Initial Operational Capability (IOC): 2016
Maiden Flight: 2015
Total Production: ?
Origin: Canada
Corporations: Pratt & Whitney Canada
Parent System: PW300
Initial Operational Capability (IOC): 1993
Total Production: ?
Family Members: PW300 and PW307B
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Description: The PW300 is a family of turbofan engines designed by Pratt & Whitney Canada to meet the requirements of Super Mid-Size corporate aircraft. These engines yield from 4,500 to 8,000 pounds thrust range. Moreover, they are clean, quiet and offer low operating costs. This engine family incorporates the latest component technologies such as a damage-resistant wide chord fan and a titanium alloys centrifugal impeller. The PW300 engines also feature Full Authority Digital Electronic Control (FADEC) for reduced pilot workload.

As of early 2008, the PW300 engine family has logged more than 6.5 million flight hours powering roughly 1,000 aircraft in 50 countries. The PW300 program includes eight engine variants.

The Pratt & Whitney Canada PW307D engine variant has been selected to power the Dassault Aviation Falcon 8X ultra long range business jet beginning in 2016. The selection was announced on May 19, 2014. The PW307D engine is rated at 6,722-lb of thrust. It will deliver superior performance, high durability and low operating economics, with significantly lower emission and noise levels. It also offers high dispatch reliability and easy maintenance. The PW307D is a derivative of the PW307A engine powering the Falcon 7X business jet.

PW307D Applications

Private Aircraft Falcon 8X

PW307D Specifications

Max Takeoff Thrust: 6,722 pound (3,049 kilogram)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)
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