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DEFSTAN 00-970(PT7)SEC2/3(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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 7: ROTORCRAFT - SECTION 2: STRUCTURAL STRENGTH AND DESIGN FOR FLIGHT

Available format(s)

Hardcopy , PDF

Superseded date

30-09-2014

Language(s)

English

Published date

01-01-2010

€23.37
Excluding VAT

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.

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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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