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DEFSTAN 00-970(PT7)SEC2/SUPP5/6(2015) : 2015

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 7: ROTORCRAFT - SUPPLEMENT 5: POWERPLANT (SUBPART E)
Superseded date

07-26-2022

Published date

02-26-2016

Publisher

UK Ministry of Defence Standards

DevelopmentNote
Supersedes DEFSTAN 00-970(PT7)SEC2/SUPP5/5(2015). (02/2016)
DocumentType
Standard
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy
Supersedes

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

STANAG 3368 : 2014 INTERNAL AIRCRAFT ENGINE STARTING SYSTEM
DEFSTAN 47-19/1(1977) : 1977 AMD 2 AIRCRAFT PIPE FITTINGS (INCH SERIES) - SCREW THREADS, HEXAGON SIZES, TAPPED HOLES, AND 'O' RING SEALS
BS G 175:1959 Aircraft fuel nozzle grounding plugs and sockets
DEFSTAN 47-23/1(1980) : 1980 BEAD PROFILE FOR AIRCRAFT PIPING AND DUCTING (FLEXIBLE CONNECTIONS)
DEFSTAN 15-2/1(1987) : 1987 FLEXIBLE TANKS FOR USE IN AIRCRAFT FUEL AND METHANOL/WATER SYSTEMS
DEFSTAN 16-10/3(1983) : 1983 AMD 1 LOW PRESSURE AIR STARTING OF AIRCRAFT ENGINES
DEFSTAN 91-2 : LATEST PETROLEUM FUELS
BS 2C 4:1973 Specification for coupling dimensions for aero-engine refrigerant pressure replenishment connections
DEFSTAN 53-94/1(1983) : 1983 PROTECTIVE CAPS AND PLUGS FOR AIRCRAFT PIPELINES
DEFSTAN 47-12/4(1987) : 1987 POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES (WIRE REINFORCED) FOR MEDIUM AND HIGH PRESSURE FLUID SYSTEMS IN AIRCRAFT
DEFSTAN 00-971/1(1987) : 1987 GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES
DEFSTAN 17-2/3(1989) : 1989 REPLENISHMENT EQUIPMENT FOR AERO ENGINE THRUST AUGMENTATION (REFRIGERANT INJECTION) SYSTEMS
BS C 13:1960 Sizes of gravity filling orifices on aircraft
BS 4C 14:1991 Specification for aircraft pressure refuelling connectors
STANAG 4270 : 0 AVIATION FUEL DESIGN PARAMETER FOR FUTURE NATO LAND BASED TURBINE POWERED MILITARY AIRCRAFT
DEFSTAN 53-70/2(1976) : 1976 AMD 2 DIMENSIONS OF ELASTOMERIC TOROIDAL SEALING RINGS (INCH SERIES) FOR AIRCRAFT PURPOSES
DEFSTAN 00-970/VOL1/1(1983) : AMD 14 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - AEROPLANES
DEFSTAN 61-12(PT20)/1(1980) : 1980 WIRES, CORDS, AND CABLES, ELECTRICAL - METRIC UNITS - PART 20: BRAIDS, WIRE
STANAG 3212 : 2017 DIAMETERS FOR GRAVITY FILLING ORIFICES
DEFSTAN 53-68/2(1977) : 1977 AMD 2 1984 V-FLANGE COUPLINGS FOR AIRCRAFT PIPING AND DUCTING (METRIC)

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