Pratt & Whitney Canada PW207C

E832685

The Pratt & Whitney Canada PW207C is a turboshaft aircraft engine designed for light twin-engine helicopters, offering reliable performance and efficiency for civil and military rotorcraft applications.

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Label Occurrences
Pratt & Whitney Canada PW207C canonical 1

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Statements (46)

Predicate Object
instanceOf turboshaft engine
application helicopter
certificationAuthority EASA NERFINISHED
FAA NERFINISHED
Transport Canada NERFINISHED
compressorType axial-centrifugal compressor
configuration two-shaft turboshaft
controlSystem dual-channel FADEC
full authority digital engine control
coolingSystem air-cooled
countryOfOrigin Canada
cycle Brayton cycle
family Pratt & Whitney Canada PW200 NERFINISHED
feature high reliability
low emissions
low fuel consumption
low maintenance requirements
modular design
redundant electronic control
fuelType Jet A
Jet A-1
aviation kerosene
generation PW200 series improved variant
ignition electronic ignition
intendedRole twin-engine helicopter powerplant
manufacturer Pratt & Whitney Canada NERFINISHED
marketSegment civil rotorcraft
military rotorcraft
notableFor efficient fuel consumption for its class
reliable performance in light twin helicopters
operatorType civil operators
military operators
powerClass small turboshaft
primaryUse light twin-engine helicopters
relatedEngine Pratt & Whitney Canada PW206 NERFINISHED
Pratt & Whitney Canada PW207D NERFINISHED
Pratt & Whitney Canada PW207E NERFINISHED
series PW207 NERFINISHED
status in service
usedFor corporate transport
emergency medical services
law enforcement operations
training missions
utility helicopter missions
usedOnAircraft Airbus Helicopters EC135 NERFINISHED
Eurocopter EC135 NERFINISHED

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Referenced by (1)

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

AW109E Power naval helicopter engineModel Pratt & Whitney Canada PW207C