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DEFSTAN 00-970(PT7)SEC3/2(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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 3: STRUCTURAL STRENGTH AND DESIGN FOR OPERATION ON SPECIFIED SURFACES

Available format(s)

Hardcopy , PDF

Superseded date

24-12-2010

Language(s)

English

Published date

01-01-2007

LEAFLET 300 DESIGN OF UNDERCARRIAGES - OPERATIONAL REQUIREMENTS
LEAFLET 301 DESIGN OF UNDERCARRIAGES - GENERAL REQUIREMENTS
LEAFLET 302 DESIGN OF UNDERCARRIAGES - HANDLING QUALITIES,
            STRENGTH AND STIFFNESS ON SPECIFIED SURFACES
LEAFLET 303 DESIGN OF UNDERCARRIAGES - WHEEL STEERING
LEAFLET 304 DESIGN OF UNDERCARRIAGES - ALIGHTING
LEAFLET 305 DESIGN OF UNDERCARRIAGES - VERTICAL AND NEAR
            VERTICAL OPERATION ON ROUGH SURFACES
LEAFLET 306 DESIGN OF UNDERCARRIAGES - RETRACTION AND
            LOWERING
LEAFLET 307 CRASH LANDING, DITCHING AND PRECAUTIONARY
            ALIGHTING ON WATER
LEAFLET 308 STRENGTH FOR GROUND HANDLING
LEAFLET 309 PICKETING, TIE-DOWN AND RAPID SECURING SYSTEMS
LEAFLET 310 DESIGN OF UNDERCARRIAGES - WHEELS, TYRES, BRAKES
            AND BRAKING SYSTEMS
APPENDIX No 1 - STRUCTURAL STRENGTH AND DESIGN FOR OPERATION
                ON SPECIFIED SURFACES FOR MILITARY DERIVATIVES
                OF CIVIL ROTORCRAFT
APPENDIX No 2 - U.S. MILITARY SPECIFICATIONS, STANDARDS
                AND HANDBOOKS

Applies to the design of undercarriage units for military rotorcraft and, where relevant, to the rotorcraft as a whole.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT7)SEC3/1(2006). (03/2007)
DocumentType
Standard
Pages
174
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

MIL-S-58095 Revision A:1986 SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
MIL-W-5013 Revision L:1991 WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-S-85510 Base Document:1981
STANAG 3950 : 0 HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION
STANAG 3209 : 2014 TYRE VALVE COUPLINGS

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