Standard Article

Commercial Fixed-Wing Aircraft

  1. Grant A. Gordon1,
  2. Christian Boller2,3

Published Online: 15 SEP 2009

DOI: 10.1002/9780470061626.shm153

Encyclopedia of Structural Health Monitoring

Encyclopedia of Structural Health Monitoring

How to Cite

Gordon, G. A. and Boller, C. 2009. Commercial Fixed-Wing Aircraft. Encyclopedia of Structural Health Monitoring.

Author Information

  1. 1

    Honeywell Inc., Research Technology Centre, Phoenix, AZ, USA

  2. 2

    Saarland University & Fraunhofer Institute for Non-Destructive Testing, Saarbrücken, Germany

  3. 3

    formerly of The University of Sheffield, Sheffield, UK

Publication History

  1. Published Online: 15 SEP 2009

The development history and future opportunities for structural health monitoring in fixed-wing commercial aircraft are described. Starting from an analysis of critical past avionic events, the role of SHM in improving vehicle safety and operational efficiency is examined. Current ideas, requirements, and approaches are explored from the perspective of major large airframe manufacturers and aircraft subsystem manufacturers.

Keywords: aircraft; loads monitoring; damage tolerance; integrated vehicle health monitoring (IVHM)