Pratt & Whitney Canada PW300
The Pratt & Whitney Canada PW300 is a family of turbofan engines in the thrust range from 20 to 35 kN that have been specially developed for business jets. The basic construction consists of a single-stage fan, driven by a three-stage low-pressure turbine , a four-stage axial and single-stage centrifugal high pressure compressor , driven by a two-stage high pressure turbine, and an annular combustion chamber . Some versions have a non-mixing nozzle, but the PW306 and PW308 include a forced draft mixer for the exhaust jet. The engines are powered by a FADEC-System controlled.
The PW300 is used in the Learjet 60 , Cessna Citation Sovereign , Gulfstream G200 , Hawker 1000 , Dassault Falcon 7X , Fairchild-Dornier 328JET and White Knight Two, among others .
The PW307 was specially developed for the three-turbine arrangement of the Dassault Falcon 7X . It was approved by the Canadian Aviation Administration in March 2005.
Technical specifications
Type | Thrust (kN) | By- pass ratio at start |
Total pressure ratio |
Blower diameter (m) |
Length (m) | Dry matter (kg) |
Admission | Use at |
---|---|---|---|---|---|---|---|---|
PW305A | 20.81 | 4.3: 1 | 19: 1 | 0.79 | 1.651 | 450 | 1992 | Learjet 60 |
PW305B | 23.4 | 4.3: 1 | 15.5: 1 | 0.80 | 1.547 | Hawker 1000 | ||
PW306A | 28.86 | 4.5: 1 | 18.3: 1 | 0.81 | 1.92 | 473 | 1995 | Gulfstream G200 |
PW306B | 26.91 | 4.5: 1 | 0.81 | 1.92 | 473 |
Fairchild Dornier 328 Jet IAI Galaxy |
||
PW306C | 25.66 | 4.5: 1 | 0.81 | 1.92 | 473 | 2002 | Cessna Sovereign | |
PW307A | 28.48 | 0.83 | 2.184 | 2007 | Dassault Falcon 7X | |||
PW308A | 30.7 | 4.1: 1 | 20.4: 1 | 0.84 | 2.134 | 607 | 2004 | Hawker 4000 |
PW308B | 32.92 | 0.84 | 2.134 | Fairchild Dornier 428 Jet | ||||
PW308C | 31.13 | 3.8: 1 | 25.5: 1 | 0.84 | 2.134 | 614 | 2001 | Dassault Falcon 2000EX |
Web links
- Manufacturer site (English)
- Type certification of the PW306 series - EASA-TCDS-A.051 (PDF; 189 kB)
- Type certification of the PW307 series - EASA-TCDS-A.035 (PDF; 171 kB)
- Type certification of the PW308 series - EASA-TCDS-A.057 (PDF; 268 kB)
- Letter of approval from the FAA (English) (PDF file; 145 kB)
- Data sheet from MTU