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DEFSTAN 00-970(PT7)SEC2/2(2007) : 2007

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT
Available format(s)

Hardcopy , PDF

Superseded date

29-01-2010

Language(s)

English

Published date

01-01-2007

LEAFLET 200 STATIC STRENGTH AND DEFORMATION
LEAFLET 201 FATIGUE
LEAFLET 202 MANOEUVRES
LEAFLET 203 CONTROL SYSTEMS - MECHANICAL COMPONENTS
LEAFLET 204 STRENGTH CONSIDERATIONS FOR AUTOMATIC CONTROL
            SYSTEMS
LEAFLET 205 CARRIAGE OF UNDERSLUNG LOADS
LEAFLET 206 DESIGN TO RESIST BIRDSTRIKE DAMAGE
LEAFLET 207 ACTIVE CONTROL SYSTEMS
LEAFLET 208 GUST LOADS
LEAFLET 209 RADOMES
APPENDIX No 1 - STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT FOR
                MILITARY DERIVATIVES OF CIVIL ROTORCRAFT
APPENDIX No 2 - U.S. MILITARY SPECIFICATIONS, STANDARDS AND
                HANDBOOKS

Describes the requirements for static strength and freedom from deformation which might adversely affect airworthiness, handling or maintenance.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT7)SEC2/1(2006). (03/2007)
DocumentType
Standard
Pages
159
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

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