Shaping a new generation of helicopters with 1,100 shaft horsepower class. Game-changing performance. The heart of an exciting new generation of helicopters. Impressive improvements in fuel burn, power-to-weight, and operating economics. Maintaining Pratt & Whitney’s reputation for high durability and reliability.
The PW210, Pratt & Whitney’s new 1,000 shaft horsepower class engine, sets the stage for a new era of advanced helicopter engines.
Shaping a new generation of helicopters with 1,100 shaft horsepower class. Game-changing performance. The heart of an exciting new generation of helicopters. Impressive improvements in fuel burn, power-to-weight, and operating economics. Maintaining Pratt & Whitney’s reputation for high durability and reliability.
The PW210 raises the bar on performance and operating economics by introducing an impressive menu of advanced technologies and leveraging technologies from Pratt & Whitney's latest engine families.
Plan your budget and minimize unscheduled maintenance with our Maintenance Programs: Our Eagle Service PlanTM (ESPTM) for single aircraft, our Fleet Service Plan (FSP) for growing fleets of two to five helicopters, and our Fleet Management Plan (FMP) for fleets of six or more aircraft.
You can keep your helicopter in the air with our SMART program. Our two-year, 500-hour Certified Pre-Owned program benefits buyers and sellers of used helicopters.
Use our oil analysis technology, now included as part of Eagle Service™ Plan (ESP™) coverage. You may also purchase it separately through the MyP&WC Power portal.
The 1,000 shaft horsepower class PW210 is simple in concept, with only five major rotating components and a modular design enabling easy maintenance. A two-stage centrifugal compressor, driven by a single-stage turbine with an advanced technology reverse flow combustor, powers a free, two-stage power turbine. The power turbine, in turn, powers the output shaft through a front-mounted reduction gearbox. Combining the reduction and engine accessory gearbox contributes to the PW210's compact design. The PW210's control system features a Dual Channel Full Authority Digital Engine Control (FADEC) delivering a new standard in ease of operation, maintenance diagnostics and other control features. Game-changing performance is the key to an exciting future for the PW210. Low fuel consumption, lightweight, a compact architecture, minimum maintenance and low maintenance cost will contribute strongly to the success of a new generation of helicopters.
Yes, we retrofit legacy systems (e.g., GE Frame 5, Siemens V94.2) with modern digital controllers, typically completing hardware integration within 4-8 weeks. Software migration requires additional validation time.
We recommend annual performance testing under ISO 3977-2 standards. Critical applications (e.g., offshore platforms) may require semi-annual tests with emissions compliance checks.
All rad-hard devices (e.g., FPGA, ADC) are QML Class V certified under MIL-PRF-38535 and tested to MIL-STD-883 Method 1019 for SEU tolerance. Full qualification reports are available upon request.
Our ASICs and power management ICs operate across -55°C to +175°C ambient temperatures, with derating curves provided in military temperature range (MTR) datasheets.
Our PMA parts (e.g., actuators, sensors) hold FAA/EASA Form 1 certification and match OEM form/fit/function. Installation requires SB/MB documentation per FAA AC 23.1529.
All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
AOG orders ship within 4 hours for stocked items (FAA-PMA, EASA Part 21G). Non-stock critical parts trigger priority manufacturing with 72-hour max turnaround.
Gas Turbine
Aircraft parts
