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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE
Hardcopy , PDF
31-01-2011
English
01-01-2010
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Superseded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 |
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 |
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) |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.