EASA has issued proposed airworthiness directive 19-148 for Pilatus PC-12/47Es, requiring inspection, modification and replacement of flap-drive system flap fairings and front inboard tension rods, effective 14 days after airworthiness directive is issued.
EASA has issued proposed airworthiness directive 19-149 for Pilatus PC-24s, requiring replacement and alignment for fuel saddle clamps and motive-flow fuel pipes, effective 14 days after airworthiness directive is issued.
EASA has issued proposed airworthiness directive 19-150 for Fokker F28 Mark 0070s and 0100s, requiring inspection, replacement and modification of main landing gear piston, effective 14 days after airworthiness directive is issued.
EASA has issued airworthiness directive 2018-0249R1for certain Airbus: A330s and A340s, requiring inspection and modification of center wing box fastener holes at frame 40 vertical web, effective August 30, 2019.
EASA has issued airworthiness directive 2019-0188 for certain Airbus A300-600s, A300-600STs and A310s, requiring functional tests of hydraulic reservoir air pressurization system lines, effective Aug 31, 2019.
EASA has issued airworthiness directive 2019-0190 for certain Airbus A300s, requiring functional tests of hydraulic reservoir air pressurization system lines, effective August 31, 2019.
EASA has issued airworthiness directive 2019-0171R1 for certain Airbus A321s, amending aircraft flight manual section limitations, effective August 7, 2019.
EASA has issued airworthiness directive 2019-0189 for certain Airbus A320s, amending aircraft flight manual section limitations, effective Aug 14, 2019.
EASA has issued proposed airworthiness directive 19-151 for Airbus A340-541s, A340-542s, A340-642s and A340-643s, requiring replacement of center landing gear wheel axle, effective 14 days after airworthiness directive is issued.
FAA has issued airworthiness directive 2019-15-05 for all Rolls-Royce Deutschland Trent 1000-AE3s, -CE3s, -D3s, -G3s, -H3s, -J3s, -K3s, -L3s, -M3s, -N3s, -P3s, -Q3s and -R3s, requiring removal of the affected high-pressure turbine disk front cover plate before reaching its new life limit, effective August 16, 2019.
Transport Canada has issued airworthiness directive CF-2010-30R2 for De Havilland DHC-8-400s, DHC-8-401s and DHC-8-402s, requiring conducting a detailed visual inspection and conductivity check on each of the four nacelle attachment fittings and other actions, effective August 13, 2019.
Transport Canada has issued airworthiness directive CF-2014-08R1 for De Havilland DHC-8-400s, DHC-8-401s and DHC-8-402s, requiring a detailed visual inspection of the translating door crank assembly bolts in accordance and other actions, effective August 13, 2019.
