Post-Cold War political and economic considerations have resulted in effort
s to extend the life of many aircraft that are the backbone of NATO operati
onal forces. Although some are designated to be replaced with new aircraft,
the replacement schedule for many often requires an unprecedented life spa
n of up to 80 years before retirement. Aircraft within these older fleets h
ave had, and continue to experience with growing frequency, fatigue and cor
rosion related cracking problems that are of concern to operators. To susta
in their airworthiness and reduce the maintenance burden, structural compon
ents undergoing these aging problems will have to be repaired or replaced.
Material development that has taken place since most of the older vintage m
ilitary aircraft entered service has resulted in improved alloys and proces
ses that can be used to upgrade life expectation, performance, and affordab
ility of older systems. Some of these newer materials and the advantages th
ey offer over their older counterparts are described.