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Study of turboprop systems reliability and maintenance costsThe overall reliability and maintenance costs (R&MC's) of past and current turboprop systems were examined. Maintenance cost drivers were found to be scheduled overhaul (40%), lack of modularity particularly in the propeller and reduction gearbox, and lack of inherent durability (reliability) of some parts. Comparisons were made between the 501-D13/54H60 turboprop system and the widely used JT8D turbofan. It was found that the total maintenance cost per flight hour of the turboprop was 75% higher than that of the JT8D turbofan. Part of this difference was due to propeller and gearbox costs being higher than those of the fan and reverser, but most of the difference was in the engine core where the older technology turboprop core maintenance costs were nearly 70 percent higher than for the turbofan. The estimated maintenance cost of both the advanced turboprop and advanced turbofan were less than the JT8D. The conclusion was that an advanced turboprop and an advanced turbofan, using similar cores, will have very competitive maintenance costs per flight hour.
Document ID
19800005872
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
June 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
EDR-9132
NASA-CR-135192
Report Number: EDR-9132
Report Number: NASA-CR-135192
Accession Number
80N14129
Funding Number(s)
CONTRACT_GRANT: NAS3-20057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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