Abstract
The philosophy as developed by Fokker with regard to the structural maintenance is presented. The maintenance schedules have always included a part with a mandatory character: the Structural Integrity Program (SIP). In this document the stress corrosion aspect is also covered.
As a result of the first FAA aging aircraft conference a Fokker/Piedmont-USAir Task Group was formed for the F28, resulting in a maintenance review activity. The first meeting of the Task Group was in March 1989.
The objectives of the Task Group are presented.
The review is now in the final stage. The last meeting is scheduled in May 1990.
The paper discusses the results of the review as far as these are available and closes with a number of conclusions.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1991 Springer-Verlag Berlin, Heidelberg
About this paper
Cite this paper
Roll, R., van Dalen, A., Jongebreur, A.A. (1991). Results of Review of Fokker F 28 “Fellowship” Maintenance Program. In: Atluri, S.N., Sampath, S.G., Tong, P. (eds) Structural Integrity of Aging Airplanes. Springer Series in Computational Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-84364-8_21
Download citation
DOI: https://doi.org/10.1007/978-3-642-84364-8_21
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-84366-2
Online ISBN: 978-3-642-84364-8
eBook Packages: Springer Book Archive