JTI-CS2-2015-CFP02-SYS-03-01 - Electromechanical actuator for primary moveable surfaces of small aircraft with health monitoring
To test an available EMA up to failure. Based on the evaluation of failure conditions to identify technologies that improve EMA reliability in respect of any failure leading to an uncontrolled EMA position. Health monitoring and any other technology which do not require additional sensors and/or electromechanical devices are preferred. The initial tests have to repeated on the improved EMA to demonstrate compliance with reliability requirements. Please refer to the full and formal topic descriptions published in this call.