GE CF34-3B1

Service difficulty reports · 5,402

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 = '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 04239658Warning System · failedEVENT SUMMARY STATED THAT STALL FAIL. RETURN TO FIELD. INTERROGATED MDC AND FOUND NO STALL RELATED FAULTS. PERFORMED OPS CHECK AFTER RESETTING AIRCRAFT POWER AND FOUND NO DEFECTS WITH STALL SYSTEM AT THIS TIME.Aug 26, 2004 · N658BR · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200413759Apu · smokeFOLLOWING APU START, RECEIVED A (CARGO SMOKE) WARNING AND AURAL MESSAGE MOMENATARILY. INSPECTED APU ASSEMBLY AND DUCTING FOR LEAKS. STARTED APU SEVERAL TIMES WITH NO ANNOUNCED INDICATIONS, OPERATIONAL CHECK GOOD.Aug 26, 2004 · N440SW · Cndair CL6002B19 · APU Core EngineSDR CA040829002Wire · burned(CAN) IN DESCENT THROUGH 20-25, 000A STRONG TOXIC SMELL WAS PRESENT. SIMULTANEOUSLY, NR 1 JET OVHT FAIL CAUTION MESSAGE APPEARED FOR 10 SECONDS AND DISAPPEARED. ECS PAGE WAS SELECTED, IT WAS NOTICED THAT NR 1 PACK WAS NOT OPERATING. NR 1 PACK WAS SELECTED OAug 26, 2004 · Cndair CL6002B19 · Air Conditioning System WiringSDR MASA200400476Engine · vibrationABORTED TAKEOFF DUE TO NR 1 ENG N2 VIB. MAINTENANCE WAS ABLE TO DETERMINE THAT THE VIBRATION WAS TRANSIENT AND ALLOWABLE FOR 10 CYCLES PER GE MAINTENANCE MANUAL.Aug 26, 2004 · N77302 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA200413761Control Unit · malfunctionedSTAB TRIM CHANNEL 1 WILL NOT ENGAGE. INSTALLED A SERVICEABLE HSTCU. OPERATIONAL CHECK GOOD.Aug 24, 2004 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR COMA0460485Floor Support · crackedLT CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV A.Aug 23, 2004 · N420CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413763Switch · malfunctionedON APPROACH STAB TRIM CHANNEL 1 DISENGAGED. REMOVED AND REPLACED CAPTAINS STAB TRIM SWITCH AND STAB TRIM/MACH TRIM POND ASSY IAW MM 27-41-00 AND 27-41-25. OPERATIONAL CHECK GOOD.Aug 23, 2004 · N918SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413732Control Unit · inoperativeSTAB CHANNEL 1 INOPERATIVE. REMOVED AND REPLACED HSTCU IAW MM 27-41-00. OPERATIONAL CHECK GOOD.Aug 22, 2004 · N937SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413745Charger · malfunctionedCEILING EMERGENCY EXIT SIGN DIM. REMOVED AND INSTALLED SERVICEABLE NR 2 BATTERY CHARGER UNIT. OPERATIONAL CHECK GOOD.Aug 22, 2004 · N917SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200413729Pcu · malfunctionedON TAXI OUT, DURING FLIGHT CONTROL CHECK, SPOILERON FAULT MESSAGE ILLUMINATES. REPLACED RT SPOILERON IB PCU IAW MM 27-62-01. REPLACED SECU NR 1 AS IAW MM 27-61-05. OPERATIONAL CHECK GOOD.Aug 21, 2004 · N934SW · Cndair CL6002B19 · Drag Control SystemSDR 04233687Line · looseON 08-20-04 LEFT ENG LOW OIL PRESSURE WARNING, ENG SHUTDOWN. RESECURED OIL PRESS LINE AND SERVICED 7 QTS OF OIL. MDC VERIFIED 10 PSI FOR 7.1 SEC AND 7 PSI FOR 151.7 SEC.Aug 20, 2004 · N687BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0408013Connector · looseTHE CREW REPORTED THAT THE APU FIRE BOTTLE ARMED PUSH TO DISCHARGE GREEN LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND FOUND CONNECTOR 1PS1WA LOOSE. MAINTENANCE THEN RESECURED CONNECTOR 1PS1WA IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMEAug 20, 2004 · N242JS · Cndair CL6002B19 · Fire Bottle, FixedSDR SWIA200413744Control Unit · malfunctionedON SHORT FINAL IB GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU IAW MM 27-60-01. OPERATIONAL CHECK GOOD.Aug 20, 2004 · N908SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413728Handle · stuckUNABLE TO OPEN SERVICE DOOR. REMOVED AND REPLACED OUTER HANDLE ASSY ON SERVICE DOOR IAW SRM 51-11-06 AND 51-42-06.Aug 19, 2004 · N453SW · Cndair CL6002B19 · Service DoorsSDR 04232678Engine · shutdownLT ENG SHUTDOWN FOR LOW OIL PRESSURE. R&R LT OIL PRESS TRANSDUCER. LK & OP'S CK GOOD. PERFORMED FDR DOWNLOAD. REMOVED SCREENS FROM LT ENGINE C-SUMP FITTINGS. R&R LT ENG OIL LUBE & SCAVANGE PUMP. R&R LT ENG OIL VENT LINE & B-SUMP VENT REGULATOR VALVE. PEAug 19, 2004 · N678BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR 04230678Engine · leakingLEFT ENGINE SHUTDOWN FOR LOW OIL PRESSURE. EMERGENCY DECLARED AND DIVERTED TO CMH. LANDED UNEVENTFULLY. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE PROBLEM.Aug 17, 2004 · N678BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200413726Pcu · malfunctionedRT SPOILERON CAUTION MESSAGE. REMOVED AND REPLACED RT OB SPOILERON PCU AND FLIGHT SPOILER LEVER IAW MM 27-61-01. OPERATIONAL CHECK GOOD.Aug 17, 2004 · N923SW · Cndair CL6002B19 · Drag Control SystemSDR COMA0460473Floor Support · crackedRT FS 621 FLOOR ANGLE CRACKED. CW 601R-53-61-004.Aug 16, 2004 · N479CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460474Intercostal · crackedCRACK FOUND TO FLANGE IN CABIN FLOOR LT SIDE INTERCOSTAL. C/W REO 601R-53-41-059.Aug 16, 2004 · N479CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413922Intercostal · crackedINTERCOSTAL FLOATING ANGLE AT FS 484 RBL 27 OB CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLE IAW REO 601R-53-41-059.Aug 16, 2004 · N431SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413923Intercostal · crackedINTERCOSTAL AT FS 484 LBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059 REPAIR TO INTERCOSTALS FS 484 DL 27-00-36-00.Aug 16, 2004 · N431SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413924Intercostal · crackedINTERCOSTAL AD FS 484.0 RBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059. REPAIR TO INTERCOSTALS FS 484 BL 27-00-36-00.Aug 16, 2004 · N431SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413925Angle · crackedFS 625 OBLIQUE ANGLE IS CRACKED ON LT SIDE OF AFT PRESSURE BULKHEAD, APPROX .65 INCH LONG. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PN 601R-35012-51 IAW CRJ 200 SRM 51-42-06.Aug 16, 2004 · N431SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA200413926Angle · crackedFS 625 OBLIQUE ANGLE IS CRACKED APPROX .65 INCH LONG ON RT SIDE OF AFT PRESSURE BULKHEAD AT STR 14R. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PN 601R-35-012-52 IAW CRJ 200 SRM 51-42-06.Aug 16, 2004 · N431SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413927Floorbeam · crackedFS 280.00 ANGLES AT RBL9/LBL9 IB AND OB ARE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLES AT RBL9/LBL9 AT FS 280.00 IAW CRJ SRM 51-42-13, 51-42-21, 51-22-00.Aug 16, 2004 · N431SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200413928Floorbeam · crackedRT AFT FLOORBOARD ATTACHMENT ANGLE CRACKED AT RIGHT OUTBOARD AT EDGE OF FRAME 621.0. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ALL REPAIR PARTS IAW REO NR 601R-53-61-117.Aug 16, 2004 · N431SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR 04227678Engine · overservicedLT ENGINE OIL PRESSURE WARNING INFLIGHT. DECLARED EMERGENCY. DIVERT TO CAE. LANDED UNEVENTFULLY.WO PERFORMED GVI OF LT OIL SYSTEM AND ENGINE AND FOUND NO EXCEEDANCES OF OIL PRESSURE. DESERVICED AND SERVICED LT ENGINE OIL SYSTEM. PERFORMED SEVERAL ENGINE GROUNDAug 15, 2004 · N678BR · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0408008Control Unit · failedDURING FLIGHT, THE CREW RECEIVED A MACH AND STAB TRIM AMBER CAS MESSAGE AND RETURNED TO GSO. MAINTENANCE THEN DISPATCHED MECHANICS FROM DAY. MAINTENANCE THEN RETRIEVED CODES FROM THE MDC AND RESET THE HSTCU AND PERFORMED A FUNCTIONAL TEST WHICH WAS GOOD IN AAug 15, 2004 · N213PS · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0460460Bpsu · unreliableFLIGHT 5034 FLAPS FAIL CAUTION MESSAGE. REPLACED THE BPSU.Aug 13, 2004 · N507CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA040814001Camlock · weak(CAN) UPON INSPECTION OF AIRCRAFT DURING ROUTINE MAINTENANCE, THE LT ENGINE FORWARD LOWER COWL WAS FOUND TO HAVE 3 CAMLOCK FASTENERS UNDONE ON THE FORWARD IB SIDE. THE COWL WAS REMOVED, INSPECTED AND THE THREE CAMLOCKS (ONE LONG PN:40S5-11, THE REST SHORT PN:Aug 13, 2004 · Cndair CL6002B19 · Engine Cowling SystemSDR CA040814002Fastener · worn(CAN) UPON INSP OF AC DURING ROUTINE MAINTENANCE, THE RT ENGINE FORWARD LOWER COWL WAS FOUND TO HAVE 3 CAMLOCK FASTENERS PULLED THROUGH THE COWL WHILE STILL LOCKED IN THEIR RECEPTACLES, ON THE IB TRAILING EDGE. THE COWL WAS REMOVED, INSPECTED, AND THE THREE AAug 13, 2004 · Cndair CL6002B19 · FastenersSDR 04225677Door · defectivePAX DOOR CABLE KEEPS GETTING STUCK WHILE OPENING AND CLOSING DOOR. UPON INSPECTION FOUND PAX DOOR POWER ASSIST CABLE OFF PULLEY. ROUTED CABLE ONTO PULLEY. PAX DOOR POWER ASSIST FUNCTION OPERATES NORMAL IAW AMM 52-11-08.Aug 12, 2004 · N677BR · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0460464Warning Light · illuminatedFLIGHT 5048, FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01.Aug 12, 2004 · N507CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR 04193690Switch · out of adjustRT REV UNLOCKED MSG AFTER TAKEOFF. MECHANIC ADJUSTED RT ENG STOW SWITCH REF 78-37-00. OPS CHECK GOOD.Aug 11, 2004 · N690BR · Cndair CL6002B19 · Engine Thrust ReverserSDR 04224629Door · stuckPAX DOOR WILL NOT OPEN. MX NO DEFECTS WERE NOTED. OPS CHECK GOOD.Aug 11, 2004 · N629BR · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200413682Trim Panel · malfunctionedINFLIGHT, MACH TRIM AND CHANEL 1 STAB DISENGAGED. REMOVED AND REPLACED STAB TRIM/MACH TRIM PANEL FOR IAW CRJ 200 MM 27-41-20. OPERATIONAL CHECK GOOD.Aug 11, 2004 · N918SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413687Lamp · burned outRT SIDE EXTERNAL EMERGENCY LIGHT BURNED OUT. RELAMPED RT SIDE EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.Aug 11, 2004 · N934SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200413688Control Unit · malfunctionedON SHORT FINAL WHILE RUNNING STAB TRIM, STAB AND MACH TRIM CAUTION MESSAGE DISPLAYED. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD.Aug 11, 2004 · N410SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413730Wire · brokenFORWARD CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPAIRED BROKEN WIRE LY3D22 IN RT SIDEWALL. EMERGENCY LIGHTING OPERATION CHECKED OKAY.Aug 11, 2004 · N935SW · Cndair CL6002B19 · Light System WiringSDR CA040817008Structure · frayed(CAN) DURING THE POST FLIGHT INSPECTION THE RT AND LT WINGLET TIPS WERE FOUND TO BE DAMAGED BY STATIC DISCHARGE. THE RESIN MATERIAL WAS WAS BLOWN AWAY EXPOSING THE CARBON FIBERS AND LEAVING THE TRAILING EDGE FRAYED. CREW DID NOT EXPERIENCE LIGHTNING ON THE LASAug 11, 2004 · Cndair CL604 · Wing Main, Frame StructureSDR SWIA200413680Connector · dirtyFRONT FLOOR EMERGENCY LIGHTS AND 1 SIDE EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. CLEANED CONNECTOR AT BATTERY NR 2. OPERATIONAL CHECK GOOD.Aug 10, 2004 · N929SW · Cndair CL6002B19 · Electrical ConnectorsSDR SWIA200413667Actuator · malfunctionedAP PITCH TRIM, CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED HSTA AND MCU IAW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD.Aug 8, 2004 · N442SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413685Control Unit · malfunctioned(FLT. SPOILERS FAULT AND SPOILERONS FAULT) STATUS MESSAGES APPEARED ON TAXI-OUT. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK OK.Aug 8, 2004 · N909SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413686Control Unit · malfunctionedSTAB CHANEL 1 FALLS OFF LINE. REMOVED AND REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. PN 7062-3 SN OFF 331.Aug 8, 2004 · N913SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413668Pcu · malfunctionedLT SPOILERON NR 1 PCU STATUS MESSAGE ON EICAS. REMOVED AND REPLACED LT IB SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.Aug 7, 2004 · N435SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413683Door · lack of lubeUNABLE TO OPEN THE GALLEY ACCESS DOOR FROM OUTSIDE. ADJUSTED, CLEANED AND LUBED SERVICE DOOR AS REQUIRED IAW MM 52-41-00. OPERATIONAL CHECK GOOD.Aug 7, 2004 · N945SW · Cndair CL6002B19 · Service DoorsSDR A6WA200440113Engine · vibrationENGINE 2 VIBRATION EXCEEDED LIMITS AT V1 WITH CONSTANT AIRFRAME VIBRATION INDICATION GOT OVER 3. REMOVED AND REPLACED NR 2 ENGINE DUE TO HIGH VIBRATION IAW AMM 72-10. (M)Aug 6, 2004 · N452AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200413866Angle · crackedLT FS 625 OBLIQUE ANGLE IS CRACKED ON AFT SIDE OF AFT PRESSURE BULKHEAD IN ECS BAY. ( ITEM FOUND AT C-CHECK INSPECTION.) REMOVED AND REPLACED DAMAGED BRACKET IAW SRM 51-42-06. N 601R-35012-51.Aug 5, 2004 · N430SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA200413867Floor Support · crackedRT FS 621 FLOOR SUPPORT ANGLE IS CRACKED ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. ( ITEM FOUND AT C-CHECK INSPECTION). INSTALLED REPAIR PARTS IAW STEPS 5 AND 6 OF MFG 601R-53-61-117, PN 601R53-61-004-6 (ANGLE), 1R53-61-117-6 (RT ASSY).Aug 5, 2004 · N430SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413868Support Angle · crackedSUPPORT ANGLES ARE CRACKED AT RBL 9.0 AND LBL 9.0 FS 280.0 WL 73.5. (ITEM FOUND AT C-CHECK INSPECTION.) REMOVED AND INSTALL NEW ANGLE AT 9.0 IAW SRM CRJ 200 51-24-06 AND 51-42-21.Aug 5, 2004 · N430SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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