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 VNAA2015080800013B-Nut · looseCREW REPORTED RT ENGINE OIL PRESSURE MESSAGE IN FLIGHT AND ELECTED TO DIVERT. PRIOR TO LANDING, OIL PRESSURE CONTINUED TO DROP, SO CREW ELECTED TO SHUTDOWN RT ENGINE. MAINTENANCE INSPECTED AND FOUND OIL LEAK DUE TO LOOSE B-NUT ON B-SUMP SCAVENGE TUBE BELOW PUAug 8, 2015 · N258PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA150807006Isolation Valve · leaking(CAN) LT ENGINE 14TH STAGE BLEED AIR DUCT WARNING MESSAGE FLICKERING ON CLIMBOUT THROUGH 7,000`. CREW ACTIONED QRH, LH 14TH SELECTED OFF AND 14TH ISOL VALVE OPEN. MESSAGE WAS STILL FLICKERING. QRH DIRECTED THEM TO LAND AT NEAREST SUITABLE. FLT RETURNED. MAINTEAug 7, 2015 · Cndair CL6002B19 · Pneumatic Distribution SystemSDR CA150810003Bleed Valve · failed(CAN) LEFT ENGINE 14TH STAGE DUCT WARNING MESSAGE ON CLIMB OUT. RETURNING TO AIRPORT. ECS PAGE SHOWED NORM. ANTI ICE PAGE SHOWED RED BETWEEN THE CMD VALVES ON LT SIDE. MESSAGE CONTINUED TO GO ON/OFF. MAINTENANCE INSPECTED AND CHECKED LT 14 STAGE SENSE LOOPS ELAug 7, 2015 · Cndair CL6002B19 · Pneumatic Distribution SystemSDR ASOA2015080413446Scavenge Pump · failedDURING CLIMBOUT, AT ABOUT 1400 FT, RECEIVED A MASTER WARNING LT ENGINE OIL PRESSURE. OIL PRESSURE WAS FLUCTUATING FROM 15 PSI TO 66 PSI, RAN QRH DID NOT SHUTDOWN THE ENGINE KEEP ENGINE AT IDLE. ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY DECLARED. R & Aug 4, 2015 · N900EV · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2015080200002Skin · inflt separationBOTTOM OF LT ENGINE COWL FELL OFF DURING LANDING. MAINTENANCE INSPECTED, REPLACED LOWER NOSE COWL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Aug 2, 2015 · N223JS · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2015080200003Access Door · inflt separationBOTTOM OF LT ENGINE COWL FELL OFF DURING LANDING. MAINTENANCE INSPECTED, REPLACED POWER DRIVE UNIT ACCESS DOOR ASSEMBLY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Aug 2, 2015 · N223JS · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA150814004Acm · failed(CAN) AFTER PASSENGER DISEMBARKATION SMOKE WAS OBSERVED IN THE COCKPIT. THE APU WAS RUNNING, ACCORDING TO MAINTENANCE PERSONNEL AND LEFT PACK AIR CYCLE MACHINE IS DEFECTIVE. SHUT OFF THE APU IMMEDIATELY AND NORMAL INDICATIONS WERE OBSERVED. AT THE EVENT AIRPORJul 31, 2015 · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA201541378Engine · vibrationNR 2 ENGINE VIBRATION, SHUTDOWN ENGINE. VIBRATION MONITOR SPIKED TO YELLOW (N2). REPLACED RT ENGINE FWD UPPER AND LOWER NOSE COWLINGS, AND REPAIRED HORIZONTAL AND RUDDER DAMAGE IAW AMM.Jul 28, 2015 · N964SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA150731001Cowling · departed(CAN) CREW REPORTED HIGH VIBRATION IN THE RT ENGINE. THE RT ENGINE WAS SHUTDOWN IN FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. AFTER LANDING IT WAS REPORTED NUMEROUS PORTIONS OF THE ENGINE COWL WERE MISSING AND NUMEROUS DENTS ON THE VEJul 28, 2015 · Cndair CL6002B19 · Engine Cowling SystemSDR ASOA2015072513386Oil System · overservicedHOT RT ENGINE OIL TEMP 170-175 ON DEPARTURE. COMPLIED WITH QRH. TEMP DID NOT DECREASE WITH THRUST REDUCTION. SHUTDOWN RT ENGINE TO COMPLY WITH QRH. LANDING WEIGHT APPROXIMATELY 46,000 LBS RT OIL PRESSURE 50-42 PSI. LANDING A/S 154 KTS, ACFT RETURNED TO DJul 25, 2015 · N925EV · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA150727027Line · broken(CAN) DURING CLIMB, FLIGHT CREW HAS REPORTED L/H ENGINE SPOOL DOWN TO IDLE WITH NO RESPONSE TO THROTTLE MOVEMENT. THE ENGINE WAS SHUT-DOWN AND EMERGENCY DECLARED. BROKEN PS3 TUBE IDENTIFIED AS CAUSING THE PROBLEM.Jul 19, 2015 · Cndair CL6002B19 · Fuel Controlling SystemSDR CA150728011Fcu · failed(CAN) FLAPS FAIL AT 0 DEGREES WHEN SELECTED ON APPROACH REMOVED AND REPLACED FECU IAW AMM 27-51-05. OPS CHECK OK REMOVED AND REPLACED LT MOST OUTBAORD FLEXSHAFT IAW AMM 27-53-10. OPS CHECK OK. REMOVED AND REPLACED LT BPSU IAW AMM 27-51-10. ALL CHECKS OK. PERFOJul 13, 2015 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA150706001Window · cracked(CAN) ON CLIMB OUT AT FL200 CREW RECEIVED A LEFT WINDOW HEAT CAUTION MESSAGE. CREW THEN OBSERVED A CRACK IN THE WINDOW AND VISIBLE ARCING. QRH WAS FOLLOWED, ARCING STOPPED AND FLIGHT LANDED UNEVENTFULLY AT DEPARTURE AIRPORT. MAINTENANCE REPLACED THE LT PILOT SJul 3, 2015 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA201541355Engine · failedCLIMBOUT AT 7000', 88 PERCENT, FELT VIBRATION. LOOKED AT EICAS AND SAW RT ENGINE N2 VIBRATION ICON AND ITT AT 998, 20 SECS, PULLED BACK TO IDLE, ITT WENT DOWN. PERFORMED ENGINE SHUTDOWN. REMOVED AND REPLACED THE RT ENGINE IAW AMM.Jul 1, 2015 · N962SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA150624004Flex Drive · damaged(CAN) WHILE PERFORMING TASK 000-27-690-104, DETAILED INSPECTION OF THE RT FLAP FLEXIBLE DRIVE, MX OBSERVED THAT THE NR 4 RT FLAP FLEX DRIVE CASING WAS FOUND TO HAVE INNER COIL SEPARATED FROM END. THIS CONDITION ALLOWS FOR THE POSSIBILITY OF MOISTURE & FINE DEJun 24, 2015 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA150624005Drive Shaft · damaged(CAN) DURING MX TASK 000-27-690-104, MX NOTED THE NR 5 DRIVE SHAFT HAD A BROKEN STRAND WHICH HAD UNRAVELED FROM THE CORE. SHAFT REQUIRES REPLACEMENT.Jun 24, 2015 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA150605007Access Panel · separated(CAN) FOLLOWING LANDING AND APPLICATION OF REVERSE THRUST, THE FLIGHT CREW WAS ALERTED BY ATC THAT A PART HAD SEPARATED FROM THE ACFT. THE FLIGHT CREW CONDUCTED A POST SHUTDOWN INSPECTION OF THE ACFT AND FOUND THE RT ENGINE NOSE COWL LOWER ACCESS PANEL INSTAJun 4, 2015 · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR CA150513005Transmitter · failed(CAN FLAP FAIL AFTER LANDING ON TRYING TO RETRACT THE FLAPS FROM 45 DEGREES TO ZERO DEGREES. THE OUTSIDE AIR TEMP WAS AT 23 DEGREES. THE FLAPS STOPPED AT 25 DEGREES AS INDICATED ON BOTH SIDES, FERRY FLIGHT DEFERRAL. ACTION PLAN CARRIED OUT & RT BPSU R & R WMay 8, 2015 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA150501001Clamp · failed(CAN) DURING THE CLIMB, CREW REPORTED AN ANTI-ICE DUCT WARNING MESSAGE AND A DUCT FAIL LIGHT ON THEIR ICE PROTECT PANEL. THE DECISION WAS MADE TO RETURN TO DEPARTURE POINT FOR MAINTENANCE ACTION. MAINTENANCE ACTION FOUND SUBSTANTIAL LEAK NOTED DURING ENGINEMay 1, 2015 · Cndair CL6002B19 · Pneumatic Distribution SystemSDR SWIA201541112Engine · reads highDURING CLIMBOUT RT ENGINE ITT WENT TO RED AND OIL TEMP WENT RED. ENGINE SHUTDOWN ON ITS OWN. R & R RT ENG IAW AMM. OPS AND LEAK CHECKED GOOD.Apr 30, 2015 · N453SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201542687Stiffener · crackedRIGHT ENG EXHAUST NOZZLE FAIRING SECOND STIFFENER FROM LE IS CRACKED.Apr 29, 2015 · N461AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR CA150427013Control Unit · failed(CAN) SHORTLY AFTER TAKEOFF FROM POINT A, CREW RECEIVED LT WING ANTI-ICE DUCT WARNING MSG. DISPATCH & MOC WERE CONTACTED & THE QRH WAS FOLLOWED. AFTER WEIGHING, AVAILABLE OPTIONS, DIVERSION INTO POINT B WAS DEEMED SAFEST OPTION AS THE ACFTT WOULD NOT BE ABLEApr 26, 2015 · Cndair CL6002B19 · Pneumatic Distribution SystemSDR A6WA201542654Stiffener · crackedRT ENG EXHAUST FAIRING 2ND STIFFENER CRACKED.Apr 17, 2015 · N434AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201542638Stiffener · crackedLEFT ENG TAIL PIPE FAIRING HAS A CRACK IN NR 2 STIFFENER.Apr 15, 2015 · N463AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201542630Pressure Switch · malfunctionedAFTER TAKEOFF, RECEIVED NUMEROUS LT ENGINE OIL WARNING MESSAGES ALONG WITH A FLUCTUATION OF LT LOW OIL PRESSURE INDICATIONS. OIL PRESSURE NEVER DROPPED BELOW 5 PSI. DECLARED AN EMERGENCY. COMPLIED WITH QRH & RETURNED TO DEPARTURE. R & R OIL PRESSURE TRANSApr 13, 2015 · N455AW · Cndair CL6002B19 · Engine Oil Indicating SystemSDR CA150409004Cvr · failed(CAN) WE CARRIED OUT THE CVR INTEL CHECK, THE RECORDER WAS SENT TO NRC FOR READ BACK, ON THE READ BACK WAS DETERMINED THAT THE CVR WAS US. HAD A RED LIGHT ON THEIR UNIT & THE NEEDLE WAS PEGGED AT FULL DEFLECTION. SO THE CVR WAS PUT BACK IN THE ACFT & TRIED AApr 7, 2015 · Cndair CL6002B19 · Audio/Video MonitoringSDR CA150331004Drain Line · chafed(CAN) AIRBORNE RETURN. WHILE ENROUTE TO DESTINATION THROUGH 15,000`, THE CREW ADVISED THAT THEY HAVE LOST THE NR 1 HYDRAULIC SYSTEM. THE NR 1 HYDRAULIC QTY QUICKLY WENT TO 0 AND THE PRESSURE WENT TO 0 PSI. THEY RECEIVED ALL ASSOCIATED MESSAGES. ADDITIONALLY, Mar 27, 2015 · Cndair CL6002B19 · Hydraulic System, MainSDR CA150327001Adc · failed(CAN) AIRBORNE RETURN. FLIGHT WAS ENROUTE TO DESTINATION WHEN FLIGHT CREW ADVISED OF A NR 1 ADC FAILURE. FLIGHT RETURNED TO ORIGINATING POINT FOR MAINTENANCE RECTIFICATION WHICH CONSISTED OF ADC REPLACEMENT.Mar 26, 2015 · Cndair CL6002B19 · Air Data ComputerSDR CA150324003Actuator · failed(CAN) AFTER DEPARTURE NR 1 YD KICKED OFF LINE AND CREW REPORTS PULSING/JERKING FELT IN THE RUDDER SYS IN FLT WITH AND WITHOUT YDS ENGAGED. PULSING FELT IN THE AIRFRAME AND IN THE RUDDER PEDALS. CREW RETURNING TO AIRPORT DUE TO SAFTEY CONCERN. ON THE FLT CONMar 23, 2015 · Cndair CL6002B19 · Autopilot Main ServoSDR VNAA2015031700023Blades · damagedCREW REPORTED LOUD VIBRATION ON TAKEOFF AND LT FAN VIBRATION OF 1.6. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION AND FOUND DAMAGE TO LT ENGINE FAN BLADES FROM BIRD STRIKE. NO OTHER DEFECTS NOTED. MAINMar 17, 2015 · N249PS · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR A6WA201542506Support · crackedLEFT TAIL PIPE FAIRING NR 3 SUPPORT HAS CRACK NEAR 8 POSITION.Mar 13, 2015 · N413AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR VNAA2015030800013Switch · failedCREW REPORTED RECEIVING REV ICON ON RT ENGINE IN FLIGHT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. AN INTERMITTENT RT REVERSER UNLOCKED CAUTION MESSAGE ALSO RECEIVED DURING CLIMB. CREW RETUNED TO FIELD AND LANDED WITHOUT INCIDENT. INSPECTED THRUST REVERSERMar 8, 2015 · N218PS · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2015022700024Engine · damagedCREW REPORTED LT N2 VIBRATION MESSAGE WHILE ON RUNWAY. WHEN SETTING TAKEOFF POWER, CREW HEARD LOUD POP FOLLOWED BY GRINDING SOUND COMING FROM LT SIDE OF ACFT. CREW REJECTED TAKEOFF, SHUTDOWN LT ENGINE AND RETURNED TO GATE. MAINTENANCE INSPECTED LT ENGINE AND Feb 27, 2015 · N242JS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA150303005Engine · shutdown(CAN) IN FLIGHT SHUTDOWN AFTER LANDING, THE OIL QUANTITY WAS NORMAL. NO FINDINGS HAVE BEEN FOUND SO FAR EXCEPT SLIGHT OIL LEAK EVIDENCE ON RT ENGINE COWLING. INVESTIGATION ON-GOING.Feb 25, 2015 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA150305011Engine · shutdown(CAN) ENGINE SHUTDOWN ON DESCENT.Feb 20, 2015 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA150220008Door · departed(CAN) DURING THE WALKAROUND AFTER LANDING, THE CREW NOTICED LT MLG DOOR MISSING. THERE IS NO DAMAGE NOTICED TO AIRFRAME OR FLAPS. DISPATCH FIGURES THAT THE FUEL BURNS WERE BANG ON FOR THIS FLIGHT SUCH THAT PERHAPS IT DEPARTED THE A/C CLOSER TO LANDING. MAINTEFeb 19, 2015 · Cndair CL6002B19 · Landing Gear DoorsSDR VNAA2015021600011Transducer · failedCREW REPORTED LT ENGINE OIL PRESSURE DROP ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT ENGINE OIL PRESSURE TRANSDUCER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Feb 16, 2015 · N237PS · Cndair CL6002B19 · Engine Oil PressureSDR A6WA201542410Unknown · odorAFTER STARTING APU & TRANSFERRING PACKS TO APU BLEED, STARTED TO SMELL SMOKE, OIL SMELL FOLLOWED BY SMOKE TOILET CAUTION MSG. TRANSFERRED BACK TO ENG BLEEDS SMELL CLEARED ALONG WITH CAUTION MSG. COMPLIED WITH CM ACTION. PLACARDED & PLACED ON MEL, PLACED APUFeb 12, 2015 · N421ZW · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2015020700004Warning Message · activatedCREW REPORTED RIGHT THRUST REVERSER UNLOCKED MESSAGE APPEARED AND EXTINGUISHED IN FLIGHT. CREW DIVERTED AND LANDED SAFELY.Feb 7, 2015 · N249PS · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201542357Cowling · crackedRIGHT UPPER CORE COWL INBD FWD LE CRACKED.Jan 31, 2015 · N415AW · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201542350Fuel Control · failedDURING CLIMB OUT, FELT AN AIRFRAME VIBRATION. LT N1, N2, ITT & FUEL FLOW ERRATIC. LT VIBRATION 0.5. LT ENGINE PARAMETERS FLUCTUATED +/- 2% & FF 300LBS. DECLARED AN EMERGENCY & RETURNED. R & R LT FUEL CONTROL ASSEMBLY IAW AMM 73-21-00. PERFORMED OPS, LEAK,Jan 24, 2015 · N403AW · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR VNAA2015011600026Engine · vibrationWHILE DESCENDING THROUGH 20,000 MSL, CREW REPORTED A VIBRATION AND THAT LT ENGINE INTERTURBINE TEMPERATURE (ITT) SPIKED AND ENGINE SHUTDOWN. ATTEMPT TO RELIGHT ENGINE WAS UNSUCCESSFUL. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INJan 16, 2015 · N262PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA150123009Lockout · failed(CAN) ABORTED TAKE OFF DUE TO THROTTLE QUADRANT MOTION IRREGULARITY. AFTER LOW ENERGY ABORT AIRCRAFT WAS ABLE TO RETURN TO GATE WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REPLACED THE THROTTLE LOCKOUT SWITCH AND RE-RIGGED THE STOW SWITCH.Jan 9, 2015 · Cndair CL6002B19 · Power LeverSDR CA150109002Selector Valve · bypassing(CAN) CREW RECEIVED A GEAR DISAGREE CAUTION MESSAGE AFTER GEAR SELECTED UP. BOTH MAIN GEAR RETRACTED HOWEVER THE NOSE GEAR REMAINED EXTENDED WITH DOORS OPEN. ABOUT 5 MINUTES LATER THE NOSE GEAR RETRACTED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT FOR AN UJan 7, 2015 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA150116017Actuator · failed(CAN) FLAP FAIL AFTER TAKE OFF OUT WHEN SEL FLAPS FROM 8 TO 0 SETTING. FLAPS DID NOT MOVE THEY REMAINED AT 8 DEG. DECISION WAS MADE TO DIVERT TO ANOTHER AIRPORT. MAINENANCE DOWNLOADED AND FORWARDED ALL CODES FROM FECU TO FLEET TECH SUPPORT. AS PART OF TROUBLESJan 4, 2015 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA141224002Window · failed(CAN) F/O SIDE WINDOW SHATTERED IN CRUISE AFTER ELECTRICAL ACRING. MAINTENANCE REPLACE THE WINDSHIELD IAW AM 56-12-01. AC PRESSURIZED. LEAK CHECKED AND HEAT FUNCTION CHECKED SERVICABLE.Dec 22, 2014 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA150108005Transmitter · failed(CAN) FLIGHT DIVERTED DUE TO FLAP INDICATION DURING FLIGHT. EMERGENCY WAS DECLARED AND THE PLANE LANDED WITHOUT INCIDENT.Dec 21, 2014 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA201440423Mount · galledRT ENGINE FORWARD MOUNT LINK ASSY AND CLAMP BUSHING GALLED. R & R RT FWD MOUNT LINK ASSY IAW AMM.Dec 19, 2014 · N452SW · Cndair CL6002B19 · Engine Mount SectionSDR CA141217010Windshield · cracked(CAN) CRACK RT WINDSHIELD.Dec 15, 2014 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA141217021Controller · failed(CAN) RIGHT WINDSHIELD HEAT CAUTION MESSAGE ON IN FLIGHT. WILL GO OUT AFTER BEING SHUT OFF FOR A LITTLE WHILE AND WHEN TURNED BACK ON THE MESSAGE WILL RETURN AFTER A FEW MINUTES. MAINTENANCE RETURNED THE SPARE TEMP ELEMENT WIRING TO ORIGINAL POSITIONS. RT WDec 15, 2014 · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
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