GE CF34-3A1

Service difficulty reports · 1,372

Newest first. General aviation reporting is voluntary.

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 COMA0560567Outflow Valve · out of positionOVERBOARD COOL SYSTEM WAS ALREADY ON DEFERRED MAINTENANCE LIST. SECURED VALVES IN PROPER POSITION.Oct 25, 2005 · N982CA · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR COMA0560565Door · out of positionCABIN DOOR WARNING. AC LOST PRESSURIZATION. CND SUSPECT DOOR NOT CLOSED PROPERLY. NO DEFECTS NOTED WITH DOOR OR PRESSURIZATION SYSTEM.Oct 24, 2005 · N917CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0560563Wire · brokenOVERHEAD EMERGENCY LIGHT, BACK OF CABIN IS INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT.Oct 22, 2005 · N926CA · Cndair CL6002B19 · Light System WiringSDR COMA0560564Bpsu · failedFLAPS FAIL CAUTION. CND REPLACED THE RT BPSU.Oct 22, 2005 · N932CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA051013001Bulkhead · crackedFOUND NUMEROUS CRACKS AT PRESSURE BULKHEAD MARKED BY BLACK MARKING REF 53-61-153 PAGE 9. PRESSURE BULKHEAD CRACKS AT STN 621 REPAIRED IAW REO 601R53-61-1230 AND PROD PERM CRJ-53-21664.Oct 13, 2005 · Cndair CL6002B19 · Fuselage Main, BulkheadSDR CA051013002Bulkhead · crackedREAR PRESS BULKHEAD CRACKED AT LBL 27.5, WL97.5, FS 621.11. REPAIRED PER: REO 601R-53-61-1285. INTEL FITTING, REPAIRED PER REO 601R-53-61-1230 UPPER OF TRACK: AS PER REO 601R-53-61-1458.Oct 13, 2005 · Cndair CL6002B19 · Fuselage Main, BulkheadSDR CA051013003Bolt · shearedWHILE CARRYING OUT CANADAIR SB601R-53-061 PART C, BOLT P/N NAS6204L11ON THE RT SIDE ENGINE PYLON WAS FOUND SEPARATED IN TWO PARTS. FRACTURE OCCURRED UNDER THE HEAD OF BOLT. BOTH THE HEAD AND SHANK OF THE BOLT LOCATED ARE IN OUR POSSESSION. WILL BE DOING A DOct 12, 2005 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA051012006Control Cable · severedWHEN BOTH ENGINES WERE REMOVED FOR INSPECTION ACCESS DURING A HEAVY MAINTENANCE VISIT, THE LT ENGINE AUTO THROTTLE RETARD CABLE (ITEM 220 IN FIGURE 2 ON CANADAIR IPC CHAPTER 76-10-00) WAS FOUND SEVERED BETWEEN THE DRILLED JAM NUT (ITEM 125) AND NUT (ITEM 165) Oct 10, 2005 · Cndair CL6002B19 · Power LeverSDR CA051005006Pin · broken(CAN) DURING A WALK AROUND THE NLG UPLOCK ROLLER PIN WAS FOUND BROKEN AT THE COTTER PIN HOLE.Oct 5, 2005 · Cndair CL604 · Landing Gear Retraction/Extension SystemSDR COMA0560525Carbon Seal · leakingFLIGHT 5809 - RIGHT ENGINE OIL PRESSURE WARNING. REPLACED THE ACCESSORY DRIVE OIL SEALS.Sep 27, 2005 · N938CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA051206003Fitting · crackedDURING SCHEDULED MAINTENANCE, SLIDER FITTING FOR PROXIMITY SWITCH PS17MB ON SERVICE DOOR WAS FOUND CRACKED. UPON FURTHER INSPECTION EXTENSIVE CORROSION WAS FOUND ON PART. SLIDER FITTING WAS REPLACED AND PROXIMITY SWITCH RERIGGED. PART TIMES AND CYCLES UNKNOSep 21, 2005 · Cndair CL6002B19 · Door Warning SystemSDR COMA0560457Scavenge Pump · malfunctionedFLIGHT 5630 - LEFT ENGINE OIL PRESSURE FLUCTUATING. REPLACED THE SCAVENGE LUBE PUMP.Aug 21, 2005 · N940CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0560454BOil System · overservicedFLIGHT 5786- LEFT ENGINE OIL PRESSURE WARNING. FOUND OIL SYSTEM OVERSERVICED. REMOVED EXCESS OIL AND OPERATIONAL CHECKS WERE NORMAL.Aug 19, 2005 · N940CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0560437Wire Harness · chafedFLIGHT 5164 - EN ROUTE FSD - CVG RECEIVED A NR 2 ENGINE FIRE MESSAGE, SHUTDOWN NR 2 ENGINE. FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY AND IDG HARNESS ASSEMBLY DUE TO CHAFED BLUE WIRE ARCING AGAINST THE FUEL CONTROL.Aug 11, 2005 · N956CA · Cndair CL6002B19 · Turbine Engine System WiringSDR COMA0560439Engine · failedFLIGHT 5739 - LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LEFT ENGINE.Aug 10, 2005 · N811CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA050815003Wire · damaged(CAN) INITIAL INVESTIGATION OF RT FIRE INDICATION LEADS US TO BELIEVE THAT A CHAFED IDG HARNESS ARCED AGAINST MAIN FUEL CONTROL. THIS ACTION CAUSED MAIN FUEL CONTROL TO LEAK WHICH LEAD TO THE SMALL CONTAINED OVERHEATING EVENT. THIS CAUSED FIRE SYSTEM TO ALERT Aug 10, 2005 · Cndair CL6002B19 · Turbine Engine System WiringSDR COMA0560436Pump · failedFLIGHT 4998 - NR 2 HYDRAULIC SYSTEM HIGH TEMP AND LOW PRESSURE WARNING. REPLACED THE RT ENGINE HYDRAULIC PUMP.Aug 9, 2005 · N712CA · Cndair CL6002B19 · Engine Fuel PumpSDR COMA0560424Engine · overtempFLIGHT 5807- LT ENGINE HIGH ITT. SHUDDER AND VIBE IN AIRFRAME. REPLACED ENGINE.Aug 2, 2005 · N442CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0560407Engine · failedFLIGHT 5378- ENROUTE OKC-CVG RECEIVED A ZERO PSI OIL PRESSURE WARNING ON THE LEFT ENGINE. CREW DECLARED AN EMERGENCY, DIVERTED TO TUL AND LANDED WITHOUT INCIDENT.Jul 24, 2005 · N916CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0560356Pump · faultyRECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC.Jun 16, 2005 · N797CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR COMA0560346Gearbox · crackedWHEN PERFORMING EO 76-011 AD, THE RIGHT ENGINE THROTTLE GEARBOX HOUSING WAS FOUND CRACKED AT THE ATR ATTACH POINT. REMOVED AND INSTALLED A SERVICABLE GEARBOX.Jun 11, 2005 · N785CA · Cndair CL6002B19 · Power LeverSDR CA050505006Vane · malfunctioned(CAN) AFTER DEPARTURE THE CREW HAD AN AIRSPEED INDICATOR PROBLEM AND LATER DETERMINED THE AIRSPEED WAS CORRECT, BUT THE BARBER POLE INDICATOR SHOWED AND THE STICK SHAKER BECAME ACTIVE. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO LAND. THE EMERGENCY VEMay 5, 2005 · Cndair CL6002B19 · Stall Warning SystemSDR CA050503014Aileron · dirty(CAN) AFTER T/O, RAIN CONDITIONS, CLIMBING INTO BELOW FREEZING TEMP, AILERONS BECAME STIFF. QRH CHECKS COMPLETED, FLIGHT CONTINUED. REMOVED WING PANELS, INSPECTED CABLE CONDITION FOR DRYNESS, WHITE POWDER. IF FOUND, REMOVED POWDER AND LUBRICATE IN FULL.. INMay 3, 2005 · Cndair CL6002B19 · Aileron Control SystemSDR CA050510001Windshield · cracked(CAN) THE RT WINDSHIELD HAD THE OUTER LAYER CRACKED WHILE IN APPROACH. THE WINDSHIELD WAS REPLACED IAW AMM.May 2, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA050502003Line · broken(CAN) INVESTIGATION OF FUEL LEAK FROM SHROUD DRAIN REVEALED APU FUEL LINE BROKEN AT THE CROSS ADAPTOR FUEL SHROUD, LOCATED BENEATH THE CARGO FLOOR AT FS 574. CROSS ADAPTOR SHROUD REMOVED FOR APU FUEL LINE REPLACEMENT.May 2, 2005 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CA050425007Acm · leakingWHEN RT PACK SELECTED MANUAL TO INCREASE HT IN CABIN AT FL350 RT PACK TEMP RUN AWAY. DASH LINES DISPLAYED ON PACK 2 ON ECS PAGE. F/A ADVISES CABIN GETTING SMOKE. RT PACK SELECTED TO AUTO FULL COLD. A/C DESCENDED TO FL240. RT PACK RECYCLED. SMOKE DISSIPATApr 25, 2005 · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA0560230Engine · out of toleranceFLIGHT 5267 DURING CLIMBOUT OF CVG THE RIGHT ENGINE WOULD NOT ACHIEVE CHARTED RATED THRUST. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE ASSEMBLY.Apr 5, 2005 · N710CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0560210Sensor · faultyFLIGHT 5065 DURING TAKEOFF ROLL THE RIGHT ENGINE WOULD NOT SPOOL ABOVE 30 PERCENT N1, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE T2 SENSOR.Mar 25, 2005 · N735CA · Cndair CL6002B19 · Engine Indicating SystemSDR CA050409001Windshield · cracked(CAN) RT WINDSHIELD CRACKED ON APPROACH. RT WINDSHIELD REPLACED AND TESTED ACCORDING AMM.Mar 24, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA050303009Control Unit · failed(CAN) JUST AFTER TOUCHDOWN AT 80 KNOTS NOSE WHEEL STEERING FAILED DRAMATIC YAW TO LT CONTROLLED WITH AERODYNMIC RUDDER AND DIFF BRAKES RESET ON TAXIWAY REFAILED ON TAXI IN DURING LT TURN. REPLACED LT RVDT AND NWS HARNESS. RT RVDT RE-RIGGED. OPS CHK SERV. A/Mar 3, 2005 · Cndair CL6002B19 · Steering UnitSDR CA050303007Duct · loose(CAN) AFTER TAKEOFF, RT DUCT 14TH AND AURAL. MESSAGE REMAIN ON EVEN AT IDLE. AFTER 14TH STAGE CLOSED MESSAGE DISAPEARED. NEW CLAMP INSTALLED ON RT 14TH STAGE DUCT, JUST DOWNSTREAM OF S/OFF VLV IAW AMM SUBT 36-12-01-420-001. RUN APU AND ENGINES TO CONFIRM NMar 3, 2005 · Cndair CL6002B19 · Engine Bleed Air SystemSDR CA050301006Apu · smoke(CAN) ON DEPARTURE, AIRCRAFT FILLED WITH SMOKE FROM APU OIL. AIRCRAFT AT THE BASE, FLIGHT DATA RECORDER PULLED SENT TO PLAYBACK CENTER FOR READ OUT. APU COMPT. INSPECTED NO FAULT FOUND SO FAR EXCEPT GLYCOL. MORE INFO WILL FOLLOW AS BECOMES (AVAILABLE).Mar 1, 2005 · Cndair CL6002B19 · APU Core EngineSDR COMA0560141Engine · malfunctionedFLIGHT 5121 DURING TAXI OUT WITH BOTH ENGINES OPERATING CREW RECEIVED AN EICAS "COMP MON" MESSAGE LOOSING ALL NR 2 ENGINE INDICATIONS. WHEN INDICATIONS RETURNED 15 SECONDS LATER, ENGINE NR 2 ITT INDICATED 990C WITH ABNORMAL N1 AND N2 INDICATIONS. THE CREW NOFeb 26, 2005 · N807CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA050209007Nozzle · inoperative(CAN) DURING ENGINE RELIGHTS PROCEDURE, AN ATS (CROSSBLEED START) WAS PERFORMED ON THE LT ENGINE WHICH WAS UNSUCCESSFUL AFTER 3 ATTEMPTS. ALL THE PARAMETERS WERE NORMAL EXCEPT THERE WAS NO LIGHT OFF AFTER 25 SECONDS ON EACH ATTEMPT. A SINGLE ENGINE LANDING Feb 8, 2005 · Cndair CL6002B19 · Fuel Injector NozzleSDR COMA0560113Pump · malfunctionedFLIGHT 5487 LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LUBE AND SCAVENGE PUMP.Feb 6, 2005 · N982CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA0560117Engine · malfunctionedFLIGHT 5852 RT ENGINE OIL PRESSURE WARNING. REPLACED THE RT ENGINE.Jan 31, 2005 · N806CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA050110002Landing Gear · collapsed(CAN) FOLLOWING A REPOSITIONING FLIGHT (FERRY FLIGHT WITH NO PAX), THE RT MLG COLLAPSED ON LANDING. NOBODY WAS INJURED DURING THE INCIDENT. THE INVESTIGATION IS STILL IN PROGRESSJan 6, 2005 · Cndair CL6002B19 · Main Landing GearSDR CA041224001Windshield · cracked(CAN) RECEIVED A REPORT WHICH WE FEEL IS A REPORTABLE EVENT. FLIGHTDECK RT SIDE WINDOW CRACKED DURING APPROACH. WINDOW REPLACED IN MUNICH, AND THEN RETURNED TO SERVICE.Dec 21, 2004 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA041217001Proximity Sensor · malfunctioned(CAN) AFTER GEAR UP SELECTION PROX SYS FAULT STATUS MESSAGE APPEARED. THE GEAR WAS RE-CYCLED AND THE MESSAGE PERSISTED. MAINTENANCE CARRIED OUT PSEU BITE CHECK AND FOUND A06 FAIL AND NVRAM FAIL .THE PSEU WAS REPLACED AND THE SYSTEM TESTED SERVICEABLE.Dec 16, 2004 · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0460668Engine · malfunctionedFLIGHT 5212 LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LEFT ENGINE.Dec 6, 2004 · N809CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR RU3A0419Seal · deterioratedAFTER TAKEOFF FUEL WAS SEEN STREAMING OUT OF LT OVERWING FUEL CAP DURING CLIMB. REPLACED FUEL CAP.Nov 29, 2004 · N87 · Cndair CL6002B16 · Fuel StorageSDR CA041129014Pump · cracked(CAN) FAULT: ON CLIMB OUT MSP, CREW RECEIVED PAX DR HANDLE LATCH MSG, FOLLOWED BY HYD SYS 3 LOW PRESS. MSG FOLLOWED BY PAX DR WARNING MSG. ON AIR RETURN, ON APPROACH FLT, RECEIVED GEAR DISAGREE MSG AND CARRIED OUT MNL EXTENSION. FOUND LINE LEAKING ON PUMP 3BNov 29, 2004 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR COMA0460615Fan Blade · vibratesFLIGHT 5037 LEFT ENGINE N2 VIBE INDICATION. REPLACED THE LEFT ENGINE FAN BLADES.Nov 12, 2004 · N954CA · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA041115001Engine · malfunctionedDURING CRUISE, THE RT ENG OIL PRESSURE SLOWLY DROPPED BELOW 25 PSI AND OIL TEMPERATURE SLOWLY DROPPED FROM 106 TO 81 DEC C. PERFORMED PRECAUTIONARY SHUTDOWN OF RT ENG. PERFORMED DRY MOTOR AND SERVICED ENGINE OIL. PERFORMED OIL CONSUMPTION RUN: 2.5 QTS USED Nov 11, 2004 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA041224003Bulkhead · cracked(CAN) MAINTENANCE FOUND TWO CRACKS ON THE 'SEMI-PRESSURE BULKHEAD' (FS559) NEAR THE AFT AILERON QUADRANT. REPAIR WAS PERFORMED IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO) 601R-53-41-256. SUBSEQUENTLY CRACKS HAVE BEEN FOUND ON TWO ADDITIONAL A/C: 06-DECNov 4, 2004 · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0460581Wire · disconnectedFLIGHT 5152 EMERGENCY FLOOR LIGHT ROW 2-5 ARE INOPERATIVE. RECONNECTED LOOSE WIRE AT ROW 5.Oct 17, 2004 · N934CA · Cndair CL6002B19 · Light System WiringSDR COMA0460572Control Unit · malfunctionedFLIGHT 5263 LT ENGINE JET OVERHEAT CAUTION MESSAGE. REPLACED THE FIRE/OVERHEAT CONTROL UNIT.Oct 12, 2004 · N779CA · Cndair CL6002B19 · Overheat DetectionSDR CA041010001Windshield · cracked(CAN) IN CRUISE AT FL360 AND 0.74 MACH, THE PILOT'S WINDSHIELD CRACKED. DIVERTED FOR MAINTENANCE. WINDSHIELD REPLACED, AIRCRAFT RETURNED TO SERVICE.Oct 7, 2004 · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0460548Skin · crackedFUSELAGE IS CRACKED ON RT SIDE JUST AFT OF NOSE LANDING GEAR DOOR AT FS 230. REPARIED IAW REO 601R-53-11-048.Sep 28, 2004 · N967CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0460552Bpsu · malfunctionedFLIGHT 5908 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.Sep 25, 2004 · N781CA · Cndair CL6002B19 · Trailing Edge Flap Control System
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