JT8D-200
JT8D-200
MTU has been a risk-and-revenue sharing partner in this Pratt & Whitney engine program since 1984 and holds a 12.5-percent share. The company manufactures low-pressure turbine blades and parts of various modules for the JT8D-200 engine family.
The engine has a maximum take-off thrust of 97 kN and powers the Boeing MD-80 family of aircraft.

Facts
- Two-shaft turbofan engine
- Single-stage fan
- Six-stage low-pressure compressor
- Three-stage low-pressure turbine
- Seven-stage high-pressure compressor
- Single-stage high-pressure turbine
- Improved sealing systems
- Cooling of the high-pressure turbine
- Exhaust gas mixer
Development
- Modification of the low-pressure turbine
Production
- Low-pressure turbine (various parts)
- High-pressure compressor and high-pressure turbine components
MTU share
- 12.5 %
Partners
- Pratt & Whitney
- Mitsubishi
- GKN Aerospace
Application
- Boeing MD-80
Technical Data
Max. thrust | 21,000 lbf | |
Bypass ratio | 1.74:1 | |
Pressure ratio | 18.2 - 19.4 | |
Length | 168.6 in | |
Max. fan diameter | 54 in | |
Weight | 4,515 lbs |