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JT9D engine diagnostics. Task 2: Feasibility study of measuring in-service flight loadsThe feasibility of measuring JT9D propulsion system flight inertia loads on a 747 airplane is studied. Flight loads background is discussed including the current status of 747/JT9D loads knowledge. An instrumentation and test plan is formulated for an airline-owned in-service airplane and the Boeing-owned RA001 test airplane. Technical and cost comparisons are made between these two options. An overall technical feasibility evaluation is made and a cost summary presented. Conclusions and recommendations are presented in regard to using existing inertia loads data versus conducting a flight test to measure inertia loads.
Document ID
19780019181
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kafka, P. G.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Skibo, M. A.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
White, J. L.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
October 15, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-135395
D6-44664
Accession Number
78N27124
Funding Number(s)
CONTRACT_GRANT: NAS3-20632
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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