DEFSTAN 00-970(PT7)SEC2/SUPPE/4(2014) : INTERIM
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 - SUPPLEMENT E: POWERPLANT (SUBPART E)
Published date
15-12-2014
Publisher
Superseded date
30-01-2015
Superseded by
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1 PROPULSION SYSTEM INSTALLATIONS
2 ENGINES
3 AUXILIARY POWER SYSTEMS
4 REFUELLING AND DEFUELLING SYSTEMS
5 FUEL SYSTEMS
6 FUEL SYSTEMS
7 TRANSMISSION SYSTEMS
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT7)SEC2/3(2010). (12/2014)
|
| DocumentType |
Miscellaneous Product
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| BS C 13:1960 | Sizes of gravity filling orifices on aircraft |
| STANAG 4270 : 0 | AVIATION FUEL DESIGN PARAMETER FOR FUTURE NATO LAND BASED TURBINE POWERED MILITARY AIRCRAFT |
| STANAG 3212 : 2017 | DIAMETERS FOR GRAVITY FILLING ORIFICES |
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