DEFSTAN 00-970(PT11)/5(2014) : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 11: ENGINES
Hardcopy , PDF
13-07-2015
English
01-01-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Preface
SECTION ONE - GENERAL
SECTION TWO - ENGINE DEFINITION
SECTION THREE - GENERAL REQUIREMENTS FOR AIRCRAFT ENGINES
SECTION FOUR - MILITARY REQUIREMENTS FOR GAS TURBINE ENGINES
ANNEX
Annex A - Lifing Procedure for Critical Parts
Provides 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.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT11)/4(2012). (01/2014)
|
| DocumentType |
Standard
|
| Pages |
156
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| DEFSTAN 00-970(PT1)SEC5/13(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/11(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
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