This paper presents a five-phase switched reluctance motor designed to satisfy the requirements of flap actuators in medium size aircrafts. In normal operation the machine operates with two-phases conducting simultaneously but it is designed to satisfy the load specifications also with one or two phases faulted. The finite-element studies aiming to predict the faulty mode performance are presented. Experimental tests on the motor prototype are included, which confirm its capability to satisfy the planned degraded modes of operation. Professor of Electrical Machines Design for the degree of Engineering at the University of L'Aquila. His research interests are focused on modeling and simulation of electrical machines, energy saving in electric motors, optimization techniques for the electrical machines design, design of PM synchronous motors and Reluctance motors. He is author of more than 100 technical papers in scientific journals and conference proceedings.Marco Tursini (M'99) received the M.S. degree in electrical engineering from the University of L'Aquila, in 1987. In the same year he where he conducted research on sliding-mode control of permanent-magnet synchronous motor drives, in 1990 and with Nagasaki University, Nagasaki, Japan, in 1994. Since 1990, he has taken responsibility for several national research projects and contracts between the University of L'Aquila and industrial partners. His research interests are focused on advanced control of ac drives, including vector, sensorless, and fuzzy logic control, digital motion control, DSP-based systems for real-time implementation, and modeling and simulation of electrical drives. He has authored more than 110 technical papers on these subjects.Giuseppe Fabri was born in Rieti, Italy, on January 24, 1982. He received the M.S. degree in electronic engineering and the Ph.D. degree in electrical and information engineering from the University of L'Aquila, L'Aquila, Italy, in 2009 and 2013, respectively. He is currently with the University of L'Aquila. His research activities involve development, control, and test of electrical motor drives mainly related to fault-tolerant systems for aircraft and automotive applications. In particular, he has experience in design of power electronics and DSP-based control platforms along with related integration of motion control algorithms for ac drives. His interests also cover rapid prototyping techniques and realtime simulation systems.Lino Di Leonardo was born in Pescina, Italy, on October 28, 1986. He received the M.S. degree in Computer and Automation Engineering in 2010 and is currently a Ph.D. student in electrical and information engineering at University of L'Aquila. In particular his Ph.D. thesis concerns dynamic co-simulation analysis of motor drives. His research activities involves design, modeling and simulation of electrical machines with focus on permanent-magnet synchronous motors, Dual-Rotor Permanent Magnet Induction Machine and reluctance motors. He has experience with finite-element and multi-physics i...