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DEFSTAN 00-970(PT1)SEC5/8(2012) : 2012

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5 - POWERPLANT
Available format(s)

Hardcopy , PDF

Superseded date

07-01-2013

Language(s)

English

Published date

01-01-2012

Preface
SECTION 5 - POWERPLANT
5.0 Introduction
5.1 General
5.2 Fuel Systems
5.3 Oil Systems
Tables
SUPPLEMENTS
Leaflets 0 to 15

Specifies 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)SEC5/7(2011). (08/2012)
DocumentType
Standard
Pages
162
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

DEFSTAN 00-970(PT13)/7(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
DEFSTAN 00-970(PT13)/6(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
DEFSTAN 00-970(PT13)/8(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 13: MILITARY COMMON FIT EQUIPMENT
DEFSTAN 00-970(PT13)/9(2014) : 2014 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 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
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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