Pratt & Whitney Canada PW200
The Pratt & Whitney Canada PW200 is a family of turbine engines developed specifically for helicopter applications.
Variants
- PW206A
- Maximum continuous power 550 shp (410 kW)[1] for use on the MD Explorer
- PW206B
- Maximum continuous power 431 shp (321 kW),[1] for use on the Eurocopter EC135
- PW206B2
- Maximum continuous power 431 shp (321 kW).[1]
- PW206C
- Maximum continuous power 561 shp (418 kW),[1] for use on the Agusta A109 Power
- PW206E
- Maximum continuous power 572 shp (427 kW).[1]
- PW207C
- Maximum continuous power 572 shp (427 kW).[1]
- PW207D
- Maximum continuous power 572 shp (427 kW).[1]
- PW207D1
- Variant of the PW207 with increased mechanical power, maximum continuous power 610 shp (450 kW).[1]
- PW207D2
- Variant of the PW207D1 with a fuel heater installed, maximum continuous power 610 shp (450 kW).[1]
- PW207E
- Maximum continuous power 572 shp (427 kW).[1]
- PW210
- Approx 1,000 shp (750 kW)
Applications
Specifications
Data from [2]
General characteristics
- Type: Turboshaft
- Length: 35.9 in (91.2 cm)
- Diameter: 19.7 in (50 cm)
- Dry weight: 237 lb (107.5 kg)
Components
- Compressor: Single-stage centrifugal
- Combustors: Annular
- Turbine: Single-stage high pressure turbine, single-stage low pressure turbine
Performance
References
External links
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