DEFSTAN 00-970(PT7)SEC2/1(2006) : 2006
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Hardcopy , PDF
31-01-2007
English
01-01-2006
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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
Specifies the requirements for static strength and freedom from deformation which might adversely affect airworthness, handling or maintenance.
| DevelopmentNote |
Supersedes DEFSTAN 00-970/VOL2/1(1984). (06/2006)
|
| DocumentType |
Standard
|
| Pages |
140
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| STANAG 3542 : 2011 | TECHNICAL CRITERIA FOR THE TRANSPORT OF CARGO BY HELICOPTER |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR |
| 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 |
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