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 CA120512001Throttle Cable · not reported(CAN) AC WAS ENROUTE. CREW ADVISED DISPATCH THAT THE RT ENGINE WAS UNRESPONSIVE. THE CREW ELECTED TO DIVERT TO ANOTHER AIRPORT DUE TO LONGER RUNWAY AT THAT LOCATION. WHEN RETARDING POWER DURING DESCENT, THE RT ENGINE REMAINED AT 94 PERCENT. THERE WAS NO RESPOMay 11, 2012 · Cndair CL6002B19 · Power LeverSDR CA120511008Duct · separated(CAN) REF DEFECT-1054133. COCKPIT PACK SHOWING 85-90 DEGREE CELSIUS, GOOD PRESSURE AT PACK BUT LOW COCKPIT FLOW, AIR CONDITIONING PACKS, LH, RESOLVED ON WO: 336482, TASKCARD: NR-00001. FOUND DUCT, PN 601R95211-113 FROM LT PACK WATER SEPARATOR, BLOWN OFF/BROKMay 10, 2012 · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201240762Door · chafedLT MLG DOOR IS CHAFED ON THE INSIDE T/E. REPAIRED LT MLG DOOR CHAFE ON THE INSIDE T/E IAW REO 601R-52-82-351, REV A.May 6, 2012 · N447AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240534Bracket · brokenT2 SENSE LINE BRACKET BROKEN, SUPPORT BRACKET FOR THE T2 SENSE LINE ON TOP OF THE ENGINE. REMOVED ENG INLET AND INSTALLED A NEW SERVICEABLE BRACKET.May 4, 2012 · N406AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR ASOA201201558Support Bracket · crackedTWO SUPPORT BRACKETS CRACKED ON NOSE INLET COWLING OTBD SIDE. R & R SUPPORT BRACKETS IAW SRM 51-21-06 AND CMM 71-61-01-400-001-A01.May 3, 2012 · N860AS · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR CA120514004Engine · stopped(CAN) FLIGHT WAS ON DESCENT/APPROACH WHEN THE LT ENGINE SUDDENLY STOPPED APPROXIMATELY 17 MINUTES SHORT OF TOUCHDOWN. THE CREW APPLIED THE RELEVANT QRH PROCEDURE AND THE AC LANDED WITHOUT FURTHER EVENT. THE ENGINE WAS REPLACED AND THE ACFT WAS RETURNED TO SERMay 3, 2012 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201240493Cargo Track · corrodedTIE DOWN TRACK OF FS 574 AND LBL27 AS CORROSION. R & R TRACK IAW SRM 53-61-49.Apr 30, 2012 · N446AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240533Bracket · crackedLT ENGINE THRUST REVERSER STOW SWITCH BRACKET CRACKED. R & R LT ENGINE T/R STOW SWITCH BRACKET WITH NEW SERVICEABLE PN 228-55410-835 IAW SRM 51-42-06.Apr 25, 2012 · N406AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240494Connector · brokenRT ENGINE INBD SWITCH CONNECTOR PLUG BRACKET IS BROKEN. REMOVED BROKEN BRACKET AND REPLACED WITH NEW SERVICEABLE BRACKET PN 228-55410-835 IAW ECC 20-17-10, SRM 51-42-20, 51-41-00 IN RT ENGINE INBD T/R MICRO SWITCH CONNECTOR PLUG.Apr 22, 2012 · N446AW · Cndair CL6002B19 · Engine Exhaust System WiringSDR A6WA201240720Threshold · corrodedSERVICE DOOR THRESHOLD HAS SEVERAL CORRODED FASTENER HOLES AND CRACKED. REMOVED UNSERVICEABLE SERVICE DOOR THRESHOLD AND REPLACED WITH SERVICEABLE SERVICE DOOR THRESHOLD IAW SRM 51-41-00.Apr 18, 2012 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240471Skin · chafedLEFT UPPER CORE COWL HAS A CHAFED AREA, FWD LOWER CORNER CHAFE MARK IS APPROX 10" LONG. REPAIRED LT CORE COWL IAW REO 601R-71-12-4106.Apr 17, 2012 · N443AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR ASOA201201225Transducer · failedOIL PRESSURE FLUCTUATION ON CLIMB OUT, THEN DROPPED BELOW 25 PSI. RAN QRH WITH THRUST LEVER AT IDLE, PRESSURE STARTED TO INDICATE NORMAL. ACFT RETURNED, EMERGENCY DECLARED. R & R RT ENGINE OIL PRESSURE TRANSDUCER IAW AMM 79-31-05 (IPC 79-30-00 ITEM 35A). OApr 6, 2012 · N922EV · Cndair CL6002B19 · Engine Oil Indicating SystemSDR CA120403006Support Angle · cracked(CAN) WHILE PERFORMING AN INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION IAW TASK RJ2-57-900-320, THE AME FOUND A CRACK EMINATING FROM 1 OF THE RELIEF CUTOUTS FOR THE STR IN THE WEB OF THE SUPPORT ANGLE, PN: 601R10011-13. THE ACFT IS CURRENTLY DOWN FOR AApr 3, 2012 · Cndair CL6002B19 · Wing Miscellaneous StructureSDR CA120330008Gearbox · cracked(CAN) DURING INSPECTION FOUND ENGINE THROTTLE CONTROL GEARBOX CRACKED AT THE CABLE INPUT END.Mar 30, 2012 · Cndair CL6002B19 · Power LeverSDR ASOA201201078Scavenge Pump · failedRIGHT ENGINE OIL PRESSURE MASTER CAUTION AT 18000 FT. EMERGENCY DECLARED. R & R RT LUBE AND SCAVENGE PUMP IAW AMM 79-21-01. LEAK AND OPS CHECKED GOOD.Mar 29, 2012 · N825AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR REXA2012032100405Engine · bird ingestionAIR RETURN FOR BIRD STRIKE IN RT ENGINE, OVERWEIGHT LANDING BUT NOT A HARD LANDING. 200 FPM TOUCHDOWN. BIRD STRIKE INSPECTION CHECKLIST COMPLETED. SEE DISCREPANCY NR 2 PG 2189314 FOR RT ENGINE DAMAGE, SEE DIESCREPANCY NR 1 PG 2189315 FOR OVERWEIGHT LANDING.Mar 21, 2012 · N8924B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2012032200013Carbon Seal · defectiveCREW REPORTED LEFT ENGINE OIL PRESSURE RED CAS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT ENGINE, REMOVED AND REPLACED CARBON SEALS FOR LEFT ATS (AIR TURBINE STARTER), IDG (INTEGRATED DRIVE GENERATOR) AND EDP (ENMar 17, 2012 · N207PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201240356Structure · damagedCLIMBING THRU FL140, LT ENG OBSERVED MOMENTARY OVERSPEED OF N1. NORM ENG INDICATIONS OBSERVED. UPON DECENT LEFT ENGINE THRUST LEVER STUCK AND UNABLE TO REDUCE N1 BELOW 81 PERCENT. COMPLIED WITH QRH, THRUST LEVER JAM PROCEDURE AND SHUTDOWN LEFT ENGINE INFLIMar 17, 2012 · N408AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA120322008Door · missing(CAN) CLIMBING THROUGH 14,000 FT, THE FLIGHT CREW OBSERVED A MOMENTARY LT ENGINE N1 OVERSPEED. THE REST OF THE ENGINE PARAMETERS APPEARED NORMAL. UPON DESCENT, THE LT ENGINE THRUST LEVER BECAME STUCK AND UNABLE TO REDUCE N1 SPEED BELOW 81 PERCENT. THE FLIGHTMar 17, 2012 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR VNAA2012031600009Blade · damagedCREW REPORTED BIRD STRIKE ON NUMBER TWO (2) ENGINE. NO CHANGE IN ENGINE VIBRATION NOTED. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED RIGHT ENGINE AND NOTED FAN BLADE DAMAGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, REMOVED AND REPLACEDMar 13, 2012 · N230PS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR REXA2012031100359Engine · malfunctionedSMOKE TOILET CAUTION MSG AFTER TAKEOFF AIR RETURNED, NO SMOKE IN CABIN OR LAV ALL INDICATIONS NORMAL. CHANGED THE ENGINE.Mar 11, 2012 · N8960A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA120309001Angle · cracked(CAN) THE AME WAS PERFORMING AN INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION FOR TASK RJ2-57-900-320, WHEN HE FOUND CRACKS EMINATING FROM EACH OF THE 2 RELIEF CUTOUTS FOR THE STRINGERS IN THE WEB OF THE SUPPORT ANGLE. PN: 601R10011-13 AND ANGLES, PN:60Mar 9, 2012 · Cndair CL6002B19 · Wing Miscellaneous StructureSDR CA120309004Angle · cracked(CAN) CRACK FOUND IN THE CENTER WING FUEL TANK FWD OF THE COLLECTOR TANK, INSIDE FUEL PANEL NR 510AB, LT SIDE AT WS29.42 WHILE DOING INSPECTION RJ2-57-900-320. CRACK IS ON CLOSING ANGLE, PN: 601R10011-13. THE CRACKED ANGLE IS ATTACHED TO THE VERTICAL MEMBER Mar 6, 2012 · Cndair CL6002B19 · Wing Miscellaneous StructureSDR REXA2012030400338Warning System · activatedFLT 3759 FSD-DTW ABORTED TAKEOFF AT LESS THAN 50 KTS DUE TO HIGH LT ENGINE OIL PRESSURE CAUTION. THE CREW ONLY HAD THE ENGINE RUNNING FOR FOUR MINUTES BEFORE ATTEMPTING THE TAKEOFF. THE CREW IS GOING TO LET THE ENGINE RUN FOR LONGER TO WARM UP AND THE ATTEMPMar 4, 2012 · N8646A · Cndair CL6002B19 · Engine Oil PressureSDR REXA2012030200324Alternator · defectiveDID AN AIR TURNBACK DUE TO APR INOP/N1 FLUX/ DCU WARNING, EMERGENCY NOT DECLARED, A/C LANDED SAFELY MX IN MEETING A/C TO BEGIN T/S. REMOVED AND REPLACED NR 2 ALTERNATOR.Mar 2, 2012 · N8718E · Cndair CL6002B19 · DC Generator-AlternatorSDR VNAA2012030200015Anti-Ice Valve · failedCREW REPORTED LEFT COWL ANTI-ICE AMBER MESSAGE WITH LEFT COWL ANTI-ICE SWITCH SELECTED OFF. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT ENGINE COWL ANTI-ICE SYSTEM, REMOVED AND REPLACED LEFT COWL ANTI-ICE VALVE AND PERFORMED CHECKS USIFeb 27, 2012 · N241PS · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR A6WA201240273Panel · missingMISSING PANEL AT O`CLOCK POSITION. INSTALLED EXHAUST NOZZLE FAIRING MOUNT BOLT ACCESS PANEL IAW AMM 78-11-01, REF L/P 249882/3 FOR MEL.Feb 23, 2012 · N421ZW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR REXA2012021500235Blades · vibrationABORTED TAKEOFF DUE TO RT ENGINE FAN VIBRATION . REMOVED & REPLACED 18 FAN BLADES ON RT ENGINE IAW AMM 72-20-00.Feb 15, 2012 · N8604C · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR REXA2012021500238Blade · damagedABORTED TAKEOFF DUE TO FAN VIBRATION ON RT ENGINE. REMOVED & REPLACED 18 FAN BLADES ON RT ENGINE IAW AMM 72-20-00.Feb 15, 2012 · N8604C · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201240363Skin · damagedRT UPPER CORE COWL HAS SCRATCHES ON OUTER SKIN. REPAIRED RT UPPER CORE COWL OUTER SKIN ON OTBD SIDE IAW CMM 71-12-01, REPAIR SRS 021.Feb 15, 2012 · N428AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR REXA2012021400225Plug · missingRT ENG TAIL CONE HAS EVIDANCE OF BURN DAMAGE. FOUND BOROSCOPE PLUG S50 MISSING. REPLACED BOROSCOPE PLUG IAW AMM 72-00-00. REMOVED AND REPLACED RT EXHAUST FAIRING IAW AMM 78-11-01.Feb 14, 2012 · N8896A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2012021500010Cowling · damagedCREW REPORTED HEARING LOUD BANG AND AIRCRAFT YAWED TO LEFT DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND DAMAGE TO LEFT ENGINE LOWER TRANSCOWL AND DENTS IN FUSELAGE. PAINTED LT LOWER TRANSITION CFeb 12, 2012 · N218PS · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201240344Structure · damagedELONGATED HOLE UNDER MOLDED SEAL. REPAIRED IAW REO 601R-78-30-4091.Feb 12, 2012 · N441ZW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240365Skin · chafedLT LOWER CORE COWL OUTER SKIN CHAFED FROM LOCKER DOOR COMPLIED WITH CMM. REPAIR SRS 104428.Feb 11, 2012 · N428AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240364Skin · chafedRT LOWER CORE COWL OUTER SKIN CHAFED FROM BLOCKER DOOR. COMPLIED WITH CMM REPAIR SRS 104C.Feb 11, 2012 · N428AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR SWIA201229555Bushing · corrodedRIGHT ENGINE THRUST SHAFT BUSHING HAS PITTING. (SERVICE) REPLACED RIGHT ENGINE THRUST SHAFT BUSHING.Feb 7, 2012 · N976SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201240345Seal · chafedRT LOWER NOSE COWL HAS CHAFED T/E SEAL. R & R RT NOSE COWL T/E SEAL IAW CMM 71-14-01, SRS 091.Feb 7, 2012 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201240343Rib · crackedNR 2 FRAME & RIB IN RT JET PIPE FAIRING IS CRACKED AT 9:00 POSITION AND DENTED AT A 3:00 POSITION. REMOVED AND REPLACED RIB.Feb 4, 2012 · N441ZW · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/RibSDR VNAA2012020600018Rod · disconnectedCREW REPORTED LEFT THRUST LEVER WAS JAMMED IN POSITION DURING FLIGHT. CREW FOLLOWED QRH (QUICK REFERENCE HANDBOOK), SHUT DOWN LEFT ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND LEFT ENGINE AFT CORE UPPER COWL UPPER SUPPORT ROD DJan 31, 2012 · N242JS · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201240302Skin · crackedA CRACK IN RT (FWD) CORE COWL DOOR OUTER SKIN. REMOVED DAMAGE FROM OUTER SKIN. FABRICATED DOUBLER AND SPIGOT IAW REO 601R-71-12-4095 AND CMM 71-12-01. REPAIR SRS118.Jan 31, 2012 · N401AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR CA120131009Skin · cracked(CAN) WHILE CARRYING OUT A SCHEDULED TASK CARD RJ2-53-120-330 FOR GENERAL VISUAL INSPECTION OF THE EXTERNAL NOSE SKIN, THE AME FOUND A CRACK EMANATING FROM THE AFT LATCH CUT-OUT FOR THE LT SIDE ELECTRONICS BAY DOOR IN THE NOSE OF THE ACFT. THE DAMAGE LOCATED Jan 31, 2012 · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201240255Skin · scratchedRT ENGINE NOSE INLET L/E HAS A SCRATCH & SEVERAL PITTS ON INBD UPPER & LOWER. BLENDED PITTING AND SCRATCH ON RT ENG NOSE INLET WITHIN LIMITS IAW REO 601R-71-61-2532.Jan 28, 2012 · N439AW · Cndair CL6002B19 · Engine Air Intake SystemSDR A6WA201240142Thrust Reverser · malfunctionedDURING CLIMB OUT, RECEIVED RT THRUST REVERSER UNLOCK CAUTION WITH EMERGENCY TOW LIGHT. PUSHED EMERGENCY STOW AND LIGHT PERSISTED, ACFT FLEW NORMALLY. COMPLIED WITH THRUST REVERSER OPS CHECK, OPERATED NORMALLY 3 TIMES IAW 71-00-00-710-806.Jan 27, 2012 · N456ZW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201240141Throttle · malfunctionedCONFIGUATION SPOILER WARNING MESSAGE AT 20 KTS ON TO ROLL. R & R THROTTLE QUADRANT IAW AMM 76-11-01, OPS AND RIGGING CHECKED GOOD.Jan 27, 2012 · N438AW · Cndair CL6002B19 · Power LeverSDR A6WA201240139Duct · contaminatedF/A REPORTED "SMOKE" IN CABIN DURING FLIGHT. FOUND PACK DUCT CONTAMINATED WITH COMPRESSOR WASH FLUID, MX PERFORMED POST COMPRESSOR WASH RUN IAW SUPP 06-047A AND CLEARING OF CONTAMINATION DUCTING IAW SUPP 09-037A. NO SMOKE ODOR PRESENT.Jan 23, 2012 · N421ZW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA201240256Retainer · debondedLT LOWER CORE COWL HEAT SHIELD HAS AREAS AND DEBONDED. FABRICATED AND INSTALLED RETAINER STRIP ON LT LOWER CORE COWL HEAT SHIELD IAW CMM 71-12-01.Jan 21, 2012 · N439AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA120321007Tire · separated(CAN) TREAD SEPARATION ON MAIN WHEEL TIRES. THE LATEST INCIDENT CAUSED EXTENSIVE FLAP DAMAGE.Jan 21, 2012 · Cndair CL6002B19 · TireSDR CA120207004Wire · frayed(CAN) THE FLIGHT CREW REPORTED A PASSENGER DOOR STOW CAUTION MESSAGE ON EICAS. TROUBLESHOOTING FOUND THE MCD HANDLE PROX SENSOR PS1MB HAD A FRAYED AND DAMAGED WIRE FROM INTERFERENCE WITH THE MCD HANDLE LINKAGE. THIS PROX SENSOR WAS PREVIOUSLY REPLACED LAST SEPJan 20, 2012 · Cndair CL6002B19 · Door System WiringSDR REXA201200114Engine · vibrationAIR RETURN AT 10,000 FEET AIRCRAFT STARTED SMALL VIBRATION, UNUSUAL SOUND FROM RIGHT SIDE OF AC, RIGHT ENGINE ITT WAS POINTING TO 12 O`CLOCK, RAN QRH, SHUTDOWN ENGINE, RETURNED TO DTW. REMOVED AND REPLACED RT ENGINE IAW AMM 71-00-00. REFERENCE DISC NR 1 AML Jan 12, 2012 · N8896A · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA120112001Angle · cracked(CAN) THE AME WAS PERFORMING A INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION FOR TASK RJ2-57-900-320 WHEN HE FOUND CRACKS EMINATING FROM EACH OF THE 2 RELIEF CUTOUTS FOR THE STRINGERS IN THE WEB OF THE SUPPORT ANGLE, PN: 601R10011-13 AND ANGLE PN:601R10Jan 12, 2012 · Cndair CL6002B19 · Wing Miscellaneous Structure
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