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.

All labels observed (1)

Label Occurrences
Rolls-Royce 250-C30 turboshaft canonical 1

How this entity was disambiguated

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
linked to: Rolls-Royce plc
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
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
linked to: Bell 206

MBB Bo 105 variants
other light helicopter types

How these facts were elicited

Referenced by (1)

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

MD 530F engineModel Rolls-Royce 250-C30 turboshaft
subject linked to: MD 530F helicopter