DEFSTAN 00-970(PT1)SEC5/11(2014) : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
11-07-2014
English
01-01-2014
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)SEC5/10(2013). (02/2014)
|
DocumentType |
Standard
|
Pages |
163
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PublisherName |
UK Ministry of Defence Standards
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Status |
Superseded
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SupersededBy | |
Supersedes |
DEFSTAN 00-970(PT11)/5(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 11: ENGINES |
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 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 AIR 1662 : 2013 | 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)/8(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT |
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