PW300
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Technical Specifications
- Thrust
- 24.0 kN (5,400 lbf)
- Bypass Ratio
- 4.5:1
- Fan Diameter
- 0.760 m
- Pressure Ratio
- 18.0:1
- SFC
- 0.4000 lb/lbf·h
- Dry Weight
- 340 kg
- Length
- 1.780 m
- First Run
- 1987
- In Service
- 1991
Overview
The Pratt & Whitney Canada PW300 is a family of medium-thrust turbofan engines designed for the midsize business jet market, producing thrust ratings from approximately 4,500 lbf to 6,400 lbf depending on variant. Developed by Pratt & Whitney Canada (P&WC) — the Longueuil, Quebec subsidiary that dominates the business and regional aviation engine market — the PW300 series entered service in 1991 and has since powered a diverse range of midsize business jets including Dassault Falcon and Hawker aircraft. The PW300's combination of fuel efficiency, compactness, and reliability established it as a strong competitor to the Honeywell TFE731 in the midsize business jet segment.
P&WC brings a unique engineering philosophy to business aviation: the company focuses on optimizing engines for the specific flight profiles of business jets, which typically involve shorter cycles with more takeoffs and landings per flight hour than commercial airliners, combined with high-altitude cruise requirements. The PW300 architecture reflects this focus through its design of the high-pressure compressor and turbine sections, which are optimized for rapid power changes and extended service between overhauls despite demanding operational tempos. FADEC integration in later PW300 variants significantly improved fuel management and reduced pilot workload.
Technical Specifications
| Parameter | Value |
|---|---|
| Maximum Thrust | 24.0 kN (5,400 lbf) |
| Bypass Ratio | 4.5:1 |
| Fan Diameter | 0.760 m (29.9 in) |
| Dry Weight | 340 kg (750 lb) |
| Length | 1.780 m (70.1 in) |
| Overall Pressure Ratio | 18.0:1 |
| SFC | 0.400 lb/lbf·h |
| First Run | 1987 |
| Entry into Service | 1991 |
Variants
The PW300 family covers a wide range of thrust ratings through its variant structure. The PW305A/B (4,500–5,225 lbf) represent earlier variants powering the Learjet 60 and Hawker 1000. The PW306A (5,225 lbf) powers the Dassault Falcon 2000. The PW306C (5,905 lbf) with FADEC serves the Dassault Falcon 2000C/DX/EX series with improved performance and efficiency. The PW307A (6,400 lbf) is the highest-thrust PW300 variant, developed for the Falcon 7X tri-engine ultra-long-range business jet. Each variant shares extensive core commonality, simplifying spare parts management and type training for operators who fly multiple Falcon variants across their fleets.
Aircraft Applications
The PW300 family has been selected as the powerplant for several significant business jet programs. The Dassault Falcon 2000 series (2000, 2000EX, 2000LX, 2000S) uses PW306-series engines and represents Dassault's twin-engine wide-body offering for transatlantic range. The Dassault Falcon 7X, one of the most technologically advanced business jets ever built with fly-by-wire flight controls, uses three PW307A engines. The Learjet 60/60XR used the PW305B to achieve midsize business jet performance. The Hawker 1000 stretched Hawker variant also applied PW300-series technology. This diverse application list spanning French and North American airframers demonstrates the PW300's broad market acceptance.
Development History
P&WC launched the PW300 program in the mid-1980s to address what the company identified as a gap in its product lineup between the smaller PW500 and larger commercial engines. First run occurred in 1987, with initial FAA certification achieved in 1990–1991 for the PW305 variant. The Falcon 2000 application, launched in the same period, provided the critical launch customer commitment that justified the development investment. P&WC's engineering team in Longueuil designed the PW300 with a strong emphasis on ease of maintenance, targeting field-replaceable modules that could be exchanged without specialized tooling — an important consideration for business jet operators who often lack access to large airline maintenance infrastructures. The PW307 development for the Falcon 7X in the mid-2000s extended the family to its current thrust ceiling and introduced the most advanced FADEC implementation in the PW300 series.