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DEFSTAN 00-970(PT1)SEC3/6(2010) : 2010

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

Superseded date

31-01-2011

Language(s)

English

Published date

01-01-2010

€23.37
Excluding VAT

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Superseded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)

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