GE CF34-8C5

Service difficulty reports · 772

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 = 'CF348C5'
  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 MASA2011080103373Engine · vibrationLEFT ENG VIBE 2.0 DURING CLIMB AT FL 360; PERFORMED ENGINE BLADE INSPECTION AND BLADE SHAKE OPS GOOD ENGINE RUNS NORMAL. IDLE .03 / HIGH POWER .07.Jul 31, 2011 · N905J · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA110803018Starter · lack of lubeMX WERE CALLED TO PERFORM A MANUAL START ON THE ACFT AFTER THE ENGINE WOULD NOT CRANK AFTER SELECTED. WHEN THEY OPENED THE COWLINGS THEY FOUND THE STARTER IN PIECES. AFTER ENSURING THERE WAS NO FURTHER DAMAGE TO THE ENGINE THE STARTER AND START VALVE WERE REJul 31, 2011 · Cndair CL600* · Engine StarterSDR MASA2011080103358Engine · vibrationNR 1 ENG VIBE 3.5 INFLT AT CRUISE. SHOOK BLADES AND APPLIED TEMP RO.Jul 29, 2011 · N929LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MALA110172Transcowl · damagedHOLES IN RT UPPER TRANSCOWL UNDER OTBD NYLON INSERT ARE ELONGATED. COMPLIED WITH EO R78009, REO 690-78-30-126, REO 670-78-34-293 FOR REPAIR.Jul 28, 2011 · N916XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR MASA2011071103183Blade · lack of lubeNR 1 ENGINE VIBE IN FLIGHT 1.9 MILS. C/W BLADE LUBE & RAN ENGINES.Jul 7, 2011 · N911FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011071103184Engine · vibrationNR 1 ENG VIBE AT 1.8 IN FLT. CW FAN BLADE INSP NO DAMAGE.Jul 7, 2011 · N911FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA110628002Windshield · crackedON CLIMB, RT WINDSHIELD CRACKED. FLIGHT ABORTED. MX REPLACED RT WINDSHIELD.Jun 28, 2011 · Cndair CL6002D24 · Flight Compartment WindowsSDR JR2R2011062600268Stand Off · crackedLEFT ENGINE UPPER TRANS COWL HAS BROKEN STANDOFF.Jun 26, 2011 · N908FJ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR JR2R2011062600269Stand Off · crackedLEFT ENGINE LOWER TRANS COWL HAS BROKEN STANDOFF.Jun 26, 2011 · N908FJ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR MASA2011061603033Garlock Seal · damagedDIVERT LT ENG OIL LOSS IN FLIGHT. R2 EDP GARLOCK SEAL, SERVICED ENGINE OIL. GENERATED M055 FOR DAILY CHIP DETECTOR INSPECTION FOR NEXT 50FH DUE TO ENG.Jun 15, 2011 · N928LR · Cndair CL6002D24 · Turbine Engine Oil SystemSDR REXA201100348Blades · dirtyAIR RETURN RT ENG VIBE 2.0 IN FLT. MTX WILL PERFORM ENG TANG BLADE LUBE BLADES HAVE BEEN REMOVED CLEANED AND LUBED WILL START THE INSTALL PROCESS NOW IAW AMM 72-20-00. Jun 6, 2011 · N186PQ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2011060702964Engine · overheatedLEFT ENGINE OVERTEMP 965 FOR 4.1 SECONDS. R & R LT ENGINE.Jun 6, 2011 · N925FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR JR2R2011060300232Mount · gougedRIGHT FORWARD ENGINE MOUNT LUG GOUGED.Jun 3, 2011 · N907FJ · Cndair CL6002D24 · Engine Mount SectionSDR CA110607009Acm · overheatedDURING FLIGHT, LT PACK AUTOFAIL MESSAGE IS SHOWN ON EICAS. CREW REVERTS TO MANUAL AND SYS SEEMS TO WORK OK. ON APPROACH TO MAD AIRPORT, CREW NOTICES A BURNED ODOR AND SMOKE IN CABIN. CAPTAIN DECIDES TO DISCONNECT THE LT PACK AND CONTINUE THE OPERATION WITH JUJun 1, 2011 · Cndair CL6002D24 · Cabin Cooling SystemSDR MASA2011052702878Engine · vibrationNR 1 ENG N1 VIB AT 3.0 LEVEL FLIGHT. C/W RO.May 26, 2011 · N926LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MALA110133Selector Valve · inoperativeUPON DEPARTURE, RECEIVED A "GEAR DISAGREE" WARNING. RETURNED TO BDL AFTER BURNING FUEL TO PREVENT OVERWEIGHT LANDING. ACCESSED CURRENT FAULTS SHOW 005968 NO GEAR MOVEMENT. DEFERRED LANDING GEAR RETRACTION STS IAW MEL 32-30-1A. MX PROCEDURES C/W. REPLACED May 25, 2011 · N931XJ · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR MASA2011052602864Engine · overheatedRT ENG ITT REACHED 968 FOR 6 SECONDS. PERFORMED COMP WASH TEMP AFTER WASH 922.May 25, 2011 · N933LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011052502852Engine · overtempLT ENG OVER TEMP AT 973 DEG ON TAKEOFF, ATO. MX WORKING.May 24, 2011 · N915FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011052402839Engine · dirtyATO RIGHT ITT AT 960 DEG FOR 4 SECONDS. COMPLIED WITH COMP WASH RAN ENG OPS CHECKED.May 23, 2011 · N932LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011052302801Engine · vibrationRTG NR 1 ENG N1 VIB 1.9 DURING TAXI. C/W BLADE SHAKE.May 20, 2011 · N930LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011052002790Fan Blade · vibrationNR 2 ENG FAN VIBE IN FLT AT 2.0. PERFORMED BLADE SHAKE AND RAN ENGINES WITH CREW. VIBE WITHIN LIMITS. APPLIED 50 CYCLE RO FOR BLADE LUBE.May 19, 2011 · N938LR · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2011051702762Engine · dirtyRT ENG EXCEEDANCE TO 968 DEG C ON TAKEOFF. COMPLY WITH COMP WASH.May 16, 2011 · N909FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA110601002A/C Pack · failedDURING FLIGHT, LEFT PACK AUTOFAIL MESSAGE IS SHOWN ON EICAS. CREW REVERTS TO MANUAL AND SYS SEEMS TO WORK OK. ON APPROACH, CREW NOTICES A BURNED ODOR AND SMOKE IN CABIN. CAPTAIN DECIDES TO DISCONNECT THE LT PACK AND CONTINUE THE OPERATION WITH JUST ONE PACK. May 15, 2011 · Cndair CL6002D24 · Cabin Cooling SystemSDR MASA2011051602728Engine · vibrationENG 1 N1 VIBE AT 2.0 IN CRUISE. SHOOK BLADES, ENG RUN AT .4MILS.May 14, 2011 · N921FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MALA110124Light · missingEMERGENCY FLOOR TRACK LIGHTING STRIP IN FRONT OF FWD COAT CLOSET CAME OFF. INSTALLED EMERGENCY FLOOR TRACK LIGHTING STRIP IN FRONT OF FWD COAT CLOSET IAW AMM 33-51-00.May 14, 2011 · N935XJ · Cndair CL6002D24 · Emergency LightingSDR CA110506003Control Unit · failed(CAN) DURING ROUTINE MAINTENANCE, NEITHER STAB TRIM CHANNELS WOULD ENGAGE. AFTER COMPLETING SPOST TEST, FAULT "H STAB/MCU/ACOFF/PHASE MISSING CH1" AND "H STAB/MCU/ACOFF/PHASE MISSING CH2" DISPLAYED. CHECKED AC SERVICEABLE ALL THE WAY TO THE H STAB ACTUATOR MOTMay 6, 2011 · Cndair CL600* · Stabilizer Control SystemSDR MASA2011050602641Actuator · faultyNR 2 ENGINE LEAKING FUEL. R2 NR 2 ENGINE MASTER VG ACTUATOR.May 5, 2011 · N919FJ · Cndair CL6002D24 · Compressor Bleed ControlSDR MASA2011050302584Unknown · leakingLT ENG FUEL LEAKING. TURNED OFF BOOST PUMP. LEAK CHECK GOOD.May 2, 2011 · N911FJ · Cndair CL6002D24 · Engine Fuel DistributionSDR MASA2011042502507Engine · dirtyNR 2 ENG ITT 970 AT T/O PWR APROX 10 SEC. MX PERFORMED COMPS WASH AND POWER ASSURANCE RUNS, OPS CHECKS GOOD.Apr 22, 2011 · N922FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011042202484Unknown · malfunctionedRT ENG DEGRADED CTN IN FLT. MX RAN ENGINE 3 TIMES NO FURTHER FAULTS NOTED.Apr 21, 2011 · N914FJ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2011042202485Fadec · malfunctionedLEFT ENGINE DEGRAD CAUTION MSG IN FLT. R2 LT FADEC.Apr 21, 2011 · N929LR · Cndair CL6002D24 · Fuel Control/Turbine EnginesSDR MASA2011042102474Engine · vibrationRT ENG N1 VIBE 1.2 DURING CLIMB. SHOOK BLADES RAN ENGINE VIBE WENT TO 0.4.Apr 20, 2011 · N916FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA110419005Torque Tube · corroded(CAN) A LEFT FLAP TORQUE TUBE, PN 5912578-10 WAS REMOVED TO FACILITATE THE INSTALLATION OF A FLAP ACTUATOR. A NOISE WAS HEARD COMING FROM INSIDE THE TUBE WHEN IT WAS TIPPED END TO END. THE SPLINED ENDS WERE DERIVETED TO INVESTIGATE. A LARGE AMOUNT OF CORROSIApr 19, 2011 · Cndair CL600* · Trailing Edge Flap Control SystemSDR CA110415003Receptacle · meltedDURING A HEAVY MX CHECK, THE BASE FOR THE COFFEE MAKER ON ACFT WAS FOUND TO BE MELTED FROM THE HEATING ELEMENTS. BASE REPLACED.Apr 14, 2011 · Cndair CL600* · Buffet/GalleysSDR MALA110091Support Angle · bentRT HORIZONTAL STAB TIP FAIRING SUPPORT ANGLE BENT OTBD OF STAB END RIB UNDER PANEL 343BR/343AR. FABRICATED NEW RT STAB TIP RIB IAW EO AV670-23248 AND INSTALLED IAW SRM 51-42-06.Apr 13, 2011 · N909XJ · Cndair CL6002D24 · Horizontal Stabilizer StructureSDR MASA2011041502412Seal · leakingENG FUMES IN COCKPIT DURING TRANS PWR CHANGE. R2 SEAL PRESSSURE REGULATING VALVE.Apr 12, 2011 · N934FJ · Cndair CL6002D24 · Compressor Bleed ControlSDR MASA2011040802369Blade · lack of lubeNR 2 ENG VIBE AT 1.8 MLS IN FLT. MX PERFORMED BLADE LUBE.Apr 6, 2011 · N932LR · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2011040702358Spinner · vibrationHIGH CONT NR 1 ENG VIB 2.8 MILS CRUISE - RTF. MX REMOVED AND REPLACED SPINNER CORRECTLY AND PERFORMED ENGINE RUNS. VIBE W/IN LIMITS.Apr 5, 2011 · N928LR · Cndair CL6002D24 · Turbine Engine Air Inlet SectionSDR MALA110080Light · missingEMERGENCY LIGHTING IN FRONT GALLEY MISSING. INSTALLED NEW LIGHTING STRIP PN PL88-900LH00 IAW 33-51-01.Apr 4, 2011 · N918XJ · Cndair CL6002D24 · Emergency LightingSDR MALA110079Stringer · damagedFOUND DAMAGED STRINGER NR 8R AT STA 1155 DAMAGE DEPTH .053, W .2958, L .622. DAMAGE REMOVED FROM STR 8R ES 1162,00 AND TEMPORARY REPAIRED IAW REO 690-53-61-161. ALSO, INITIATED PWI TO COMPLETE PERMANENT REPAIR WITHIN 1200 FLT HRS.Apr 1, 2011 · N919XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR MALA110072Light · damagedFLOOR LIGHTING IN FRONT OF FWD LAV IS DAMAGED. R & R DAMAGED FLOOR LIGHTING IN FRONT OF LAV IAW AMM 33-51-01. NO FURTHER ACTION REQUIRED.Mar 29, 2011 · N908XJ · Cndair CL6002D24 · Emergency LightingSDR MASA2011040102298Compressor · lack of lubeENG 1 FAN VIBE UP TO 1.7 IN TRANSIENT. MX C/W FAN BLADE LUBE, ENGINE RUN CHECK VIBE IS 0.3 MILS.Mar 29, 2011 · N929LR · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MALA110073Floor Panel · damagedDURING GVI ZONE, FOUND FLOOR PANEL VERY SOFT. REPAIRED FLOOR PANEL USING REG 0670-53-00-087 AS REF.Mar 28, 2011 · N920XJ · Cndair CL6002D24 · Fuselage Floor PanelSDR MASA2011032202220Engine · overtempNR 1 ENGINE OVERTEMP ATO RTG. MX RAN ENGINE PER AMM COULD NOT DUPLICATE.Mar 20, 2011 · N915FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MALA110074Drag Angle · crackedROUTINE CHECK, PAX DOOR AFT DRAG ANGLE APPEARS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 670-52-11-072.Mar 18, 2011 · N601LR · Cndair CL6002D24 · Passenger/Crew DoorsSDR MALA110076Seat Track · corrodedRT SIDE FWD SEAT TRACK IN FRONT OF LAV AND BEHIND G2 GALLEY CORRODED ON MOST FWD SEGMENT. R & R FWD SEAT TRACK RAIL IAW AMM 53-00-49-400-801.Mar 18, 2011 · N601LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR MASA2011031702175O-Ring · leakingRT ENG LEAKING FUEL. MX REPLACED RT ENGINE OBV PLUG O-RING, OPS CHECK GOOD.Mar 15, 2011 · N931LR · Cndair CL6002D24 · Compressor Bleed ControlSDR MASA2011031402141Compressor Blade · lack of lubeENG 2 VIBE 1.8 AT 82% & 2.2 AT 87% N1. MX C/W FAN BLADE LUBE AND REPLACED BLADE PINS.Mar 11, 2011 · N930LR · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR CA110314008Control Unit · failed(CAN) RUDDER LIMITER CAUTION MESSAGE APPEARS ON ED1. SPOILER STABILIZER CONTROL UNIT FOUND INOPERATIVE. SSCU REPLACED AND AIRCRAFT RETURNED IN SERVICE.Mar 10, 2011 · Cndair CL6002D24 · Drag Control SystemSDR MALA110057Skin · chafedDURING ROUTINE CHECK, PANEL CARD, FOUND CHAFING ON FUSELAGE SKIN NEAR F/S 913 TO 919 FROM CHANNEL AFT FAIRING. INSPECTED CHAFE AND FOUND TO BE, 008. BLENDED AND APPLIED TOPCOAT IAW REO 670-63-00-014.Mar 7, 2011 · N907XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
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