FIELD: aircraft engineering.
SUBSTANCE: invention covers a method of controlling at least one means of locking a thrust reversing electric system for a turbomachine, herewith the method is implemented by means of a computing device prior to the aircraft take-off, and the method includes the following stages: sending a command for opening the locking means; checking the locking means opening; sending a command for closing the locking means.
EFFECT: reducing the risk of emergency during the landing phase.
9 cl, 2 dwg
