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Ten years of flight service with DC-10 composite rudders - A backward glanceCarbon-epoxy upper aft rudders have been successfully evaluated on the DC-10 during 10 years of airline flight service. They have flown for more than 320,000 flight hours, with 36,000 flight hours flown by a single rudder. The rudder box is of thin-skin buckled construction and is cocured out-of-autoclave as a one-piece assembly. Weight saving can exceed the rudder weight if full advantage is taken of removing balance weight from the forward rudder.
Document ID
19870042369
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hawley, Arthur V.
(Douglas Aircraft Co. Long Beach, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 861674
Accession Number
87A29643
Distribution Limits
Public
Copyright
Other

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