DEFSTAN 00-970(PT1)SEC3/6(2010) : 2010
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
English
01-01-2010
31-01-2011
Preface
Main Text
SECTION 3 - STRUCTURE
SUPPLEMENTS
Leaflets 0 to 44
Describes the requirements for structural strength of the aircraft.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC3/5(2007). (04/2010)
|
| DocumentType |
Standard
|
| Pages |
326
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-HDBK-17-3 Revision F:2002 | Composite Materials Handbook Volume 3. Polymer Matrix Composites Materials Usage, Design, and Analysis (S/S by SAE-R424)) |
| DEFSTAN 00-31/1(1987) : 1987 | THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| 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 |
| 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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