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.

All labels observed (2)

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Statements (46)

Predicate Object
instanceOf turboshaft engine
application helicopter
certificationAuthority EASA
FAA
Transport Canada
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
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
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
Pratt & Whitney Canada PW207D
Pratt & Whitney Canada PW207E
series PW207
status in service
usedFor corporate transport
emergency medical services
law enforcement operations
training missions
utility helicopter missions
usedOnAircraft Airbus Helicopters EC135
Eurocopter EC135

How these facts were elicited

Referenced by (3)

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

AW109E Power naval helicopter engineModel Pratt & Whitney Canada PW207C
Bell 429 engineModel Pratt & Whitney Canada PW207D1
linked to: Pratt & Whitney Canada PW207C
Pratt & Whitney Canada PW206B relatedEngine Pratt & Whitney Canada PW207C