MODUK - DEF STAN 00-970: PART 11

Design and Airworthiness Requirements for Service Aircraft Part 11 Engines

inactive

Organization:	MODUK
Publication Date:	31 October 2011
Status:	inactive
Page Count:	168

scope:

Part 11 details the general requirements for the performance, operating characteristics, design, reliability and maintainability of gas turbine aero engines and associated jet pipes for use in UK military aeroplanes and rotorcraft. It also includes the demonstrations, tests, reports and other work required to be completed satisfactorily prior to prototype flight clearance and subsequent Design Certification of the engine.

Guidelines on the content and format of individual Engine Model Specifications are given in clause 1.6.

Document History

DEF STAN 00-970: PART 11

August 28, 2020

Certification Specifications for Airworthiness Part 11: ENGINES

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...

DEF STAN 00-970: PART 11

May 14, 2018

Design and Airworthiness Requirements for Service Aircraft Part 11: Engines

INTRODUCTION This Part of the Defence Standard has been issued to provide requirements and guidance for the certification of UK military aircraft engines. This standard has been developed in full...

DEF STAN 00-970: PART 11

July 13, 2015

Design and Airworthiness Requirements for Service Aircraft Part 11: Engines