DEFSTAN 00-970(PT1)SEC5/13(2015) : 2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 1: FIXED WING - SECTION 5: POWERPLANT
Hardcopy , PDF
26-07-2022
English
01-01-2015
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Preface
SECTION 5 - POWERPLANT
SUPPLEMENTS
Specifies requirements to cover the following aspects: (a) General - covers installations and testing under ground and flight conditions. (b) Fuel System - covers fuel systems, refuelling and defuelling systems and general flight test requirements. (c) Oil System - covers oil systems for reciprocating engines.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC5/12(2014). (09/2015)
|
| DocumentType |
Standard
|
| Pages |
154
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| DEFSTAN 00-970(PT13)/11(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/12(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-003/5(2016) : 2016 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| DEFSTAN 00-003/6(2017) : 2017 | DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT |
| DEFSTAN 00-970(PT11)/5(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 11: ENGINES |
| DTD 5509 : NOV 63 | SYNTHETIC RUBBER RESISTANT TO ENGINE LUBRICATING OILS, GREASES AND FUELS |
| BS G 175:1959 | Aircraft fuel nozzle grounding plugs and sockets |
| BS 2C 13:1988 | Specification for sizes of aircraft gravity filling orifices and associated replenishment nozzles (metric series) |
| DTD 552 : JUL 61 | RUBBER PARTS FOR USE WITH ENGINE LUBRICATING OIL |
| DEFSTAN 01-5/17(2011) : 2011 | FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
| STANAG 3372 : 2014 | LOW PRESSURE AIR AND ASSOCIATED ELECTRICAL CONNECTIONS FOR AIRCRAFT ENGINE STARTING |
| DEFSTAN 15-2/1(1987) : 1987 | FLEXIBLE TANKS FOR USE IN AIRCRAFT FUEL AND METHANOL/WATER SYSTEMS |
| BS 2C 4:1973 | Specification for coupling dimensions for aero-engine refrigerant pressure replenishment connections |
| SAE AIR1662A | Minimization of Electrostatic Hazards in Aircraft Fuel Systems |
| STANAG 3416 : 0 | METHANOL/WATER AND DEMINERALIZED WATER REPLENISHMENT |
| BS M 48:1975 | Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series |
| BS 4C 14:1991 | Specification for aircraft pressure refuelling connectors |
| DEFSTAN 00-970(PT13)/10(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
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