EASA has issued proposed airworthiness directive 19-119 for Airbus A350-1041s and A350-941s, requiring inspection of main landing gear forward pintle bearing lock washer tabs and nuts, effective 14 days after airworthiness directive is issued.
EASA has issued airworthiness directive 2018-0076R1 for Fokker F28 Mark 0070s, 0100s, 1000s, 2000s, 3000s and 4000s, requiring replacement of landing gear hydraulic line T-union, effective July 17, 2019.
EASA has issued airworthiness directive 2019-0162 for Fokker F28 Mark 0070s and 0100s, requiring inspection of fuselage bottom skin, effective July 24, 2019.
EASA has issued airworthiness directive 2019-0163 for Fokker F27 Mark 050s, 0502s and 0604s, requiring inspection of horizontal stabilizer rear spar attachment angles, effective July 25, 2019.
EASA has issued proposed airworthiness directive 19-123 for Airbus A350-1041s and A350-941s, requiring inspection of trimmable horizontal stabilizer fittings and bearing assembly attachment interface to fuselage, effective 14 days after airworthiness directive is issued.
EASA has issued airworthiness directive 2019-0164 for certain Airbus A330s and A340s, requiring inspection and replacement of landing gear free fall actuators, effective July 25, 2019.
EASA has issued airworthiness directive 2014-0197R1 for Airbus A330-223Fs and A330-243Fs, requiring inspection and repair of frame and stringer attachments, effective July 18, 2019.
FAA has issued airworthiness directive 2019-12-08 for certain Bombardier CRJ 705s, 900s and 1000s, requires replacement of certain aft fuselage fittings with correctly manufactured parts, an eddy current inspection of certain fastener holes for cracking and corrective actions if necessary, effective August 12, 2019.
FAA has issued airworthiness directive 2019-12-16 for certain Airbus A350-941s, requiring replacing the original diagonal struts at a certain frame with new, improved parts, as specified in an EASA airworthiness directive, effective July 23, 2019.
FAA has issued airworthiness directive 2019-12-17 for certain Bombardier DHC-8-102s, -103s and -106s, DHC-8-200s and DHC-8-300s, requiring inspecting two elevator spring tab balance weights and the two hinge arms on each elevator spring tab, and corrective actions if necessary, effective August 12, 2019.
FAA has issued airworthiness directive 2019-12-09 for certain part-numbered Rockwell Collins FDSA-6500 flight display system applications, imposing operating limitations on the traffic collision avoidance system by revising the limitations section of the airplane flight manual or supplement and installing a placard on each aircraft primary flight display, effective July 23, 2019.
