DEFSTAN 00-970(PT7)SEC2/3(2010) : 2010
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
English
01-01-2010
30-09-2014
DEFSTAN 00-970(PT7)SEC2/SUPPF/4(2014) : INTERIM
DEFSTAN 00-970(PT7)SEC2/SUPPE/4(2014) : INTERIM
DEFSTAN 00-970(PT7)SEC2/SUPPC/4(2014) : INTERIM
DEFSTAN 00-970(PT7)SEC2/SUPPD/4(2014) : INTERIM
DEFSTAN 00-970(PT7)SEC2/SUPPA/4(2014) : INTERIM
DEFSTAN 00-970(PT7)SEC2/SUPPB/4(2014) : INTERIM
DEFSTAN 00-970(PT7)SEC2/SUPPG/4(2014) : INTERIM
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)SEC2/2(2007). (04/2010)
|
| DocumentType |
Standard
|
| Pages |
167
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy |
|
| Supersedes |
A newer version of this standard is available.
View Current Edition View Current Edition View Current Edition View Current Edition View Current Edition View Current Edition View Current Edition
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : Users cannot be edited or removed once added to your Multi user PDF.