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MODUK - DEF STAN 00-970: PT 4: VOL 1

Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials

inactive
Organization: MODUK
Publication Date: 1 November 1990
Status: inactive
Page Count: 502
scope:

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 for the satisfactory operation of the engine.

The Aeroplane designer shall be responsible for the propulsion system installation and shall be responsible for carrying out liaison with the engine and equipment manufacturers to ensure compatibility of the operating characteristics and limitations of all equipment included in the propulsion system.

For each propulsion system installation an analysis shall be completed in accordance with the requirements of Chapter 117 to ensure that no failures will jeopardise the safe operation of the aeroplane. Structural element failures need not be considered if it can be shown that such failures are extremely unlikely. (See Leaflet 117/2).

Components in the propulsion system not approved as part of the engine shall be designed in accordance with Chapter 200 and graded as defined in Chapter 400 para 2.

Each 'Auxiliary Power Unit (APU) must meet the applicable provisions of this Chapter.

The composition of an Engine Change Unit (ECU) shall be as detailed in the engine specification.

Where the requirements of this chapter impose severe and unavoidable penalties or constraints on the aeroplane design, their applicability shall be decided by the Aeroplane Project Director who will carry out the necessary consultations.

Document History

March 10, 1998
Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials
GENERAL In the detailed design of the aeroplane the variety of materials and parts shall be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight....
December 1, 1994
Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design And Strength of Materials
This Standard has been devised for the use of the Crown and of its contractors in the execution of contracts for the Crown and, subject to the unfair Contract Terms Act 1977, the Crown will not be...
October 1, 1992
Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials
GENERAL In the detailed design of the aeroplane the variety of materials and parts to be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight. The...
December 1, 1991
Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials
This Standard has been devised for the use of the Crown and of its contractors in the execution of contracts for the Crown and, subject to the unfair Contract Terms Act 1977, the Crown will not be...
DEF STAN 00-970: PT 4: VOL 1
November 1, 1990
Design and Airworthiness Requirements for Service Aircraft Volume 1 - Aeroplanes Book 2 (Parts 4 to 6 and Chapters 700 to 710) Part 4: Detail Design and Strength of Materials
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...
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