GE CF34-3A1

Service difficulty reports · 1,372

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF343A1'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA190801004Brake Disc · disintegrated(CAN) WHEN TECHNICIAN TOW THE A/C INTO THE HANGAR, HE SAW BLACK POWDER ON THE GROUND. THE TECHNICIAN FOUND MAIN WHEEL BRAKE ASSY #3 OUTER STATOR & ROTOR DAMAGED. THE BRAKE AND THE WHEEL ASSEMBLIES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. BRAKE SYSTEJul 25, 2019 · Cndair CL6002B16 · Landing Gear Brake SystemSDR SWIA2019071946078Engine · failedLEFT ENGINE FAILURE DURING CLIMB OUT. DECLARED EMERGENCY, COMPLETED QRH, SHUTDOWN LEFT ENGINE IN FLIGHT. (FLT#3780) FO: 07/19/2019 CLOSED REMOVED AND REPLACED LT ENGINE IAW AMM. OPS AND LEAK CHECKS GOOD.Jul 17, 2019 · N868CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA190815007Landing Gear · malfunctioned(CAN) NOSE GEAR DID NOT RETRACT AFTER SELECTING GEAR UP ON TAKE OFF . NOSE LANDING GEAR DOWN WHEN WHEN GEAR DISAGREE WARNING MESSAGE OCCURRED MSG OCCURRED 28 SECONDS AFTER THE HANDLE REMAINED UP AND THE QRH ACTIONED A MANUAL EXTENSION WAS PERFORMED AND THE GEAJul 9, 2019 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA190620001Autopilot Sys · faulted(CAN) FLT CREW EXPERIENCED AN UNCOMMANDED YAW MOTION, FULL DEFLECTION NOSE RIGHT WITH AP ON WHILE CRUISING AT MACH 0.74. MAINTENANCE ACTION: PERFORMED OPS TEST OF THE RUDDER CONTROL SYS AND RUDDER TRIM SYS WITH NO DEFECTS NOTED IAW AMM 27-21-00-710-801 & 802Jun 15, 2019 · Cndair CL6002B19 · Auto Flight SystemSDR CA190529003Director · faulted(CAN) DISPLAY COOL CAUTION MESSAGE. RAN QRH DIDN`T RESOLVE ISSUE ,REMOVED AND REPLACED DISPLAY COOL LOW FLOW EXHAUST SENSOR. (TC# 20190529003)May 25, 2019 · Cndair CL6002B19 · Central DisplaySDR CA190527016Fairing · damaged(CAN) LEFT WINGLET FAIRING DAMAGED DURING FLIGHT DESCENDING THROUGH 14000 FEET. MOST OF THE FAIRING WAS RIPPED OFF IN FLIGHT ALONG WITH THE LIGHTNING PROTECTION KIT. (TC# 20190527016)May 15, 2019 · Cndair CL6002B19 · Wing Main, Frame StructureSDR CA190521026Skin · cracked(CAN) DURING INSPECTION OF THE PASSENGER DOOR INNER SKIN WE HAVE NOTICED 2-OFF CRACKS. (TC# 20190521026)May 13, 2019 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA190522004Skin · corroded(CAN) PAX DOOR INNER SKIN BLENDED TO REMOVE SURFACE CORROSION UNDER CLOSING PLATE REF 601R318059. (TC# 20190522004)May 3, 2019 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA190522001Tire · failed(CAN) ABORTED TAKEOFF AT APPROXIMATELY 90 KTS DUE TO A BURST TIRE. UPON INSPECTION #3 AND #4 MAIN TIRES WERE BURST. NOTHING WAS HIT ON THE RUNWAY DURING THE TAKEOFF ATTEMPT. CORRECTIVE ACTION: REPLACED #3 AND #4 MAIN WHEEL ASSY (TC# 20190522001)May 2, 2019 · Cndair CL6002B19 · TireSDR CA190522005Skin · corroded(CAN) PAX DOOR INNER SKIN BLENDED UNDER ACCESS PANEL 832ER (TC# 20190522005)May 2, 2019 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA190522009Panel · cracked(CAN) PAX DOOR AFT SIDE PANEL CORROSION AND CRACK. CORROSION HAS BEEN BLENDED IN SEVERAL AREAS. 1EA AREA IS DOWN TO .028 MIN. REMAINING. MAT. THK. SRM ALLOWS .029. ALSO 1EA SMALL CRACK AT BOTTOM EDGE OF PANEL ADJACENT TO THE ASSIST MOTOR PULLEY MOUNT.May 2, 2019 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA190425026Frame · corroded(CAN) FRAME AT FS319 BLENDED TO REMOVE CORROSION BETWEEN STGR 25L AND 26L. (TC# 20190425026)Apr 20, 2019 · Cndair CL6002B19 · Fuselage Main, FrameSDR CA190425027Splice Strap · corroded(CAN) FS333 SPLICE STRAP BLENDED TO REMOVE SURFACE CORROSION BETWEEN STGR 25L AND 26L, FWD AND AFT OF THE FRAME AT FS333. (TC# 20190425027)Apr 20, 2019 · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR CA190405014Bpsu · failed(CAN) FLAP FAIL ON DEPARTURE, FLAPS AT 0, LEVER AT 0. COMPLIED WITH QRH. REPLACED FLAP BRAKE POSITION SENSOR UNIT (BPSU) (SEE ALSO FAA SDR #2019090100924/SWIA201904035713) (TC# 20190405014)Apr 3, 2019 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA190403010Floorbeam · corroded(CAN) 1-OFF CORROSION DAMAGE TO FLOOR BEAM OUTBOARD FLANGE DIMENSIONS POST BLEND OUT ARE AS FOLLOWS: 0 1.625`L X 1.090`W X 0.035` MIN. REMAINING THK (0.060` NOM THK, REF) (TC# 20190403010)Apr 1, 2019 · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA190322012Intercostal · corroded(CAN) OPERATOR REPORTS CORROSION DAMAGE TO PAX DOOR INTERCOSTAL (TC# 20190322012)Mar 13, 2019 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA190227008Pressure Switch · failed(CAN) RIGHT WING ANTI ICE CAUTION MESSAGE ON CLIMB OUT (SEE ALSO FAA SDR #2019081703527/SWIA2019022145537) (TC# 20190227008)Feb 21, 2019 · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR CA190225008Windshield · cracked(CAN) UPON DESCENT, WINDSHIELD CRACKED (TC# 20190225008)Feb 19, 2019 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA190220017Stator Vane · worn(CAN) ENGINE ASSY P/N 6078T7G01, WAS INSTALLED. AT 12054 :22 ENGINE HOURS, 11860 CYCLES, AS A PREVENTIVE ACTION, A SPECIAL DETAILED INSPECTION OF COMPRESSOR VARIABLE VANE SPINDLE AXIAL MOVEMENT HAS BEEN PERFORMED USING GUIDELINES AND LIMITS FROM GE HEAVY MAINTFeb 15, 2019 · Cndair CL600* · Turbine Engine Compressor SectionSDR CA180404014Gearbox · damaged(CAN) AIR TURNBACK, N1, N2 AND ITT FLUCTUATION ON CLIMB OUT. CORRECTIVE ACTION: REMOVED AND REPLACED RT THROTTLE GEAR BOX. PERFORMED IDLE SPEED CHECK. PERFORMED POWER ASSURANCE CHECK. OPS CHECKS GOOD. (TC# 20180404014)Apr 1, 2018 · Cndair CL6002B19 · Power LeverSDR SWIA201642426Engine · failedDURING APP BASE LEG RIGHT ENGINE N1 FLUCTUATED AND NOTABLE A/C ENGINE VIBRATION @ 58 N1. VIBRATION STOPPED. DECLARED EMERGENCY WITH ATC. ON TAXI IN ENG TEMP WENT TO MAX TEMP OIL PRESSURE ZERO SHUT ENG DOWN. R&R THE RT ENGINE IAW AMM. OPS CHECK AND LEAK CHAug 7, 2016 · N783CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA201641901Engine · flamed outNR 2 ENGINE FLAMED OUT AFTER TAKEOFF. ATTEMPTED TO RELIGHT ENGINE, UNSUCCESSFUL. CREW DECLARED AN EMERGENCY AND DIVERTED. CABIN WAS BRACED AND THE ACFT LANDED SAFELY. TAXIED TO THE GATE UNDER ITS OWN POWER. R & R RT ENGINE ASSY. OPS CHECKS AND LEAK CHECKS Feb 19, 2016 · N498CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2016021900022Carbon Seal · leakingCREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 6 CARBON SEAL AND PERFORMED CHECKS IAW THE AMFeb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR VNAA2016021900023Carbon Seal · leakingCREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 7 CARBON SEAL AND PERFORMED CHECKS IAW THE AFeb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR CA160126009Skin · cracked(CAN) LEFT WING LOWER PLANK 601R10045-11 DRAIN HOLE AT WS 85.5 BETWEEN S-14 AND S-15 HAS TWO (2) EACH CRACKS. THE FORWARD CRACK EMANATES FROM THE EDGE OF THE DRAIN HOLE TO THE FORWARD AND MEASURES 0.4 INCHES LONG. THE AFT CRACK EMANATES FROM THE EDGE OF THE DRJan 24, 2016 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA160120016Indicator · malfunctioned(CAN) DURING APPROACH GGN7336 CREW REPORTED FLAPS FAILURE TO ATC. WEATHER AT THE TIME INCLUDED LIGHT SNOW SHOWERS. CREW ELECTED TO CONTINUE TO DESTINATION AND PERFORM A FLAPLESS LANDING IN CYYZ AND DECLARE AN EMERGENCY IN ORDER TO HAVE EMERGENCY VEHICLES ON STJan 18, 2016 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA160121013Flap System · failed(CAN) FLAPS FAIL AT 2 DURING APPROACH, QRM ACTIONED, MOC ADVISED. CARRIED OUT RESET OF FLAP SKEW DETECTION SYSTEM CARRIED OUT. LUBRICATION CARRIED OUT. OPERATIONAL TEST CARRIED OUT. OPERATIONAL TEST SKEW DETECTION SYSTEM.Jan 18, 2016 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA160121014Flap System · warning message(CAN) FLAP FAIL MESSAGE ON LANDING, FLAP 0 LANDING CONDUCTED AS PER QRM CARRIED OUT LUBRICATION CARRIED OUT REMOVAL OF FLEX DRIVE SHAFTS CARRIED OUT LUBRICATION OF FLEX DRIVE SHAFTS CARRIED OUT OPERATIONAL TEST OF FLAPS.Jan 18, 2016 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA151221009Control Lever · corroded(CAN) ELEVATOR JAM DUE TO CORRODED ELEVATOR CONTROL LEVERS. SOME OF THE MOVING PARTS IN THIS MECHANISM WERE FOUND STUCK DUE TO CORROSION AND THE ELEVATOR COULD NOT MOVE.Dec 21, 2015 · Cndair CL6002B19 · Elevator Control SystemSDR CA151123008Rotor · failed(CAN) AFTER LANDING, THE PILOT REPORTED RT INBD BRAKE JAM DURING TAXI. THE TECH FOUND 1 OF THE BRAKE ROTORS DESTROYED. THE UNIT WAS INSTALLED LAST WEEK AND OPERATED FOR JUST 53 CYCLES.Nov 23, 2015 · Cndair CL6002B16 · BrakeSDR CA151113003Harness · damaged(CAN) ON TAKEOFF ROLL F/O HAD NO DIRECTIONAL CONTROL, ABORTED TO, THE TERM NO DIRECTIONAL CONTROL MEANT THEY LOST NOSE WHEEL STEERING. REPLACED THE NOSE WHEEL STEERING HARNESS.Nov 11, 2015 · Cndair CL6002B19 · Landing Gear Steering SystemSDR CA151026002Shield · worn(CAN) ON INVESTIGATION OF THE DOOR LOCKING SYS CAUTION MESSAGE ON THE EICAS, IT WAS NOTED THAT THE HINGE SHIELDS ON THE RAILING WERE NOT STAYING INSIDE THE RAILING WHEN THE DOOR WAS CLOSED. THE HINGE SHIELDS ARE IN A POSITION THAT IF THE DOOR WAS TO OPEN AND Oct 22, 2015 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA150916012Fitting · cracked(CAN) COCKPIT WINDSHIELD CENTER POST LT LOWER FITTING CRACK DAMAGE.Sep 15, 2015 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA150908007Skin · cracked(CAN) RT LOWER WING PLANK IS CRACKED AT WS148.019 AFT EDGE. CRACK WAS DISCOVERED WHILE PERFORMING S/B 601R-57-031 FOR THE INSPECTION OF THE LOWER WING PLANKS IN THE AREA OF THE JACK POINT FITTINGS.Sep 3, 2015 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA150809002Priority Valve · failed(CAN) AFTER T/O NOSE GEAR WOULD NOT COME UP. RECEIVED A GEAR DISAGREE WARNING MSG THEN NOSE GEAR RETRACTED ON ITS OWN AFTER A FEW MORE SECONDS.Aug 6, 2015 · Cndair CL6002B19 · Hydraulic System, MainSDR CA150730013Tire · separated(CAN) AFTER LANDING, FLIGHT CREW DURING WALK AROUND INSPECTION NOTICED THAT NR 3 TIRE WAS MISSING A STRIP OF RUBBER, APPROXIMATELY 18" LONG X 4" WIDE. TIRE PRESSURE WAS VERIFIED, AT HOME BASE THE SAME DAY.Jul 29, 2015 · Cndair CL6002B16 · TireSDR CA150728009Selector Valve · failed(CAN) ON LANDING APPROACH COMING INTO THE AIRPORT, UPON LANDING GEAR SELECTED DOWN IT WAS INDICATED THAT THERE WAS A PROBLEM WITH THE NOSE GEAR. THE PILOTS FLEW A GO AROUND AND DECLARED AN EMERGENCY, THE GEAR CAME DOWN SUCCESSFULLY WHEN THE ALTERNATE EXTENSIONJul 24, 2015 · Cndair CL6002B19 · Landing Gear SelectorSDR CA150724002Handle · failed(CAN) AFTER MLG SYSTEM COMPONENT REPLACEMENT, ROUTINE GEAR SWINGS WERE CARRIED OUT ON AIRCRAFT. DURING ALTERNATE EXTENSION FUNCTION TEST, IT WAS DISCOVERED THAT THE ALTERNATE EXTENSION CONTROL HANDLE ASSEMBLY DID NOT OPERATE CORRECTLY. THE CONTROL HANDLE WAS BJul 20, 2015 · Cndair CL6002B19 · Landing Gear SelectorSDR CA150713017Actuator · failed(CAN) ON APPROACH GEAR DISAGREE W, UPON LG EXTENSION SELECTION WITH RT MLG UNLOCKED INDICATION. LG RECYCLED & ALL DOWN LOCKED INDICATIONS OK. REPLACED RT MLG SIDE STAY ACTUATOR. ACFT RTS.Jul 2, 2015 · Cndair CL6002B19 · Landing Gear ActuatorSDR CA150602017Quick Disconnect · disconnected(CAN) DURING LANDING GEAR RETRACTION FOLLOWING MESSAGES APPEARED: NOSE DOOR OPEN GEAR DISAGREE WOW INPUT CAUTION MSG WOW OUTPUT FAIL THE CAPTAIN MADE THE EMERGENCY PROCEDUCE: GEAR DOWN IN EMERGENCY, AND EVERYTHING OK. AFTER LANDING, APPEARS NO STEERING MSG ANMay 31, 2015 · Cndair CL6002B19 · Nose/Tail Landing GearSDR CA150519027Disk · disintegrated(CAN) UPON LANDING, 2 ROTATING DISKS OF NR 4 BRAKE ASSEMBLY HAVE DISINTEGRATED INTO FRAGMENTS. MAINTENANCE PERSONEL REPLACED THE ASSY TO CORRECT THE SITUATION AND REPLACED THE BRAKE CONTROL VALVES AND THE AFFECTED WHEEL ASSY AS PREVENTIVE MAINTENANCE.May 16, 2015 · Cndair CL6002B16 · Landing Gear Brake SystemSDR CA150312002Line · worn(CAN) DURING INSPECTION, FULE LINES IN THE LT WING TANK AT BS, LBL 22.50 DAMAGE TO PIPE ASSY AND RIB SUPPORT STRUCTURE WAS FOUND. WHILE IN AN UNLOADED CONDITION THE PIPE ASSY AND THE RIB SUPPORT STRUCTURE THERE IS APPROXIMATELY .5" OF CLEARANCE. THE PIPE ASSMar 12, 2015 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR CA150112010Transmitter · failed(CAN) IAS HI SPEED Q POPPED OUT AND THE ACFT STARTED TO CLIMB. FLAPS WERE MOVING UNCOMMANDED WITH FLAP HANDLE AT 0,FROM 0-2,0-8, 0-20. HYD 2B AND 3B CAUTION MSGS. AFTER APPROX. 3 CYCLES OF FLAP EXTENSION INDICATION FLAPS DEGRADED STATUS MSG APPEARED. FLAP PJan 7, 2015 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA141215012Wire · chafed(CAN) AFTER TOUCHDOWN, THE RIGHT THRUST REVERSER DEPLOYED WHEN COMMANDED BUT THE CREW WAS UNABLE TO STOW IT. ON THE SAME TIME, NO LIGHTS WERE SHOWN ON T/R CONTROL PANEL (UNSAFE, ARMED, REVERSER UNLOCKED) ON THE LEFT THRUST REVERSER. THE MAINTENANCE PERSONNEL Nov 28, 2014 · Cndair CL6002B16 · Instrument System WiringSDR CA141008018Throttle Cable · broken(CAN) LOSS OF CONTROL OF LEFT THROTTLE ON CLIMB OUT. MAINTENANCE FOUND LEFT THROTTLE CABLE TO THROTTLE GEAR BOX BROKEN.Oct 4, 2014 · Cndair CL6002B19 · Power LeverSDR VNAA2014083000019Skin · dentedDURING SCHEDULED MAINTENANCE, THE RT ENGINE TRANSLATING COWL HAD TWO DENTS. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.Aug 30, 2014 · N228PS · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR CA140821003Proximity Switch · failed(CAN) AT TAKEOFF, CREW SELECTED GEAR UP. THE MAIN GEAR RETRACTED AS NORMAL BUT THE NOSE GEAR FAILED TO RETRACT. INDICATIONS SHOWED NOSE GEAR STILL DOWN AND LOCKED. CREW SELECTED GEAR DOWN ALL GEAR EXTENDED AND INDICATED DOWN AND LOCKED. THE ACFT LANDED WITHAug 19, 2014 · Cndair CL6002B16 · Landing Gear Position and WarningSDR CA160219006Floor Skin · cracked(CAN) FOUND CRACKS LOCATED ON PRESSURE FLOOR STRUCTURE BS 461.5 BETWEEN RBL 9 AND LBL 9Jul 29, 2014 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2014062338265Bushing · galledLEFT ENGINE, YOKE MOUNT LINK BUSHINGS ARE GALLED. R & R LT ENGINE YOKE LINK IAW AMM.Jun 21, 2014 · N779CA · Cndair CL6002B19 · Engine Mount SectionSDR SWIA2014062338266Pin · scoredLEFT ENGINE, YOKE MOUNT PINS AND BOLTS SCORED. R & R LT ENGINE FWD YOKE MOUNT PINS AND BOLTS IAW AMM.Jun 21, 2014 · N779CA · Cndair CL6002B19 · Engine Mount Section
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