DEFSTAN 00-970(PT7)SEC3/2(2007) : 2007
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 3: STRUCTURAL STRENGTH AND DESIGN FOR OPERATION ON SPECIFIED SURFACES
Hardcopy , PDF
24-12-2010
English
01-01-2007
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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Superseded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 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| STANAG 3950 : 0 | HELICOPTER DESIGN CRITERIA FOR CREW CRASH PROTECTION AND ANTHROPOMETRIC ACCOMMODATION |
| STANAG 3209 : 2014 | TYRE VALVE COUPLINGS |
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