Aircraft Maintenance Management Part 2
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1993
Abstract
It is noted that the probability of dual engine failure from all independent causes in cruise must not exceed 0.3 x 10−8 per hour.
Citation
Middleton, D.H. (1993), "Aircraft Maintenance Management Part 2", Aircraft Engineering and Aerospace Technology, Vol. 65 No. 1, pp. 10-12. https://doi.org/10.1108/eb037330
Publisher
:MCB UP Ltd
Copyright © 1993, MCB UP Limited