Type: Turbofan, 3-shaft Thrust : 187,000 N (42,000 lb) Compressor: Single-stage fan, 7-stage intermediate pressure, 6-stage high pressure Combustor: Annular chamber Turbine: Single-stage axial high pressure, single-stage intermediate pressure, 3-stage low pressure Weight: 3,267 kg (7,203 lb) Source Smithsonian National Air and Space Museum, National Air and Space Museum Cataloged Imagery Collection, NASM Acc. 1999-0070 Keywords Aviation; Commercial; Engines; Jets; Propulsion Rights and Restrictions CC0
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