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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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

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Superseded date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

$44.20
Including GST where applicable

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Superseded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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MIL-R-7705 Revision B:1975 RADOME, GENERAL SPECIFICATION FOR
ASTM D 3983 : 1998 Standard Test Method for Measuring Strength and Shear Modulus of Nonrigid Adhesives by the Thick-Adherend Tensile-Lap Specimen
MIL A 87221 : 0 AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
DEFSTAN 00-3/3(1985) : 1985 DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT

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