Indirect approaches to individual aircraft structural monitoring

Wallace, M., Azzam, H. and Newman, S. (2004) Indirect approaches to individual aircraft structural monitoring Journal of Aerospace Engineering, 218, (5), pp. 329-346. (doi:10.1243/0954410042467059).


Full text not available from this repository.


At present, aircraft structural integrity is maintained by equally applying to an entire fleet knowledge obtained during the design phase and/or from a fleet sample and by introducing conservative assumptions, load surveys, costly inspections and maintenance procedures to safeguard airworthiness. Several investigations have highlighted the significant variations in individual aircraft usage and have indicated the inadequacy of applying "conservative" assumptions and updating the assumptions by monitoring a fleet sample. They have, in addition, suggested the importance of individual aircraft tracking (IAT). IAT can be achieved by fitting each aircraft with strain gauges to monitor critical component loads directly, but maintaining a large number of strain gauges entails high operational costs. Affordable IAT can be achieved by analysing recorded flight parameters to indicate usage, loads and fatigue indirectly. This paper reviews the key investigations into indirect IAT structural monitoring methods.

Item Type: Article
Digital Object Identifier (DOI): doi:10.1243/0954410042467059
ISSNs: 0954-4100 (print)
Keywords: aircraft structural monitoring, individual aircraft tracking (iat), recorded flight parameters
ePrint ID: 22970
Date :
Date Event
Date Deposited: 23 Mar 2006
Last Modified: 16 Apr 2017 22:48
Further Information:Google Scholar

Actions (login required)

View Item View Item