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Flight service evaluation of Kevlar-49 epoxy composite panels in wide-bodies commercial transport aircraftKevlar-49 fairing panels, installed as flight service components on three L-1011s, were inspected after 9 years of service. There are six Kevlar-49 panels on each aircraft: a left hand and right hand set of a wing body sandwich fairing; a solid laminate under wing fillet panel; and a 422 K (300 F) service aft engine fairing. The fairings have accumulated a total of 70,000 hours, with one ship set having over 24,000 hours service. The Kevlar-49 components were found to be performing satisfactorily in service with no major problems, or any condition requiring corrective action. The only defects noted were minor impact damage, a few minor disbonds and a minor degree of fastener hole fraying and elongation. These are for the most part comparable to damage noted on fiberglass fairings. The service history to date indicates that Kevlar-49 epoxy composite materials have satisfactory service characteristics for use in aircraft secondary structure.
Document ID
19840002121
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stone, R. H.
(Lockheed Corp. Burbank, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-166065
NAS 1.26:166065
AFSR-9
Report Number: NASA-CR-166065
Report Number: NAS 1.26:166065
Report Number: AFSR-9
Accession Number
84N10188
Funding Number(s)
CONTRACT_GRANT: NAS1-11621
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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