PW2000

Since 1979 MTU has developed and produced the PW2000 engine family with a maximum take-off thrust of 195 kN, in cooperation with Pratt & Whitney.

PW2000s are in use in medium-to-long-haul commercial and military applications.

MTU holds a 21.2% stake in this successful engine, having developed the low-pressure turbine and turbine exit casing as well as producing critical parts of the low-pressure turbine and other highly engineered components. MTU Maintenance Hannover in turn provides full repair services for the engine.

Technical Data
Max. thrust	191 kN
Bypass ratio	5.4:1
Pressure ratio	29.5:1
Length	3729 mm
Fan diameter	1994 mm
Weight	3311 kg

Facts – PW2000

Two-shaft-turbofan engine
Active clearance control
New airfoil profiles
New materials
New combustor configuration
Modular design
Digital control unit
On-condition maintenance

Development at MTU

Low-pressure turbine
Turbine exhaust casing

Production at MTU

Low-pressure turbine (various parts)
Turbine exhaust casing
High-pressure compressor and high-pressure turbine components as well as parts of the diffuser / combustion chamber module

Support

Maintenance, repair and overhaul at MTU Maintenance Hannover

MTU share in the PW2000 program

21.2 %

Applications & Partners


Boeing C-17		Boeing 757

Partners

- Pratt & Whitney (P&W, USA)
- Avio (Italy)
- GKN Aerospace (UK)