To read the full version of this content please select one of the options below:

Air Ministry Official Notices

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 January 1939

Abstract

Cases have been reported where the elevator bias cable of B.A. Swallow II aeroplanes has caught on the rudder pedal securing pin when the bias level is in the rearmost position. This has the effect of making the rudder and elevators stiff to operate, and may lead to an accident.

Citation

(1939), "Air Ministry Official Notices", Aircraft Engineering and Aerospace Technology, Vol. 11 No. 1, pp. 31-31. https://doi.org/10.1108/eb030425

Publisher

:

MCB UP Ltd

Copyright © 1939, MCB UP Limited