Summary
The FAA proposes to supersede Airworthiness Directive (AD) 2017-19-08 and AD 2018-19-02, which apply to Airbus Defense and Space S.A. Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, and C-212-DF airplanes. AD 2018-19-02 requires repetitive inspections of the rudder pedal control system support box and shaft and applicable corrective actions; accomplishing those actions terminates the requirements of AD 2017-19-08. Since AD 2018-19-02 was issued, the FAA has determined that a modification must be done in order to address the unsafe condition. This proposed AD would continue to require repetitive inspections and applicable corrective actions; this proposed AD would also require a modification of the rudder pedal adjustment system; as specified in a European Union Aviation Safety Agency (EASA) AD, which will be incorporated by reference. The FAA is proposing this AD to address the unsafe condition on these products.