Rolls-Royce 250-C30 turboshaft

E696104

The Rolls-Royce 250-C30 turboshaft is a compact, high-performance gas turbine engine widely used in light helicopters and small aircraft for its reliability and power-to-weight efficiency.

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Observed surface forms (1)

Surface form Occurrences
Rolls-Royce 250-C30 0

Statements (44)

Predicate Object
instanceOf turboshaft engine
application light helicopter
small fixed-wing aircraft
category aero engine
compressorStages axial stages followed by a centrifugal stage
compressorType axial-centrifugal
configuration two-shaft
controlSystem hydromechanical fuel control
coolingMethod air-cooled
countryOfOrigin United Kingdom
designFocus compactness
ease of installation
high time-between-overhaul
designGoal good fuel efficiency
high reliability
low maintenance requirements
exhaustType rearward exhaust outlet
familyVariantOf earlier Rolls-Royce 250 series engines
feature accessory gearbox for helicopter installations
modular construction
quick engine change capability
fuelType Jet-A
Jet-A1
aviation kerosene
intendedMounting helicopter engine bay
manufacturer Rolls-Royce NERFINISHED
marketSegment light helicopter segment
notableCharacteristic compact design
high power-to-weight ratio
high reliability
notableFor good power-to-weight efficiency
widespread use in light helicopters
operatingEnvironment rotary-wing aircraft
small fixed-wing aircraft
partOfEngineFamily Rolls-Royce Model 250 NERFINISHED
powerTransmission output through reduction gearbox
primaryUse civil aviation
military aviation
role main propulsion engine
starterType electric starter
turbineType free power turbine
usedIn Bell 206L LongRanger NERFINISHED
MBB Bo 105 variants
other light helicopter types

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

MD 530F helicopter engineModel Rolls-Royce 250-C30 turboshaft
subject surface form: MD 530F