GE CF34-3B1

Service difficulty reports · 5,402

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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 = 'CF343B1'
  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 CA000224050Gearbox · leaking(CAN) DURING CLIMB, THE OIL PRESSURE FLUCTUATED 30-50 PSI WITH INTERMITTENT LOW OIL PRESSURE WARNING MESSAGE. THIS EVENT WAS PRECEEDED BY THE REMOVAL OF THE LUBE AND SCAVENGE PUMP FOR SIMILAR FLUCTUATIONS ON A PREVIOUS FLIGHT. THIS EVENT WAS RECTIFIED WITH THEFeb 24, 2000 · Cndair CL6002B19 · Accessory GearboxesSDR MASA00023Fuel Control · failedLGA/BHM - FLT 5844 - DURING APPROACH INTO BHM, THE CREW NOTED THE AIRCRAFT EXPERIENCED A HIGH EGT 900 DEGREES AND A DECREASING N1 AND N2 DURING APPROACH. IN ADDITION DURING CRUISE PRIOR TO APPROACH, THE 10TH STAGE BLEEDS CLOSED. THE CREW FOLLOWED PROCEDURES Feb 17, 2000 · N47239 · Cndair CL6002B19 · Fuel Controlling SystemSDR JBXA0000143Pump · failedHYDRAULIC LOW PRESSURE CAUTION MESSAGE, FOLLOWED BY HYDRAULIC ENGINE DRIVEN PUMP 1A CAUTION MESSAGE. REMOVED AND REPLACED NR 1 ENGINE DRIVEN PUMP ASSEMBLY, REPLACED CASE DRAIN, PRESSURE, AND RETURN FILTER ASSEMBLIES. ALL PRESSURE LEAK CHECKS GOOD. WORK ACOMFeb 7, 2000 · N578ML · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR JBXA0000142Door · openRETURNED TO RDU FOR LOUD NOISE IN COCKPIT, OVERWEIGHT LANDING. FOUND EXTERNAL SERVICE PANEL DOOR OPEN (PANEL NR 122CR) UPON RETURN TO GATE. CLOSED DOOR AS REQUIRED, NO DAMAGE NOTED. PERFORMED OVERWEIGHT LANDING INSPECTION (2000 LBS OVER) IAW CL-65 AMM 05-51Feb 4, 2000 · N580ML · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA000128059Brace · loose(CAN) ON APPROACH NR 2 ENGINE WOULD NOT RETARD BELOW 93 PERCENT. CREW SHUT DWN ENGINE AND DECLARED AN EMERGENCY. MAINTENANCE FOUND THE HOLD OPEN STRUT ON THE UPPER CORE COWL DOOR HAD FALLEN ONTO THE THROTTLE MECHANISM AND JAMMED THE THROTTLE CONTROLS.Jan 24, 2000 · Cndair CL6002B19 · Power LeverSDR CA000209054Carbon Seal · failed(CAN) IN CRUISE, RT ENG OIL PRESS ENGINE INDICATING AND CREW ALERT SYSTEM MESSAGE WITH STEADY DECREASING OIL PRESSURE INDICATION. AT 0 PRESSURE WITHIN 30 SEC. ENGINE WAS SECURED. TAILPIPE WAS FULL OF OIL. FWD AND AFT SCAVANGE SCEREENS & NR 4 BEARING CARBON SEAJan 12, 2000 · Cndair CL6002B19 · Engine Oil PressureSDR CA000120032Pump · failed(CAN) PRODUCTION AIRCRAFT EXPERIENCED LT ENGINE OIL PRESSURE WARNING WAS POSTED DURING FLIGHT TEST.Jan 7, 2000 · Cndair CL604 · Engine Oil PressureSDR CA000201020Valve · failed(CAN) OIL PRESSURE FLUCTUATION AND OIL TEMPRATURE RISE EXPERIENCED ON ONE ENGINE. THE PRESSURE AND TEMPRATURE STABILIZED AFTER DESCENT FROM FL370 TO FL30.Jan 2, 2000 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR JBXA9900133Door · openAIR NOISE COMING FROM FUSELAGE NOSE SECTION, F/O SIDE ON TAKEOFF. CLOSED GROUND POWER CONNECTION DOOR AS REQUIRED, NO DAMAGE FOUND.Dec 25, 1999 · N573ML · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA991231049Engine · malfunctioned(CAN) FOREIGN OPERATED A/C, NO OIL PX READING IFSD COMPLETED, PROBLEM NOT YET IDENTIFIED.Dec 17, 1999 · Cndair CL6002B19 · Engine Oil PressureSDR CA991231052Engine · malfunctioned(CAN) OIL PX OUT OF LIMITS, IFSD COMPLETED. PROBLEM NOT SPECIFICALLY IDENTIFIED.Dec 17, 1999 · Cndair CL6002B19 · Engine Oil PressureSDR CA991231053Oil Filter · clogged(CAN) HIGH OIL PX ADDRESSED BY REPLACING CLOGGED OIL FILTER, B SUMP REG VALVE AND CLEANED OIL PUMP SCAVENGE SCREENS. NO REASON GIVEN AS TO MATERIAL CLOGGING THESE ITEMS?Dec 17, 1999 · Cndair CL6002B19 · Engine Oil PressureSDR CA011005006Strut · failed(CAN) INCIDENT IN TIMISUARA, ROMENIA, THE 30 NOV 99 AT 14:20 (UTC). UPON TOUCHDOWN, THE RIGHT WING DROPPED TO THE GROUND WHILE THE CAPTAIN USED LEFT BRAKING TO KEEP THE AIRCRAFT ON THE RUNWAY CENTERLINE. INITIAL REPORT REVEALED THAT THE RT GEAR BROKE NEAR THE Dec 4, 1999 · Cndair CL6002B19 · Main Landing Gear Strut/Axle/TruckSDR CA991210086Engine · vibration(CAN) HIGH VIBS EXPERIENCED ALONG WITH LOW OIL PX AND RAPIDLY REDUCING N2.REPORT REQUIRED.PROJECT NR20000014. FOREIGN AC FSR REPORT NOT RECEIVED.Nov 20, 1999 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA991210087Valve · failed(CAN) OIL PX FLUX AT ALT. AFTER DESCENT TO 18000'' OIL PX STABILIZED. OIL TANK PX VALVE REPLACED AND SENT TO GE FOR INVESTIGATION.Nov 20, 1999 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA991231002Clamp · broken(CAN) V-BAND CLAMP HOLDING THE FCU AND FUEL PUMP FOUND PARTIALLY BROKEN.SB73-003 8 NOT COMPLIED WITH.Nov 15, 1999 · Cndair CL604 · Engine Fuel DistributionSDR CA991210027Light · overheated(CAN) WHILE PERFORMING INTERIOR WORK,THE ACCENT LIGHTS AROUND THE CABIN FLOOR LEVEL HAD SOME OVERHEAT SPOTS ON THE PLASTIC TUBES ESPECIALLY THE LONGEST ASSY. BOMBARDIER NOTIFIED AND SYSTEM DISABLED.Nov 12, 1999 · Cndair CL6002B16 · Passenger Compartment LightingSDR CA991210071Engine · vibration(CAN) DURING CLIMB OUT NR2 ENGINE VIB IND. IN CONJUNCTION WITH A VIB IN THE POWER LEVERS. ENGINE WAS SECURED AND EMERG. LANDING CARRIED OUT. THE VIB INDICATOR RECORDED 4.0 MILS FOR 7.6 SEC. ICING IS SUSPECTED AS COULD NOT BE DUPLICATED ON THE GROUND.Nov 9, 1999 · Cndair CL6002B19 · Engine Vibration AnalyzerSDR CA991104004Transducer · failed(CAN) OIL PRESSURE INDICATION ON EICAS AND ENGINE OIL AURAL MESSAGE ANNUNCIATED. TRANSDUCER FAILED.Nov 5, 1999 · Cndair CL6002B19 · Engine Oil PressureSDR CA991210064Warning System · activated(CAN) EICAS MESSAGE RECEIVED ALONG WITH ENG OIL AURAL MESSAGE. ENG WAS SHUT DOWN.Nov 5, 1999 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA991103071Duct Assy · defective(CAN) CABIN ALT WARNING AT FL 330. IMPOSSIBLE TO CONTROL CABIN PRESSURE IN MANUAL MODE. PROGRESSIVE RETURN TO NORMAL PASSING THROUGH FL 220. PRESSURE REGULATOR AND RELIEF VALVES REPLACED. NEXT FLIGHT EXPERIENCED SAME MALFUNCTION. AIR INLET DUCT FOUND DEFEOct 31, 1999 · Cndair CL6002B19 · Air Distribution SystemSDR CA991028050Flaps · failed(CAN) FLAPS FAIL AT 8 DEGREES. RIGHT OUTBOARD FLAP TWISTED AND NR 4 FLEXSHAFT BROKE. FLAP, NR 3, NR 4 RIGHT ACTUATORS AND NR 4 FLEXSHAFT REPLACED. PDU REPLACED DUE TO THREAD DAMAGE.Oct 21, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA991103068Fcu · failed(CAN) ENGINE FAILED TO ACCELERATE ABOVE 77 PERCENT N1. FCU REPLACED AS WELL AS N1 AMPLIFIERS SWAPPED. NO FURTHER DEFECTS NOTED.Oct 19, 1999 · Cndair CL6002B16 · Fuel Control/Turbine EnginesSDR CA991028048Flaps · failed(CAN) FLAP FAIL CAUTION MESSAGE AT 16 DEGREES. ONGOING INVESTIGATION BY TC.Oct 15, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA991028049Sensor · malfunctioned(CAN) AFTER LANDING GEAR DOWN SELECTION, THE NLG DID NOT EXTEND. AFTER 30 SECONDS, THE NLG EXTENDED WITHOUT ACTION FROM THE CREW. PSEU HAD CH27 FAULT AND WIRE PS4MB HAD HIGH RESISTANCE. NEW WIRE SPLICED IN.Oct 15, 1999 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA991028047Oil Filter · failed(CAN) OIL PRESSURE FLUCTUATIONS. AIRCRAFT FERRIED BACK TO HOME BASE IN SLOVENIA.Oct 11, 1999 · Cndair CL6002B19 · Turbine Engine Reduction GearSDR CA991004045Engine · failed(CAN) LOW OIL PRESSURE EXPERIENCED.Sep 27, 1999 · Cndair CL6002B19 · Engine Oil PressureSDR CA991004046Engine · failed(CAN) LOW OIL PRESSURE REPORTED.Sep 27, 1999 · Cndair CL6002B19 · Engine Oil PressureSDR CA991004048Engine · failed(CAN) REPORT FROM COMAIR, HIGH VIBRATION.Sep 27, 1999 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA991004049Engine · vibration(CAN) HIGH VIBRATIONS REPORTED BY COMAIR.Sep 27, 1999 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA991004044Bpsu · failed(CAN) FLAP FAIL MESSAGE ON SELECTION OF 8 DEGREE FLAP DURING PRE-FLIGHT. RIGHT BPSU REPLACED.Sep 26, 1999 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA991004043Selector Valve · failed(CAN) GEAR DISAGREE CAPTION ON GEAR UP SELECTION. NOSE GEAR SELECTOR VALVE REPLACED.Sep 25, 1999 · Cndair CL6002B19 · Landing Gear SelectorSDR CA991004039Bpsu · failed(CAN) UNSCHEDULED LANDING FOR FLAP FAIL AFTER TAKEOFF. BRAKE POSITION SENSOR REPLACED.Sep 18, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991004040Pseu · failed(CAN) FLIGHT CREW OBSERVED PROX FAULT STATUS MESSAGE. PSEU CIRCUIT BREAKER RESET/ MESSAGE WOULD NOT RESET. WHEN GEAR SELECTED DOWN, IT WOULD NOT EXTEND. EMERGENCY GEAR SELECTED. MULTIPLE FAILURES RELATED TO FAILED PSEU. AIRCRAFT LANDED WITH NO NWS OR ANTI-Sep 17, 1999 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA991004041Actuator · failed(CAN) FLAP FAIL ON APPROACH FROM 8-20 DEGREE FAILURE AT 16 DEGREES. LEFT OUTBOARD FLAP FOUND TWISTED. NR 3 AND NR 4 ACTUATORS FAILED.Sep 17, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA991004042Actuator · malfunctioned(CAN) FLAP FAILED ON WHEN SELECTED FROM 8-20 DEGREES. FAILED AT 13 DEGREES. LEFT OUTBOARD FLAP TWISTED. INBOARD (JAMMED) AND OUTBOARD ACTUATORS REPLACED ALONG WITH FLAP PANEL.Sep 17, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA990916013O-Ring · leaking(CAN) SUBMITTED BY BOMBARDIER AGAINST AIR LITTORAL (FRANCE). FR REG F-GPTI. EN ROUTE, THE CREW OBSERVED THE NR 3 HYDRAULIC PRESSURE DROPPED TO ZERO PSI AND THAT THE QUANTITY HAD DROPPED TO ZERO. MAINTENANCE FOUND A HYDRAULIC LEAK AT THE HOUSING OF THE NR 3Sep 10, 1999 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR MASA99137Compressor · stalledRDU/LGA - FLT 5830 - DURING TAKEOFF, CAPTAIN HEARD A LOUD BANG AND BELIEVED IT WAS A BLOWN TIRE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE TIRES AND AIRCRAFT, NO DAMAGE WAS NOTED. THE AIRCRAFT RETURNED TO SERVICE. (X)Aug 11, 1999 · N47239 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA990614078Pseu · failed(CAN) DOOR WARNING UNSAFE INDICATION. SUSPECT IMPROPER DOOR CLOSURE AT DEPARTURE. CONFIRMED WITH FEEDBACK FROM BOMBARDIER.Jun 10, 1999 · Cndair CL6002B19 · Door Warning SystemSDR USAASA00022Pseu · failed(CAN) DOOR WARNING UNSAFE INDICATION. SUSPECT IMPROPER DOOR CLOSURE AT DEPARTURE. CONFIRMED WITH FEEDBACK FROM BOMBARDIER.Jun 10, 1999 · Cndair CL6002B19 · Door Warning SystemSDR CA990510026Connector Pin · unlocked(CAN) SHORTLY AFTER TAKEOFF ON PRODUCTION FLIGHT 1, THE NR 2 ENGINE ITT CLIMBED TO 998 DEGREES CELSIUS AND REMAINED STEADY FOR ABOUT 3 SECONDS. FLUCTUATIONS WERE NEXT OBSERVED BETWEEN 650 AND 998 DEGREES. ALL OTHER ENGINE PARAMETERS WERE NORMAL. ACCOMPANYIApr 1, 1999 · Cndair CL6002B16 · Engine EGT/TIT Indicating SystemSDR CA990323027Wheel · damaged(CAN) NR 1 ENGINE ITT WAS 100 DEGREES CELSIUS HIGHER THAN NR 2 ENGINE DURING CLIMB. MAXIMUM CONTINUOUS 860 DEGREES CELSIUS REACHED WITH N1 5 PERCENT BELOW MAXIMUM. DURING THRUST REDUCTION ON TURN- AROUND, AN UNUSUAL NOISE WAS HEARD FROM NR 1 ENGINE AND ITT WMar 18, 1999 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA990318061Clamp · loose(CAN) IN CRUISE, THE FLIGHT CREW GOT A WARNING 'R 14TH DUCT' ON EICAS. EMERGENCY PROCEDURES CARRIED OUT. AIRCRAFT LANDED OK. THE 14TH STAGE BLEED AIR LEAK 'C' CLAMP FOUND LOOSE.Mar 10, 1999 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR MASA99004O Ring · cutYYZ/CLT - FLT 5780 - AFTER DEPARTURE FROM YYZ. CAPTAIN REPORTED A NR 2 ENGINE OIL PSI MESSAGE ON THE EICAS. CREW PERFORMED A NR 2 ENGINE SHUT DOWN AND DECLARED AN EMERGENCY. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THEJan 7, 1999 · N17217 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR 99ZZZX438Seal · failedSTL/PHL - FLT 5758 - AFTER DEPARTURE FROM STL, CAPTAIN NOTED A LEFT ENGINE LOW OIL PRESSURE MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY, SHUT DOWN THE ENGINE, AND DIVERTED TO CVG. AIRCRAFT WAS FERRIED TO BHM WHERE MAINTENANCE REPLACED THE GARLOCK SEAL. OPSNov 1, 1998 · N17175 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR MASA98195Seal · failedSTL/PHL - FLT 5758 - AFTER DEPARTURE FROM STL, CAPTAIN NOTED A LEFT ENGINE LOW OIL PRESSURE MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY, SHUT DOWN THE ENGINE, AND DIVERTED TO CVG. AIRCRAFT WAS FERRIED TO BHM WHERE MAINTENANCE REPLACED THE GARLOCK SEAL. OPSNov 1, 1998 · N17175 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA970909010Fuel Control · failed(CAN) WHEN PULLING BACK FROM GATE WITH THRUST REVERSER LEVER ABOUT .500 INCH FORWARD OF FLIGHT IDLE THE LEFT ENGINE RAN AWAY. ALL INDICATIONS WERE HEADING FOR RED. ENGINE SHUT DOWN. ONLY INDICATION NOTICED ABOVE RED WAS N1. THE ITT WENT 926 DEGREES FOR 1.2Aug 20, 1997 · Cndair CL6002B19 · Fuel Control/Reciprocating EnginesSDR SWIA97916Controller · malfunctionedON CLIMBOUT, CABIN ALTITUDE MESSAGE CAME ON. TRIED THE MANUAL PRESSURIZATION CONTROL BUT IT WOULDN'T PRESSURIZE. RETURNED TO BTM. MEL 21-31-1. REPLACED NR 2 CONTROLLER IAW MM 21-31-16, TEST OK IAW MM 21-31-16.Aug 9, 1997 · Cndair CL6002B19 · Cabin Pressure ControllerSDR SWIA97921Engine · failedFIVE MINUTES AFTER TAKEOFF, LEFT ENGINE OIL TEMP WENT UP TO 173 DEGREES AND OIL PRESSURE WENT TO 48 PSI. IN FLIGHT SHUT DOWN ACCOMPLISHED IAW QRH. REMOVED AND REPLACED LEFT A SUMP SCAVENGE PUMP IAW MM 32. REPLACED LEFT ENGINE IAW MM, OPS AND LEAKS CHECKS GOAug 5, 1997 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA97913Priority Valve · malfunctionedAFTER TAKEOFF, SELECTED GEAR UP AND GOT A GEAR DISAGREE MESSAGE. THE LEFT AND RIGHT MAIN GEAR DID NOT LOCK UP. WE SELECTED GEAR DOWN AND RETURNED TO THE AIRPORT. REMOVED AND REPLACED MLG PRIORITY VALVE IAW MM 32-32-15. PERFORMED SYSTEM TEST OF THE LANDING Jul 9, 1997 · Cndair CL6002B19 · Landing Gear Retraction/Extension System
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