Analysis of turbofan engine performance deterioration and proposed follow-on testsData and engine parts on in-service JT3D and JT8D engines were analyzed and documented relative to engine deterioration. It is concluded that the fan-compressor system of these engines contributes to the long term engine deterioration. An engine test and instrumentation plan was formulated for a proposed follow-on program. The goal of this program is to verify the above conclusion and to attempt to identify more precisely which components of the fan-compressor system are at fault.
Document ID
19750018937
Document Type
Contractor Report (CR)
Authors
Sallee, G. P. (American Airlines, Inc. New York, NY, United States)
Kruckenberg, H. D. (American Airlines, Inc. New York, NY, United States)
Toomey, E. H. (American Airlines, Inc. New York, NY, United States)