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 COMA9760156Speed Control · malfunctionedLT ENGINE WOULD ACHIEVE ONLY 76 PERCENT N1 DURING TAKEOFF. ENGINEELECTRONIC SPEED CONTROL SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.Aug 12, 1997 · N983CA · Cndair CL6002B19 · Fuel Controlling SystemSDR SWIA97917Transducer · failedAFTER TAKEOFF, RIGHT OIL PRESSURE WENT FROM 27 PSI TO 138 PSI AND FLUCTUATED FOR 2 TO 3 MINUTES. RETURNED TO SLC. REMOVED AND REPLACED RIGHT ENGINE OIL PRESSURE TRANSDUCER PER MM 70-31-05, OPS AND LEAK CHECKS OK.Aug 9, 1997 · N406SW · Cndair CL6002B19 · Engine Oil PressureSDR SWIA97918Web · tornON CLIMBOUT, HEARD A VERY LOUD LOW FREQUENCY VIBRATION. OCCURRED 2 TIMES AND SUBSIDED BOTH TIMES WITHOUT ANY CHANGES BY CREW TO CONFIGURATION. RETURNED TO TUC FOR PRECAUTIONARY LANDING. INSPECTED ENTIRE AIRCRAFT EXTERNALLY. INSPECTED INTERIOR OF BELLY AND Aug 9, 1997 · N410SW · Cndair CL6002B19 · Rudder StructureSDR CA970812018Split Rim · failed(CAN) ON DEPARTURE, THE TOWER ADVISED THAT TIRE HAD BEEN FOUND ON THE RUNWAY. INNER RIGHT HAND TIRE ASSEMBLY HAD SEPARATED. THE SPLIT RIM HAD FAILED LEAVING THE INNER RIM STILL ATTACHED TO THE AXLE. NR3 AND NR4 MAIN WHEEL ASSEMBLY REPLACED.Aug 3, 1997 · Cndair CL6002B19 · Wheel/Ski/FloatSDR SWIA97952Seat Tracks · corrodedBOTH FORWARD SEAT TRACKS HAVE EXTENSIVE CORROSION. REPLACED BOTH FORWARD SEAT TRACKS IAW MM 53-00-00.Aug 2, 1997 · N407SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA97922Service Door · not closedCABIN DOOR WAS WHISTLING BADLY AND CABIN WOULDN'T PRESSURIZE ABOVE 6.2 PSI. RAMPERS LEFT THE SIDE SERVICE DOOR OPEN. RETURNED TO SLC. CHECKED PRESSURIZATION IAW MM 21-31-00. ALL CHECKS GOOD. CLEANED AND INSPECTED PASSENGER AND SERVICE DOOR SEALS WITH NO Aug 1, 1997 · N405SW · Cndair CL6002B19 · Service DoorsSDR COMA9760144Turbine · damagedLEFT ENGINE WILL NOT START. HUNG START TWO TRIES. FOUND DAMGE TO HPT. REPLACED ENGINE.Jul 29, 1997 · N986CA · Cndair CL6002B19 · Turbine SectionSDR CA970807052Panel · failed(CAN) UNABLE TO PRESSURIZE CABIN IN EITHER AUTO OR MANUAL MODE. QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT. CABIN PRESSURE CONTROL PANEL AND CABIN PRESSURE ACQUISITION MODULE CHANGED.Jul 22, 1997 · Cndair CL6002B19 · Cabin Pressure ControllerSDR SWIA97914Ahrs · malfunctionedAFTER TAKEOFF ATTITUDE AND HEADING BECAME INOP, YAW DAMPER 1 BECAME INOP AND AUTO PILOT INOP. RETURNED TO SLC. REPLACED CAPTAINS AHRS COMPUTER. OPS CHECKS GOOD IAW MM 34-21-01. THIS AIRCRAFT IS CATEGORY II.Jul 8, 1997 · N410SW · Cndair CL6002B19 · Integrated Flight SystemSDR COMA9760125Engine · fodRT ENGINE FOD DURING TAKEOFF. ITT EXCEEDED LIMITS. REPLACED RIGHT HAND ENGINE.Jul 2, 1997 · N965CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA97945Floorbeam · corrodedLBL 9.00 FLOORBEAM HAS CORROSION EXTENDING THROUGH BEAM BETWEEN FS 310.0 AND 333.0. REMOVED CORRODED AREA OF EDGE OF LBL 9.00 BETWEEN FS 310.0 AND FS 333.0 AND INSTALLED DOUBLER REPAIR IAW ON1R-53-21-092.Jul 1, 1997 · N403SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA970811008Switch · defective(CAN) DURING GEAR DOWN SELECTION, MAIN AND NOSE GEAR DID NOT EXTEND. NOSE DOORS OPEN "GEAR DISAGREE" WARNING MESSAGE ON EICAS. GEAR INDICATION ON EICAS 3 WHITE BOXES. DURING EVENT CREW ALSO REPORTED "CAS MISCOMP" STATUS MESSAGE ON EICAS. DENOTING THE WARNING MJun 17, 1997 · Cndair CL6002B19 · Landing Gear SelectorSDR CA970624024Switch · failed(CAN) AFTER TAKEOFF THE STABILIZER TRIM AND MACH TRIM CAUTION MESSAGE ON EICAS. UNABLE TO RESET. FIRST OFFICER'S STABILIZER DISCONNECT SWITCH FOUND FAULTY AND REPLACED.Jun 11, 1997 · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA97899Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.Jun 4, 1997 · N403SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA97900Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.Jun 4, 1997 · N405SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA97901Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.Jun 4, 1997 · N406SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA97902Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128. CRACK EXTENDED 160 INTO THE WEBBING AND CREATED CABIN PRESSURIZATION LOSS.Jun 4, 1997 · N407SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA97903Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.Jun 4, 1997 · N409SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA97904Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.Jun 4, 1997 · N411SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA97905Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.Jun 4, 1997 · N413SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA9760107Fuel Line · looseDURING DESCENT AT 5,000 FEET, THE LT ENGINE FLAMED OUT. FOUND LOOSE FUEL LINE AT NR 13 FUEL NOZZLE. TIGHTENED FUEL LINE AND AIRCRAFT RETURNED TO SERVICE.Jun 3, 1997 · N969CA · Cndair CL6002B19 · Engine Fuel DistributionSDR SWIA97958Angle · corrodedFLOOR SUPPORT ANGLE IN PASSENGER DOOR OPENING HAS CORROSION. REMOVED LOWER FLOOR BOARD SUPPORT ANGLE IN ENTRANCE WAY OF CABIN DOOR AND FABRICATED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED IAW SRM 51-24-16.Jun 3, 1997 · N410SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA970603024Actuator · failed(CAN) AFTER FLIGHT ATTENDANT REPORTED LOUD NOISE COMING FROM PASSENGER DOOR, FLIGHT RETURNED TO START POINT. MAIN PASSENGER DOOR AFT SNUBBER SHOWED LACK OF CABLE TENSION AND THE LEFT CABLE BRACKET HUNG DOWN AND DAMAGED THE DOOR ON CLOSURE. PASSENGER DOOR REPAIMay 23, 1997 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA970605010Tire · blown(CAN) BOTH LEFT AND RIGHT NOSE LANDING GEAR TIRES BLEW ON TAKEOFF ROLL AT 100 KNOTS. COMPLETE LOSS OF PRESSURE. TAKEOFF ABORTED. SEVERE DAMAGE TO BOTH TIRES. SIGNIFICANT DAMAGE TO NOSE LANDING GEAR WHEEL RIM ASSEMBLIES. ALSO DAMAGE TO AFT NOSE GEAR DOOR.May 22, 1997 · Cndair CL6002B19 · TireSDR CA970604009Tires · blown(CAN) BOTH LEFT AND RIGHT NOSE GEAR TIRES BLEW ON TAKEOFF ROLL. BOTH TIRES, AS WELL AS BOTH LEFT AND RIGHT NOSE WHEELS SUFFERED EXTENSIVE DAMAGE. NO REPORT OF DAMAGE TO GEAR OR DOORS. INVESTIGATION UNDERWAY.May 18, 1997 · Cndair CL6002B19 · TireSDR CA970603022Contrl Unit · failed(CAN) FLIGHT SPOILER/SPOILERON CAUTION MESSAGE DISPLAYED. FOUND RIGHT HAND SLAT ELECTRONIC CONTROL UNIT AT FAULT.May 17, 1997 · Cndair CL6002B19 · Drag Control SystemSDR SWIA97953Floorbeam · corrodedON FLOORBEAM LBL 9-00 AT FS 348 CORROSION AT INBOARD NUT PLATE. FABRICATED AND INSTALLED BACK UP ANGLE ON FLOORBEAM LBL 9-00 AT FS 348 IAW MM SRM 51-40-02.May 9, 1997 · N408SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA97954Floorbeam · corrodedON FLOORBEAM RBL 9-00 AT FS 345 HAS CORROSION AT INBOARD NUT PLATE. FABRICATED AND INSTALLED DOUBLER REPAIR ON THE FLOORBEAM RBL 9-00 AT 345 IAW.May 9, 1997 · N408SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA97955Floorbeam · corrodedON FLOORBEAM RBL 27-00 AT FS 336 CORROSION AT OUTBOARD NUT PLATE. FABRICATED AND INSTALLED A DOUBLER REPAIR ON THE FLOORBEAM IAW MM.May 9, 1997 · N408SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA97956Floorbeam · corrodedON FLOORBEAM LBL 27-00 AT FS 345 ON OUTBOARD WING OF BEAM, CORROSION AT RIVETS. FABRICATED AND INSTALLED A DOUBLER REPAIR ON FLOORBEAM LBL 27 AT FS 345.May 9, 1997 · N408SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA97957Crossbeam · corrodedAFT FS 349 CROSSBEAM CAPS BETWEEN LBL 9.00 AND LBL 27.00 AND BETWEEN LBL 27.00 AND FUSELAGE SIDE ARE REMOVED DUE TO DEEP CORROSION. REPLACED TWO WINDSCREEN SUPPORT LOCATED ON FS 349, BETWEEN LBL 9.00 AND FUSELAGE WALL IAW SRM 51-40-00.May 9, 1997 · N408SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97946Angle · corrodedRIGHT SUPPORT ANGLE IN FRONT OF SERVICE DOOR HAS CORROSION. REMOVED, FABRICATED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED ON LOWER SERVICE DOOR ENTRY WAY IAW SRM 51-24-36.May 5, 1997 · N405SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97947Angle · corrodedLEFT SUPPORT ANGLE IN FRONT OF PASSENGER DOOR HAS CORROSION. REMOVED, FABRICATED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED ON LOWER PASSENGER DOOR ENTRY WAY, IAW SRM 51-24-36.May 5, 1997 · N405SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97949Beam · corrodedLBL 27.00 HAS TWO SPOTS OF CORROSION ON WINGS OF BEAM AT FS 325, (ONE SPOT ON INBOARD SIDE, ONE SPOT OUTBOARD SIDE). FABRICATED AND INSTALLED A DOUBLER REPAIR OVER THE CORRODED AREA.May 4, 1997 · N406SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA97950Angle · corrodedFLOOR SUPPORT ANGLE IN SERVICE DOOR OPENING HAS CORROSION. FABRICATED, INSTALLED FLOOR SUPPORT ANGLE ON SERVICE DOOR IAW MM SRM 51-42-01.May 4, 1997 · N406SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97895Downlock Pin · dirtyAIRCRAFT FERRIED TO PSP DUE TO NOSE LANDING GEAR NOT COMING UP AT SFO. RETURNED TO FIELD FOR LANDING. JACKED AIRCRAFT UP AND FOUND DIRT IN GEAR DOWNLOCK PIN. CLEANED AND OPERATED GEAR PER MM 32-30-00, OPS CHECKS GOOD.May 3, 1997 · N410SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA97948Seat Track · corrodedFORWARD SEAT TRACKS AT AISLE LEFT AND RIGHT HAVE CORROSION AT FORWARD END. REMOVED CORROSION IAW SRM 51-21-00 AND TESTED BY PRESSURE AND PAINTED BOTTOMS OF TRACKS.May 3, 1997 · N406SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA97951Angle · corrodedFLOOR SUPPORT ANGLE IN PASSENGER DOOR OPENING HAS CORROSION. FABRICATED AND INSTALLED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED ON PASSENGER DOOR FUSELAGE LOWER FRAME IAW SRM 51-40-02.May 3, 1997 · N406SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA970624011Ahrs · malfunction(CAN) DURING TAKEOFF ON ROTATION BOTH ATTITUDE INDICATORS SHOWED 10 DEGREES TO 15 DEGREES DOWN EYE BROW ON. FLEW STANDBY HORIZON ON FINAL APPROACH WINDSHEAR WARNING CAME ON. #1 AND #2 ATTITUDE HEADING REFERENCE SYSTEMS REINSTALLED IN THEIR ORIGINAL POSITION FRMay 2, 1997 · Cndair CL6002B19 · Integrated Flight SystemSDR CA970529011Hstcu · failed(CAN) AFTER TAKEOFF, STABILIZER TRIM AND MACH TRIM CAUTION MESSAGE ON. TRIED RESET, NO GOOD. HORIZONTAL STABILIZER TRIM CONTROL UNIT (HSTCU) REPLACED.Apr 30, 1997 · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA97959Angle · corrodedFLOOR SUPPORT ANGLE IN PASSENGER DOOR OPENING HAS CORROSION PAST SERVICE LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE IN THE PASSENGER ENTRY WITH NEW. ALL WORK DONE IAW MM 51-40-00.Apr 26, 1997 · N412SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97960Crossbeam · corrodedFLOORBEAM CROSS MEMBER AT STA 349 BETWEEN LBL 27.00 AND LT FUSELAGE SIDE HAS CORROSION PAST SERVICE LIMITS. REPLACED FLOORBEAM STRAP BETWEEN LBL 27.00 AND FUSELAGE SIDE ON FS 349 IAW SRM 51-40-00.Apr 26, 1997 · N412SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97890Ahars · inoperativeCAPT AHARS INOP. NO HDG/ATT AFTER TAKEOFF. RETURNED TO SLC. INITIALIZED NR 1 AHARS, OPS CHECKS GOOD AT THIS TIME.Apr 20, 1997 · N405SW · Cndair CL6002B19 · Integrated Flight SystemSDR CA970505026Pump · failed(CAN) ON APPROACH, WHEN LANDING GEAR SELECTED DOWN; NOSE GEAR STAYED UP WITH EICAS INDICATION GEAR DISAGREE. HYDRAULIC SYSTEM #3 LOW PRESSURE NOSE GEAR. ON GO AROUND GEAR SELECTED UP OK. SELECTED GEAR DOWN WITH SAME EICAS MESSAGE FOR ABOUT 20 SECONDS. REPLACEDApr 19, 1997 · Cndair CL6002B19 · Hydraulic Pump, AuxiliarySDR CA970505021Bpsu · failed(CAN) FLAPS FAILED MESSAGE ON EICAS. FLAPS UNABLE TO EXTEND. BRAKE AND POSITIONING SENSOR UNIT REPLACED. ALSO FLAP ELECTRONIC CONTROL UNIT AND POWER DRIVE UNITS REPLACED. FECU P/N 865D100-5 AND PDU P/N 860D100-18.Apr 13, 1997 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA97884Overtemp Switch · failedDEPARTURE, SMOKE TOILET MESSAGE AND SMOKE REPORTED BY FLIGHT ATTENDANT. RETURNED FOR LANDING SLC. DEF RT PACK PER MM 21-51-1. FOUND RIGHT PACK OVERTEMP SWITCH INOPERATIVE. PARTS ON ORDER 04/15/97 -UPDATE - REPLACED RIGHT PACK OVERTEMP SWITCH, OPS CHECKS GOApr 13, 1997 · N412SW · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA9760049Clamp · brokenDURING A CHECK INSPECTION, THE RIGHT HAND ENGINE DRIVEN FUEL PUMP ATTACH CLAMP WAS FOUND BROKEN. REPLACED CLAMP.Feb 27, 1997 · N956CA · Cndair CL6002B19 · Engine Fuel PumpSDR CA970318014Computer · failed(CAN) BOTH PRIMARY FLIGHT DISPLAYS FAILED. #2 AHRS COMPUTER REPLACED.Feb 26, 1997 · Cndair CL6002B19 · Integrated Flight SystemSDR SWIA97862Switch · out of adjustCARGO DOOR CAUTION CAME ON CLIMBING OUT OF APPROXIMATELY 16,000 FEET AND STAYED ON UNTIL DESCENDING OUT OF 14,300 FEET. RETURNED TO SLC. FOUND CARGO DOOR PROXIMITY SWITCH TO BE OUT OF THE .50 INCH GAP. READJUSTED CARGO DOOR HANDLE PROXIMITY SWITCH IAW MM 52Feb 11, 1997 · N405SW · Cndair CL6002B19 · Door Warning SystemSDR CA970218002Bracket · worn(CAN) ON DEPARTURE CREW GOT AN AURAL MESSAGE AND AN EICAS MESSAGE. GEAR DISAGREE, NOSE DOOR OPEN. CENTERING TARGET LOOKED WORN. PROXIMITY SWITCH S23 BRACKET REPLACED.Jan 30, 1997 · Cndair CL6002B19 · Landing Gear Position and Warning
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