DEFSTAN 00-970(PT1)SEC3/14(2015) : 2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
13-07-2015
English
01-01-2015
Preface
SECTION 3 - STRUCTURE
SUPPLEMENTS
Gives 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)SEC3/13(2014). (03/2015)
|
DocumentType |
Standard
|
Pages |
323
|
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Superseded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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