DEFSTAN 00-970(PT1)SEC3/12(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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 1: FIXED WING - SECTION 3: STRUCTURE
Hardcopy , PDF
11-07-2014
English
01-01-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Preface
SECTION 3 - STRUCTURE
3.0 Introduction
3.1 Static Strength and Deformation
3.2 Fatigue
3.3 Symmetric Manoeuvres
3.4 Asymmetric Manoeuvres
3.5 Gust Loads
3.6 High Lift Devices and Airbrakes
3.7 Pressure Cabins
3.8 Spinning and Spin Recovery
3.9 Control Systems
3.10 Active Control Systems
3.11 Strength for Ground Handling
3.12 Picketing
3.13 Lightning Protection
SUPPLEMENTS
Leaflets 0 to 45
Describes requirements for structural strength of the aircraft.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC3/11(2013). (02/2014)
|
| DocumentType |
Standard
|
| Pages |
333
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| MIL-HDBK-17-3 Revision F:2002 | COMPOSITE MATERIALS HANDBOOK - VOLUME 3: POLYMER MATRIX COMPOSITES MATERIALS USAGE, DESIGN, AND ANALYSIS |
| 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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