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DEFSTAN 00-970(PT1)SEC3/4(2006) : 2006

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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: COMBAT A/C - SECTION 3 - STRUCTURE

Available format(s)

Hardcopy , PDF

Superseded date

31-01-2007

Language(s)

English

Published date

01-01-2006

£20.00
Excluding VAT

Preface
Main Text
SECTION 3 - STRUCTURE
  3.0 Introduction
  3.1 Static Strength
  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
Tables
Figures
SUPPLEMENTS
Leaflets 0 to 41

Specifies the requirements for structure strength of the aircraft.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT1)SEC3/3(2003) (04/2006)
DocumentType
Standard
Pages
281
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
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
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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