Flying Control Units
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 April 1975
Abstract
AT AN early stage in Hawk design, it was decided that ailerons and tailplane would use hydraulically‐powered flying controls without manual reversion. The flying control control system employs push/pull rods exclusively to transmit pilot demands to the flying control surfaces with friction and backlash reduced to a minimum.
Citation
(1975), "Flying Control Units", Aircraft Engineering and Aerospace Technology, Vol. 47 No. 4, pp. 29-33. https://doi.org/10.1108/eb035241
Publisher
:MCB UP Ltd
Copyright © 1975, MCB UP Limited