DEFSTAN 00-970(PT1)SEC3/13(2014) : 2014
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 1: FIXED WING - SECTION 3: STRUCTURE
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
01-01-2014
Publisher
Superseded date
30-01-2015
Superseded by
€22.71
Excluding VAT
Preface
SECTION 3 - STRUCTURE
SUPPLEMENTS
Specifies requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military operation.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC3/12(2014). (10/2014)
|
| DocumentType |
Standard
|
| Pages |
340
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
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| DEFSTAN 00-31/1(1987) : 1987 | THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS |
| FAA AC 20-107 : 2009 | COMPOSITE AIRCRAFT STRUCTURE |
| BS C 11:1958 | Coupling dimensions for aircraft pressure cabin ground test connections |
| DEFSTAN 16-17/2(1983) : 1983 | AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT |
| MIL-DTL-9490 Revision E:2008 | Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for |
| BS C 10:1958 | Coupling dimensions for aircraft ground air-conditioning connections |
| DEFSTAN 53-68/2(1977) : 1977 AMD 2 1984 | V-FLANGE COUPLINGS FOR AIRCRAFT PIPING AND DUCTING (METRIC) |
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