Pratt & Whitney Canada PW210A

E320584

The Pratt & Whitney Canada PW210A is a modern turboshaft engine designed for light and medium twin-engine helicopters, offering improved fuel efficiency, reliability, and reduced emissions.

All labels observed (2)

How this entity was disambiguated

Statements (35)

Predicate Object
instanceOf turboshaft engine ⓘ
application helicopter propulsion ⓘ
category aerospace engine ⓘ
helicopter engine ⓘ
configuration free-turbine turboshaft ⓘ
countryOfOrigin Canada ⓘ
designedFor light twin-engine helicopters ⓘ
medium twin-engine helicopters ⓘ
designGoal high dispatch reliability ⓘ
improved fuel economy over previous generation engines ⓘ
lower operating costs ⓘ
reduced environmental impact ⓘ
emissionStandard reduced CO emissions ⓘ
reduced NOx emissions ⓘ
feature dual-channel FADEC ⓘ
electronic engine control ⓘ
extended time between overhauls ⓘ
health and usage monitoring capability ⓘ
high reliability ⓘ
improved fuel efficiency ⓘ
low maintenance requirements ⓘ
reduced emissions ⓘ
fuelType aviation kerosene ⓘ
manufacturer Pratt & Whitney Canada ⓘ
marketSegment light twin-engine helicopter market ⓘ
medium twin-engine helicopter market ⓘ
partOfFamily Pratt & Whitney Canada PW200 family ⓘ
powerplantFor twin-engine helicopter platforms ⓘ
status in production ⓘ
technologyLevel modern turboshaft technology ⓘ
use civil helicopter operations ⓘ
corporate transport helicopters ⓘ
emergency medical service helicopters ⓘ
law enforcement helicopters ⓘ
utility helicopter missions ⓘ

How these facts were elicited

Referenced by (2)

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

AW169 → engineModel → Pratt & Whitney Canada PW210A ⓘ
subject linked to: AW169 helicopter
Pratt & Whitney Canada PW200 family → member → Pratt & Whitney Canada PW210 ⓘ
linked to: Pratt & Whitney Canada PW210A