DEFSTAN 00-970(PT1)SEC5/7(2011) : 2011
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
20-07-2012
English
01-01-2011
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Preface
SECTION 5 - POWERPLANT
5.0 Introduction
5.1 General
5.2 Fuel Systems
5.3 Oil Systems
SUPPLEMENTS
Leaflets 0 to 15
Specifies 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)SEC5/6(2011). (11/2011)
|
| DocumentType |
Standard
|
| Pages |
160
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| DEFSTAN 00-970(PT13)/4(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| DEFSTAN 00-970(PT13)/5(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| 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) |
| DEFSTAN 00-970(PT13)/3(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
| 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 |
| DEFSTAN 00-970(PT11)/3(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 11: ENGINES |
| BS 4C 14:1991 | Specification for aircraft pressure refuelling connectors |
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