GE CF34-3A1

Service difficulty reports · 1,372

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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 CA061205002Flap · malfunctioned(CAN) AT APROX 2500-3000 FT ON FINAL APPROACH THE CREW RECEIVED A FLAP FAIL MESSAGE. THE QRH WAS FOLLOWED AND THE FLAPS WERE INDICATING AT 30 DEGREES. THE CREW LANDED WITHOUT INCIDENT AND PERFORMED A CIRUIT BREAKER REST AND THE FLAPS RETURNED TO ZERO. FLT TO Dec 4, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA061211006Line · broken(CAN) RT AIR CONDITIONING PACK WAS DEFERRED AND CREW HAD TO SHUTDOWN APU ON APPROACH BECAUSE OF OIL/FUEL ODOR IN THE CABIN. CREW REPORTED A PRESSURE BUMP WHEN APU WAS SHUTDOWN. APU WAS SUSPECTED TO BE OVER SERVICED, BUT EVEN AFTER DRAINING A LITRE OF OIL APUDec 3, 2006 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CA061206002Bolt · misinstalled(CAN) LT ELEVATOR, FOUND NUT/BOLT COMBINATION INCORRECTLY INSTALLED ON LT NR 1 PCU JAM TOLERANT MECHANISM. AIRFRAME HOURS: 25355:05. CYCLES: 20701. (TC NR 20061206002)Dec 2, 2006 · Cndair CL6002B19 · Elevator StructureSDR CA061212004Windshield · cracked(CAN) DURING CRUISE CAPTAIN’S FRONT WINDSHIELD SHATTERED. (NO PRESSURIZATION LOSS). CREW DECLARED EMERGENCY AND DESCENDED TO 10000 FT AND DIVERTED TO NEAR BY ALTERNATE AIRPORT. MAINTENANCE REPLACED WINDSHIELD AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20061212Dec 2, 2006 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0660650Engine · overservicedFLIGHT 9465 - LEFT ENGINE OIL PRESSURE 24-29 PSI. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. FOUND ENGINE TO BE OVERSERVICED. SERVICED TO PROPER LEVEL.Nov 24, 2006 · N804CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA061118001Engine · bird ingestion(CAN) AFTER GEAR-UP SELECTION THE AIRCRAFT ENCOUNTERED A VIBRATION, FELT THROUGHOUT ENTIRE PLANE,THAT WOULD INCRESE/DECREASE WITH THROTTLE MOVEMENT. AIRCRAFT RETURNED TO THE ORIGINATING DEPARTURE STATION AND LANDED SAFELY. MAINTENANCE FOUND NR 1 ENGINE FAN BLANov 17, 2006 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA061218017Gearbox · stiff(CAN) PILOT REPORTED LT POWER LEVER STIFF TO MOVE AS COMPARED TO RT. TROUBLESHOOTING REVEALED THAT INPUT SHAFT ON GEARBOX ATTACHED, (COULD BARELY BE RETACTED BY HAND). SB601-0583 (TC NR 20061218017)Nov 17, 2006 · Cndair CL6002B16 · Power LeverSDR COMA0660601Actuator · faultyENROUTE, RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS SELECTED AT 8 DEGREES. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RT WING IB-OB FLAP ACTUATOR.Nov 3, 2006 · N786CA · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0660608Actuator · faultyENROUTE, RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS SELECTED AT 8 DEGREES. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RT WING OB-OB FLAP ACTUATOR.Nov 3, 2006 · N786CA · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA061107011Check Valve · failed(CAN) THE CREW REPORTED THAT ON DESCENT THEY HAD PRESSURIZATION PROBLEMS. DURING THE DESCENT THEY GOT AUTO PRESS1 AND AUTO PRESS 2 FAIL AND MASKS DEPLOYED AND WERE USED. ALSO LT PACK HAD A BLOWN DUCT. LH PACK AIR CONDITIONING DUCT P/N601R895211-113 REPLACED BONov 3, 2006 · Cndair CL6002B19 · Cabin Pressure Control SystemSDR CA061101002Clamp · burned(CAN) ELECTRICAL ARC BURN MARKS FOUND ON THE REAR FACE OF NUTPLATES (QTY 17) FOR THE WING FUEL TANK ACCESS DOORS. AS PER THE TECHNICAL RECORDS THERE WERE TWO REPORTED LIGHTNING STRIKES ON THIS AIRCRAFT SINCE NOVEMBER 09/2005. THE BURN MARKS ARE A LIKELY INDICOct 30, 2006 · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA200617355Window · crackedLT WINDOW CRACKED, FERRIED TO SLC, REPLACED LT WINDOW IAW RII 52-220-1000 AND IAW MM 56-12-01. LEAKS, OPERATIONAL CHECKS GOOD. SN OFF: 03063H7733.Oct 25, 2006 · N461SW · Cndair CL6002B19 · Flight Compartment WindowsSDR CA061017006Gearbox · failed(CAN) LEFT ENGINE IN-FLIGHT SHUTDOWN DUE TO ACCESORIES GEARBOX (AGB)FAILURE. AGB BORESCOPE INSPECTION REVEALED A BROKEN GEAR. AIRFRAME HOURS=25499:54. CYCLES=21133. (TC# 20061017006)Oct 13, 2006 · Cndair CL6002B19 · Accessory GearboxesSDR CA061206001Flap System · malfunctioned(CAN) ON APPROACH FLAPS SELECTED TO 8 DEG, FLAP DID NOT TRAVEL AND (FLAP FAIL) MESSAGE DISPLAYED. NORMAL FLAP ZERO LANDING . AFTER LANDING , FLAP CIRCUIT BREAKER RESET PROCEDURE CARRIED OUT . FLAPS INSPECTED AND NO FAULTS FOUND. FLAPS CYCLED WITH NO FAULTS Oct 11, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0660556Floorbeam · crackedANGLE BRACKET AT FS 484.00 RBL36 MARKED IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET CLIP IAW REO 601R-53-41-059.Sep 28, 2006 · N784CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA060925005Screen · failed(CAN) ABOUT 50 NM EAST AND AT FL330 THE CREW REPORTED LT ENG OIL PRESSURE WARNING LIGHT WITH FLUCTUATING LOW OIL PRESSURE READINGS (20-46PSI) AT IDLE POWER LT OIL TEMP WAS INCREASING. THE CREW ELECTED TO SHUT DOWN THE LT ENGINE. LINE MAINTENANCE REMOVED LT ENSep 22, 2006 · Cndair CL6002B19 · Engine Oil PressureSDR CA060919004Visor · cracked(CAN) BOTH THE LT AND RT LOWER VISOR ASSEMBLIES WERE FOUND DAMAGED FROM CRACKING AT THE AFT TOP END. THIS MAY HAVE BEEN DUE TO FLUTTER AT THE AFT END OF THE FAIRING DURING FLIGHT. SINCE IT IS ATTACHED TO THE MOVABLE HORIZONTAL STABILIZER, THERE IS NO FASTENERSep 17, 2006 · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR CA060918009Track · cracked(CAN) NR 2 ENGINE LT LOWER THRUST REVERSER TRACK FOUND CRACKED DURING A C-CHECK INSPECTION. PART REPLACED AS A MAIN TRACK ASSEMBLY P/N 228-50809-801. REFERENCE :MFG CSP A-006 IPC CHAP 78-34-11 FIGURE 1 , ITEM 75A AND 95A. (TC NR 20060918009)Sep 16, 2006 · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0660464Engine · false indicationFLIGHT 9498- DURING TAKEOFF ROLL, THE LEFT ENGINE ITT ROSE ABOVE 900 DEGREES, CREW ABORTED TAKEOFF AND FLIGHT RETURNED TO THE GATE. PERFORMED GROUND RUNS OF THE LEFT ENGINE, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.Jul 31, 2006 · N999CA · Cndair CL6002B19 · Turbine Engine Combustion SectionSDR COMA0660436Engine · malfunctionedFLIGHT 5015 - NR 2 ENGINE ROLLED BACK TO SHUTOFF DURING LIGHTNING STRIKE, CREW DECLARED AN EMERGENCY. RESTARTED THE RIGHT ENGINE AND FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE.Jul 13, 2006 · N920CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA060801003Ballast · odor(CAN) DURING PASSENGER BOARDING AND UPON ENTRY TO FLIGHT DECK A STRONG ELECTRICAL SMELL WAS APPARENT AND PROGRESSIVELY GOT WORSE. PASSENGERS WERE DE-PLANED. LINE MAINTENANCE CREW FOUND FORWARD BOARDING LIGHT BALLAST P/N BR9000-2 BURNED. THE BURNED BALLAST WAS Jul 13, 2006 · Cndair CL6002B19 · Passenger Compartment LightingSDR COMA0660379Engine · malfunctionedFLIGHT 5205 - EN ROUTE MCO-MCI ENCOUNTERED A BRIEF VIBRATION AND LOSS OF POWER ON NR 1 ENGINE. CREW DECLARED AN EMERGENCY, DIVERTED TO TLH WITH SINGLE ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE ASSEMBLY.Jun 5, 2006 · N927CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA060607003Engine · failed(CAN) DURING CLIMB AT 2000 FT THE NR1 ENGINE FAILED, N1 DROPPED OFF AND TGT PEGGED. EMERGENCY WAS DECLARED AND AC RETURNED AND LANDED SAFELY. THIS REPORT IS INITIAL ONLY, FURTHER INFORMATION WILL BE FORWARDED ON RECEIPT OF THE TEARDOWN REPORT FROM THE MANUFACJun 4, 2006 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA060605004Thrust Reverser · failed(CAN) FLIGHT CREW REPORTED THAT THEY RECEIVED A (L REV UNLOCKED) CAUTION MESSAGE ON RUNWAY AND LINED UP FOR TAKEOFF WITH NO REPORTED CHANGE TO THE N1 OR N2 INDICATIONS. MESSAGE THEN FLICKERED ON AND OFF. WHILE TAXIING BACK TO THE GATE THE MESSAGE WENT OUT. AFJun 3, 2006 · Cndair CL6002B19 · Engine Thrust ReverserSDR CA060604002Apu · inoperative(CAN) WHILE TAXING IN PREPARATION FOR TAKEOFF, CREW NOTED SMOKE AROUND AC, TOWER REPORTED SMOKE, FLAMES COMING FROM AFT AREA OF AC UNDER NR 2 ENG. APU WAS SHUTDOWN, CREW THEN ELECTED TO TAXI OFF ACTIVE TAXIWAY TO A NON ACTIVE TAXIWAY. SHORTLY AFTER STOPPING AMay 25, 2006 · Cndair CL6002B19 · APU Core EngineSDR CA060515001Panel · missing(CAN) DURING FLT NR 1 ENG NOSE COWL LWR ACCESS PNL DEPARTED AC (ACCESS PNL). FLIGHT EXPERIENCED A SLIGHT BUFFET DURING FLT. UPON LANDING, FLT CREW DISCOVERED NOSE COWL LWR ACCESS PNL WAS MISSING. DAMAGE TO TRANSLATING COWL, UPPER NOSE COWL ACCESS PNL, CAUSED May 10, 2006 · Cndair CL6002B19 · Engine Cowling SystemSDR RU32006F00001Wing · scratchedUPON POST FLT, DISCOVERED STRATCHES ON RT WINGLET. APPARENTLY WHILE POSITIONING OVER GCP AT RKTP, SCRAPED GCP SIGN. NO INDICATION OF CONTACT WHILE AT RTKP. RETURNED TO RKSO WHERE DAMAGE WAS NOTED. PERFORMED TEMP REPAIR REFERENCE REO. (K)Apr 17, 2006 · N87 · Cndair CL6002B16 · Wing, Plate/SkinSDR COMA0660293Oil System · lowFLIGHT 9470 - EN ROUTE BOS-CVG RECEIVED A LEFT ENGINE OIL PRESSURE WARNING MESSAGE, PRESSURE FLUCTUATED BETWEEN 27 AND 45 PSI, FLIGHT DIVERTED TO PIT. DEFERRED THE OIL REPLENISHING SYSTEM PER MEL 79-12-01.Apr 6, 2006 · N804CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA060403020Elbow · split45 DEGREE UNIVERSAL ELBOW FITTING FOUND SPLIT WITH HYDRAULIC FLUID LEAKAGE ON THE NR 2 HYDRAULIC SYSTEM, IPC 29-11-00, FIG 20, VIEW K, ITEM NR 45. FITTING REPLACED WITH THE SYSTEM CHECKED SERVICEABLE.Apr 2, 2006 · Cndair CL6002B19 · Hydraulic System, MainSDR CA060405004Fastener · shearedHI-LIGHT FASTENERS (P/N HST22DU5-22) THAT ATTACHES LINKS (P/N 601R24056-55) TO FITTINGS (P/N 601R24056-51 ON LT AND FITTINGS P/N 601R24056-49 ON THE RT ELEVATOR), FOUND WITH SHEARED HEADS.Mar 31, 2006 · Cndair CL6002B19 · Elevator Control SystemSDR CA060404006Bushing · wornON DEPARTURE (200 KTS GEAR UP FLAPS 0), A LOW FREQUENCY VIBRATION WAS FELT THROUGH THE AIRCRAFT, BOTH FLIGHT DECK AND CABIN. VIBRATION WAS NOTICEABLE ENOUGH TO SHAKE SEATS SIDE TO SIDE, ENGINE FAN VIBRATION 0.2 AND 0.5, SMOOTH AIR FLIGHT CONDITIONS. CHECKED Mar 23, 2006 · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR COMA0660149Pump · faultyFLIGHT 5682- EN ROUTE PWM-CVG RECEIVED A LEFT ENGINE OIL PRESSURE WARNING, FLIGHT DIVERTED TO CAK. REPLACED THE LEFT ENGINE OIL LUBRICATION PUMP.Feb 14, 2006 · N594CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA060309001Switch · failed(CAN) ON DEPARTURE, THE FLIGHT CREW REPORTED THEY HAD LOST THE AUTOPILOT, MACH TRIM AND THE STAB TRIM. NR 1 STAB TRIM SWITCH WAS NOTICED TO BE STICKY AND HARD TO DISENGAGE. THE CREW WAS ADVISED THAT IT WAS PROBABLY THE NR 1 (CAPT'S) DISENGAGE SW (P/N 996-0013Feb 8, 2006 · Cndair CL6002B19 · Autopilot SystemSDR CA060211002Window · cracked(CAN) THE COPILOT SIDEWINDOW CRACKED IN DESCENT. WINDOW REPLACED, AIRCRAFT RELEASED TO SERVICE. (TC NR 20060211002)Feb 7, 2006 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA060124006Fuel Control · unserviceable(CAN) NR 1 ENGINE FAILED TO START WITH IGNITION OPERATING NORMALLY. 5 ATTEMPTS WERE MADE BY THE FLIGHT CREW. GROUND PERSONNEL NOTED EXTREME AMOUNT OF FLAMES COMING FROM THE JETPIPE AND ADVISED FLIGHT CREW. FUEL CONTROL SN WYG85082 REPLACED, ENGINE GROUND RJan 18, 2006 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA060117002Duct · failedL14TH DUCT MSG ON DESCENT. ACTIONED CHECKLIST AND SHUTDOWN ENGINE. CHANGED DETECTOR ELEMENT A59WK. OP TEST CARRIED OUT IAW AMM SERV.Jan 17, 2006 · Cndair CL6002B19 · Turbine Engine Combustion SectionSDR COMA0560759Skin · corrodedAFT WING PLANK, FUEL BOOST PUMP SATELLITE HOLE NR 7 HAS CORROSION DAMAGE. INCORPORATED REPAIRS IAW REO 601R-57-21-169 REV B.Dec 31, 2005 · N927CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0560789Skin · dentedRT WING SKIN DENTED 1 INCH DIA BY .030 DEEP AT WS 252.8. REPAIRED RT WING SKIN AT WS 252.8 BY BLENDING DAMAGED AREA, PERFORMED EDDY CURRENT ROTO PEN AND TOUCHED UP REWORK AREA IAW REO 601R-57-21-671.Dec 31, 2005 · N927CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0560753Seat Track · corrodedFLOOR SEAT RAIL CORRODED FROM FS363 TO 398. REPAIRED LT FWD SEAT TRACK FROM FS363 TO 398 BY REMOVING AND REPLACING SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.Dec 30, 2005 · N927CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR COMA0560754Seat Track · corrodedFLOOR SEAT RAIL CORRODED FROM FS363 TO 398. REPAIRED RT FWD SEAT TRACK FROM FS363 TO 398 BY REMOVING AND REPLACING SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802.Dec 30, 2005 · N927CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR COMA0560758Seat Track · corrodedFLOOR SEAT RAIL CORRODED FROM FS 399.50 TO FS 409+126. REPAIRED LT FLOOR SEAT RAIL FROM FS399.50 TO FS409+126 BY REMOVING AND REPLACING TRACK IAW BRAS EO 601R-53-7965A.Dec 30, 2005 · N927CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR COMA0560788Seat Track · corrodedRT SIDE SEAT RAIL FROM FS 535.02 TO 559.79. REPAIRED RT SIDE SEAT RAIL FROM FS 535.02 TO 559.79 BY REMOVING AND REPLACING SEAT RAIL IAW MFG EO 601R-53-7965A.Dec 30, 2005 · N927CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR COMA0560714Engine · failedFLIGHT 5482 - LEFT ENGINE EXCEEDED ITT LIMITS. IFSD. REPLACED THE LEFT ENGINE.Dec 12, 2005 · N916CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA051208010Angle · crackedWHILE REPLACING THE ENGINE PYLON BOLTS AS PER THE SB601R-54-005, THE AME WORKING IN THE AREA NOTICED THAT BOTH THE LT AND RT SIDE FORMED ANGLES INSIDE ENGINE PYLON AT STA FS 640, STRINGER 10 WERE CRACKED. BOTH ANGLES P/N 601-37003-81 FOR THE LHS AND ANGLE P/NDec 8, 2005 · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR COMA0560657Spoiler · deployedUNCOMMANDED ROLL, RT FLIGHT SPOILER DEPLOYED. CND, NO FAULTS FOUND, REPLACED SECU AND SYSTEM 2A PRESSURE SWITCH FOR TROUBLESHOOTING.Nov 30, 2005 · N957CA · Cndair CL6002B19 · Drag Control SystemSDR COMA0560655Engine · lack of lubeFLIGHT 5309 - EN ROUTE RDU-BOS RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, DIVERTED TO JFK AND PERFORMED IFSD OF THE RIGHT ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE ASSEMBLY.Nov 28, 2005 · N804CA · Cndair CL6002B19 · Engine Oil Indicating SystemSDR COMA0560644Selector Valve · unreliableGEAR DISAGREE. REPLACED THE NLG SELECTOR VALVE.Nov 26, 2005 · N967CA · Cndair CL6002B19 · Landing Gear SelectorSDR COMA0560640Drive Shaft · dirtyFLIGHT 5343 - FLAPS FAIL CAUTION. CLEANED AND LUBRICATED FLAP FLEX DRIVE SHAFTS.Nov 24, 2005 · N969CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560628Engine · vibrationFLIGHT 5004 - DURING TAKEOFF, ROLL RECEIVED A LT ENGINE VIBRATION CAUTION, ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED AN INSPECTION OF THE MASTER CHIP DETECTOR, PERFORMED GROUND RUNS, DISCREPANCY COULD NOT BE DUPLICATED.Nov 19, 2005 · N735CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0560566Wire · brokenFLAPS FAIL CAUTION. REPAIRED BROKEN WIRE AT THE LT BPSU.Oct 25, 2005 · N952CA · Cndair CL6002B19 · Flight Control System Wiring
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