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MODUK - DEF STAN 47-21

Flexible Hose Assemblies for Pitot and Static Systems in Aircraft (Metric)

inactive, Most Current
Organization: MODUK
Publication Date: 1 January 1979
Status: inactive
Page Count: 4

Document History

DEF STAN 47-21
January 1, 1979
Flexible Hose Assemblies for Pitot and Static Systems in Aircraft (Metric)
A description is not available for this item.

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: 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: 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 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.
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: 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: 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...
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