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, environmental emissions and operating economics. Maintaining Pratt & Whitney’s reputation for high durability and reliability.

Overview

The PW210, Pratt & Whitney’s new 1,000 shaft horsepower class engine, sets the stage for a new era of advanced helicopter engines.

Setting New Standards

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The PW210 is helping shape a new generation of twin-engine helicopters setting new standards in fuel burn, power-to-weight ratio, environmental emissions and operating economics while maintaining Pratt & Whitney’s reputation for high durability and reliability, the hallmarks of dependability.

Raising the Bar on Performance and Operating Economics

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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.

The PW210 Engine Incorporates the Latest Technologies to Exceed Our Customers' Expectations

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, low environmental emissions, minimum maintenance and low maintenance cost will contribute strongly to the success of a new generation of helicopters.

Specs

Engines Thermo Power Class* (Shaft Horsepower) Mechanical Power Class*(Shaft Horsepower) Output Shaft Speed (RPM) Height** (Inches) Width** (Inches) Length** (Inches)
PW210 Series 1,000 800-900 6,000 to 14,000 23.5 19.7 43

*Powers are approximate values at take-off. Available at sea level, standard day, static conditions, uninstalled.

** Dimensions are approximate values.

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