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 LEJM2011FA0000421O-Ring · failedDURING AN UNRELATED MX GROUND RUN, THE NR1 IDG OVERHEATED, A BOLT AND A O-RING ON THE GENRERATOR MODULE FAILED, AND THE LUBRICATING OIL SPRAYED UNDER HIGH PRESSURE ONTO THE CORE OF AN OPERATING ENGINE. THE ENGINE WAS IMMEDIATELY SHUTDOWN. THERE WAS A LARGE SMJun 27, 2011 · N591ML · Cndair CL6002B19 · AC Generator-AlternatorSDR SWIA201126580Carbon Seal · damagedSHUT DOWN THE RIGHT ENGINE DUE TO OIL PRESSURE WARNING MESSAGE. (FLT 6396) REPLACED CARBON SEALS ON ACCESORY GEARBOX.Jun 26, 2011 · N925SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201140725Seal · chafedLT UPPER NOSE COWL T/E SEAL CHAFED. R & R LT UPPER NOSE COWL SEAL IAW CMM 71-14-01.Jun 24, 2011 · N463AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140708Skin · chafedRT LOWER CORE COWL T/E CHAFED. REPAIRED IAW REO 601R-71-12-3276.Jun 24, 2011 · N462AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR CA110624005Nut · misinstalledSCHEDULED HEAVY MX WAS BEING PERFORMED ENGINE. DURING SEPARATION OF THE STAGE 1 AND 2 HIGH PRESSURE TURBINE DISKS, ONE RETAINING STUDS WAS HEARD TO UNSEAT AND FALL ONTO THE STAGE 2 DISK. WHEN THE 2 DISKS WERE SEPARATED, THE NUT WAS EVALUATED AND WITNESS MARKJun 23, 2011 · Turbine SectionSDR REXA201100401Engine · malfunctionedLT ENGINE OIL PRESS FLUX. REMOVED AND REPLACED LT ENGINE IAW CRJ AMM 71-00-00, OP CHECK GOOD. OK FOR SERVICE.Jun 19, 2011 · N8477R · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA110623003Scavenge Pump · fluctuates(CAN) LEFT ENGINE OIL LOW PRESSURE WARNING MESSAGE AT FL290. PSI FLUCTUTATING BETWEEN 19-35 PSI WITH OIL TEMP AT 137 DEGREES. DID NOT SHUTDOWN ENGINE AND LANDED AT AIRPORT .Jun 17, 2011 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201140709Strip · chafedRT ENG UPPER NOSE COWL AFT SEAL STRIP IS KNIFE EDGED. REMOVED UNSERVICEABLE AFT EDGE STRIP & REPLACED WITH SERVICEABLE AFT EDGE STRIP IAW CMM 71-14-01-300-814-A01.Jun 16, 2011 · N462AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR CA110617004Structure · departedUPON LANDING, THE RT ENGINE LOWER FAN COWL, FELL OFF THE ACFT ON THE RUNWAY. THE ACFT TAXIED TO THE GATE UNEVENTFULLY. INVESTIGATION REVEALS THAT THE ACFT HAD AN A1 CHECK THE NIGHT BEFORE AND THE COWLS WERE OPEN. THIS WAS THE SECOND LANDING OF THE DAY WHENJun 16, 2011 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140707Skin · chafedRT UPPER CORE COWL T/E CHAFED. REPAIRED UPPER CORE COWL T/E IAW REO 61R-71-12-3276.Jun 15, 2011 · N462AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140653Bracket · crackedRT ENGINE NOSE INLET FAN CASING WIRE HARNESS BRACKET CRACKED 8 O`CLOCK POSITION AFT END. REPAIRED RT HOSE INLET FAN CASING WIRE HARNESS BRACKET CRACKED AT 8 O`CLOCK POSITION BY INCORPORATING REO 601R-71-61-3941.Jun 12, 2011 · N434AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA201140654Torque Box · crackedRT ENGINE TORQUE BOX AFT FLANGE CRACKED AT FASTENER LOCATION 5 O`CLOCK. REPAIRED IAW REO 601R-78-34-2527, REV B.Jun 11, 2011 · N434AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140659Flange · crackedLT ENGINE TORQUE BOX FLANGE CRACKED AT 7 O`CLOCK POSITION BELOW SKIN PANEL BRACKET. REPAIRED IAW REO 601R-78-34-2527, REV B.Jun 11, 2011 · N434AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140500Engine · failedIN CLIMB, BETWEEN 8000-8500 FT A/P LT ENG MADE LOUD BANG FOLLOWED BY SHUDDERING AND VIBRATION ITT WELL ABOVE 900 DEGREES. BROUGHT LT ENGINE THRUST TO IDLE VIBRATION DAMPENED. ADVANCED ENGINE THRUST, BROUGHT NO ADDITIONAL THRUST RAN IMMEDIATE ACTION CHECKLISTJun 10, 2011 · N419AW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA201140646Link · chafedLT ENGINE NR 10 BLOCKER DOOR LINK ARM CHAFING DAMAGE BLENDED CHAFED AREA LT NR 10 BLOCKER DOOR LINK ARM MATERIAL LOSS .007 REMAINING MATERIAL .193. FOUND TO BE WITHIN LIMITS IAW REO 601R-78-30-2940.Jun 10, 2011 · N434AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA110606010Sensing Element · failed(CAN) IN CRUISE, FLIGHT CREW RECEIVED A LT 14TH DUCT WARNING MESSAGE. THE AFFECTED ENGINE POWER LEVER WAS REDUCED TO FLIGHT IDLE, THE CREW DECLARED AN EMERGENCY AND DIVERTED TO THE NEAREST SUITABLE AIRPORT. MX FOUND A FAULTY HEAT SENSING ELEMENT. THE LT PYLOJun 5, 2011 · Cndair CL6002B19 · Overheat DetectionSDR A6WA201140657Skin · chafedRT ENGINE UPPER CORE COWL T/E IS CHAFED KNIFE EDGED. REPAIRED CHAFED/KNIFE DAMAGE ON EDGE AFT T/E RT ENGINE UPPER CORE COWL IAW REO 601R-71-12-3276, REV. NC.Jun 4, 2011 · N434AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140660Blocker Door · chafedALL RT THRUST REVERSER BLOCKER DOORS ARE CHAFED ALONG THE BACK SEAL WHERE THEY CONTACT THE STOPS. REPAIRED DOORS NR 1 TO 5 AND 7 TO 10 ON RT T/E BLOCKER DOOR IAW CMM 78-30-00, SRS 100 AND REPLACED DOOR NR 6.Jun 3, 2011 · N434AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA110601003Access Door · departedTHE THRUST REVERSER ACCESS COWLS FOUND MISSING DURING TAXI AFTER LANDING.May 30, 2011 · Cndair CL6002B19 · Engine Thrust ReverserSDR REXA201100313Engine · smokeCREW REPORTED SMOKE IN LAV. FIRE DEPARTMENT CALLED, PAX DEBOARDED ON THE RAMP. RUNNING THE ENG CAUSES THE CABIN TO SMELL LIKE SMOKE. GOING TO BORESCOPE LT ENG. STILL IN WORK FOR RESULTS.May 26, 2011 · N8745B · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2011060200018Engine · malfunctionedCREW REPORTED LEFT ENGINE OIL PRESSURE DROPPED TO ZERO PSI IN FLIGHT EN ROUTE FROM CLT TO PGV. CREW SHUT DOWN LEFT ENGINE, DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFMay 26, 2011 · N245PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA2011053100017Oil Tank · faultyCREW REPORTED RIGHT OIL PRESSURE FLUCTUATING BETWEEN 57 AND 62 PSI ON CLIMBOUT FROM CLT. PRESSURE STABILIZED BELOW 60 PERCENT N1. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT RIGHT ENGINE OIL SYSTEM, SWAPPED RIGHT May 25, 2011 · N248PS · Cndair CL6002B19 · Engine Oil Storage (Airframe Furnished)SDR MASA2011052302826Blade · lack of lubeLEFT N2 VIBE CTN IN FLT. MX R2 ENG BLOCKER DOOR, LUBE SCAVENGE FILTER, PERFORM BLADE LUBE.May 22, 2011 · N77260 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR ASOA201101069Angle · corrodedWHILE ACCESSING FOR REPAIR TO INTERCOSTAL AT FS 349 FOUND SERVICE DOOR ANGLE TO BE CORRODED. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06, 51-42-21, AND 51-42-04.May 20, 2011 · N885AS · Cndair CL6002B19 · Service DoorsSDR CA110526005Selector Valve · malfunctionedON APPROACH AFTER A 5 HR FLIGHT THE CREW SELECTED GEAR DOWN. THE MAIN GEAR EXTEND, THE NOSE DOORS OPEN BUT THE GEAR REMAIN IN THE NOSE WELL. THE GEAR DISAGREE WARNING ILLUMINATES. CREW EXECUTES A GO-AROUND, THE CREW SELECTS MANUAL GEAR RELEASE. THE NOSE GEAMay 20, 2011 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA201101022Floorbeam · crackedFS 280, FLOORBEAM CRACKED INBD SIDE OF RBL 9. REPAIRED IAW REO 601R-53-11-926.May 18, 2011 · N885AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101024Angle · corrodedFLOOR SUPPORT INTERCOASTAL J-ANGLE CORRODED AT FS 349, RBL 45. REMOVED ANGLE IAW SRM 51-41-06, 5142-01 AND 51-41-02. FOUND ANGLE TO BE CORRODED BEYOND REPAIRABLE LIMITS IAW 53-00-00. REPAIRED IAW REO 601R-53-21-1290.May 18, 2011 · N885AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2011051800009Seal · blownCREW REPORTED LEFT ENGINE OIL PRESSURE MASTER WARNING AND TRIPLE CHIME SHORTLY AFTER TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND SEAL BLOWN OUT OF LEFT ENGINE OIL PRESSURE TRANSDUCER, REMOVED AND REPLACED May 15, 2011 · N242JS · Cndair CL6002B19 · Engine Oil PressureSDR ASOA201101046Panel · dentedPAX DOOR FWD AND AFT CLOSE OUT/CORNER PANELS, TOP END HAVE DENT DAMAGE. COMPLIED WITH REO 601R-52-11-827, REV D AND REO 601R-52-11-827, REV--DATED 11-21-2005 AS WRITTEN THIS IS A MAJOR REPAIR . RII FOUND TO BE SATISFACTORY.May 13, 2011 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR REXA201100284Engine · malfunctionedRIGHT ENG ITT SPIKE PERFORMED ENGINE RUNS AT ALL POWER SETTINGS. NO DEFECTS NOTED IAW AMM 76-10-0.May 10, 2011 · N8884E · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR MASA2011050602623Fcu · faultyRT ENGINE LEAKING FLUID FROM DRAIN. R2 RT ENGINE FUEL CONTROL UNIT.May 4, 2011 · N7291Z · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA110503003Ballast · overheated(CAN) FLIGHT CREW NOTICES A SMOKE ODOR. F/A CONFIRMS SMOKE IN GALLEY, DURATION 10 SECONDS, ATB. ACFT LANDED AT ORIGIN AIRPORT. MAINTENANCE FOUND BALLAST ROW 2 DF WITH OVERHEAT MARKS. BALLAST REPLACED IAW AMM 33-21-01. ACFT RTS.Apr 27, 2011 · Cndair CL6002B19 · Passenger Compartment LightingSDR VNAA2011042600017Pump · shearedCREW REPORTED AN OIL PRESSURE WARNING MESSAGE AT CRUISE. CREW SHUT DOWN ENGINE AND DIVERTED TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED, REPLACED, AND OPERATIONAL CHECKED THE SCAVAGE PUMP USING THE AIRCRAFT MAINTENANCE MANUApr 22, 2011 · N209PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201140297Track · damagedRT THRUST REVERSER INBD LOWER TRACK AND LUG DAMAGED. BLENDED LUG WITHIN LIMITS IAW REO 601R-78-34-2435. R & R WITH INBD TRACK.Apr 18, 2011 · N415AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA110421004Shaft · sheared(CAN) WHEN THE PASSENGER DOOR WAS OPENED THE AFT PAX DOOR COUNTERBALANCE BRACKET SHAFT FAILED FOLLOWED BY THE FWD COUNTERBALANCE BRACKET SHAFT. THIS ALLOWED THE DOOR TO FREEFALL TO THE GROUND WITH POTENTIAL TO CAUSE SERIOUS INJURY TO ANYONE OUTSIDE OF THE Apr 17, 2011 · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140285Skin · dentedOUTER SKIN DENTED ON 435AT UPPER CORE COWL. REPAIR DENTED DAMAGE ON OUTER SKIN UPPER CORE COWL.Apr 16, 2011 · N415AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR VNAA2011042100012Access Panel · departedLEFT UPPER ENGINE COWL DEPARTED AIRCRAFT DURING LANDING ROLL AT DCA. MAINTENANCE INSPECTED AIRCRAFT, REPLACED UPPER NOSE COWL ACCESS PANEL ON LEFT ENGINE, REMOVED AND REPLACED LOWER NOSE COWL ACCESS PANEL ON LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAIApr 15, 2011 · N246PS · Cndair CL6002B19 · Engine Cowling SystemSDR A6WA201140286Skin · chafedINNER SKIN ON LT TAIL PIPE FAIRING CHAFED IN 2 AREAS MARKED. REPAIRED CHAFED AREAS ON LT TAIL PIPE IAW CMM 78-11-00 AND REO 601R-78-10-1173.Apr 15, 2011 · N415AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR VNAA2011041500011Engine · failedCREW REPORTED RIGHT ENGINE OIL PRESSURE CAS MESSAGE, AURAL WARNING AND ENGINE OIL PRESSURE AT 20 PSI EN ROUTE FROM DCA TO TYS AT FL300. CREW SHUT DOWN RIGHT ENGINE PER QRH, DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLAApr 12, 2011 · N216PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201140424Skin · chafedLT LOWER CORE COWL CHAFED ON OUTER SKIN NEXT TO DOUBLE LATCH, C/W CMM 71-12-01.Apr 12, 2011 · N415AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140293Structure · chafedT/E OF RT LOWER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT LOWER NOSE COWL IAW CMM 71-14-01.Apr 10, 2011 · N415AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140291Strip · chafedT/E STRIP ON RT UPPER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT UPPER NOSE COWL IAW CMM 71-14-01.Apr 10, 2011 · N415AW · Cndair CL6002B19 · Engine Cowling SystemSDR MASA2011040702348Fuel · leakingNR 2 ENGINE FUEL LEAK AND FIRE DURING RUN-UP CHECKS. REMOVED AND REPLACED NR 2 ENGINE.Apr 4, 2011 · N77302 · Cndair CL6002B19 · Engine Fuel DistributionSDR A6WA201140340Structure · crackedLT T/R UPPER INBD CASCADE CRACKED. REPAIRED LT T/R UPPER INBD CASCADE IAW PROCESS SPECIFICATION 1, DWG AW78-30-0711-04.Apr 4, 2011 · N417AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140370Cowl Door · chafedLT LOWER CURE COWL CHAFED BY FWD LATCHES. BLENDED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLER.Apr 1, 2011 · N459AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR MASA2011033102288Engine · malfunctionedLEFT ENG OIL PRESS WARNING & READING 0 ON DESCENT INTO ABQ. CREW PULLED THE NR 1 THROTTLE BACK TO IDLE AND CONTINUED THE DESCENT. MX REMOVED AND REPLACED LT ENGINE, ENG RUN C/W.Mar 28, 2011 · N7291Z · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA201125890Carbon Seal · defectiveSMOKE TOILET CAUTION MESSAGE. (FLT 6954) REPLACED NR 1 CARBON SEAL ON THE RIGHT ENGINE.Mar 27, 2011 · N978SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201140315Latch · wornLT LWR CORE COWL AFT OF FWD DOOR LATCH IS WORN. REPAIR IAW CMM 71-12-01.Mar 23, 2011 · N413AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR VNAA2011032500017Wire Harness · chafedCREW REPORTED LEFT ENGINE UNCOMMANDED ACCELERATION AND N1 RED, WITH INDICATION WELL ABOVE 100 PERCENT DURING CLIMBOUT FROM CLT. ALL OTHER LEFT ENGINE INDICATIONS WERE TRACKING HIGHER PRIOR TO THRUST REDUCTION. CREW FOLLOWED QRH, RETURNED TO CLT AND LANDED WIMar 22, 2011 · N230PS · Cndair CL6002B19 · Engine Fuel System WiringSDR VNAA2011032300016Pin · not seatedCREW REPORTED UNCOMMANDED LEFT ENGINE ACCELERATION DURING CLIMBOUT FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESEATED AN UNSEATED PIN ON FUEL CONTROL UNIT TORQUE MOTOR CIRCUIT HARNESS CONNECTOR AND PERFORMED CHECKS Mar 19, 2011 · N230PS · Cndair CL6002B19 · Engine Fuel System Wiring
Back to GE CF34-3B1