Description
A notice of proposed amendment to EASA Part CS-25 is intended to mitigate the safety risk stemming from pilots of large airplanes applying inappropriate rudder control inputs, in particular pedal reversals, which may create structural loads exceeding limits that could lead to the failure of primary structure and/or flight controls. The proposed changes are expected to ensure that large airplanes are designed with features protecting the structure against rudder control pedal reversals like the ones demonstrated in several reported occurrences.
UUID
63