on July 13, 2015
INTRODUCTION Requirements are provided to cover the following aspects: (a) General - covers installations and testing under ground and flight conditions. (b) Fuel System - covers fuel systems,...
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.
This document is referenced by:
DEF STAN 00-970: PART 11 - Certification Specifications for Airworthiness Part 11: ENGINES
Published by MODUK on August 28, 2020
Unless otherwise specified in this Standard, the certification requirements of EASA CS-E (amendment 6) including related AMC and Appendices shall be applied. Additionally, the requirements of CS-E...
This document is referenced by:
DEF STAN 00-970: PART 13 - Certification Specifications for Airworthiness Part 13: MILITARY COMMON FIT EQUIPMENT
Published by MODUK on August 28, 2020
Note 1 Where a CS makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
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