Abstract: A method of diagnosing a trailing edge flap fault in an aircraft having a trailing edge flap system including multiple trailing edge flaps, a flap handle for setting the position of the trailing edge flaps, and a flap position sensor, the method includes receiving a position signal, determining a variation in the position signal relative to a reference position, diagnosing a fault, and providing an indication of the diagnosed fault.
Type:
Application
Filed:
October 29, 2013
Publication date:
November 13, 2014
Applicant:
GE Avivation Systems Limited
Inventors:
Christopher Joseph Catt, Julia Ann Howard