GE CF34-8C5

Service difficulty reports · 772

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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 CA120627015Compressor · damaged(CAN) THE CLIMB THE NR 1 ENGINE LET OUT A SHUDDER AND THE ITT ROSE TO 950 DEGREE C FROM APPROXIMATELY 840 DEGREES C. THE CREW LEVELED OFF AND ALL APPEARED NORMAL OTHER THAN THE ITT WAS ABOUT 100 DEGREES HIGHER THAN THE NR 2 AT CRUISE POWER. THE CREW ATTEMPTEJun 25, 2012 · Bombdr CL6002D15 · Turbine Engine Compressor SectionSDR CA120619008Control Unit · failed(CAN) DURING CRUISE FLIGHT THE CREW RECEIVED OTBD FLIGHT SPOILER & OTBD SPOILERON EICAS MESSAGES. IF WAS CONFIRMED THAT THE LT MULTI-FUNCTION SPOILER WAS NOT MOVING. A DECISION WAS MADE TO DIVERT & THE ACFT LANDED UNEVENTFULLY. TROUBLESHOOTING REVEALED THE Jun 18, 2012 · Bombdr CL6002D15 · Drag Control ActuatorSDR CA120625003Sensor · failed(CAN) WHILE IN CRUISE FLIGHT AT FL390 THE FLAP FAIL CAUTION MESSAGE CAME ON. A FLAP ZERO LANDING WAS CARRIED OUT UNEVENTFULLY. ALTHOUGH THE FLIGHT CREW DID REQUEST EMER SERVICES ON STANDBY, NO EMER WAS DECLARED. INVESTIGATION FOUND THE LT INBD FLAP SKEW SENJun 16, 2012 · Bombdr CL6002D15 · Trailing Flap Position Indicating SystemSDR CA120523018Cable · frayed(CAN) AFTER FINDING A BROKEN ICE BREAK CABLE ON ANOTHER ACFT, SEVERAL OTHER ACFT IN THE FLEET WERE CHECKED. THIS ACFT HAD A BADLY FRAYED ICE BREAK CABLE IN THE MAIN CABIN DOOR. THE CABLE ATTACHES TO THE PRESSURE VENT FLAP ON THE DOOR. SHOULD THIS CABLE BREAMay 18, 2012 · Bombdr CL6002D15 · Passenger/Crew DoorsSDR CA120523019Cable · frayed(CAN) AFTER FINDING A BROKEN ICE BREAK CABLE ON ANOTHER ACFT, SEVERAL OTHER ACFT IN THE FLEET WERE CHECKED. THIS ACFT HAD A BADLY FRAYED ICE BREAK CABLE IN THE MAIN CABIN DOOR. THE CABLE ATTACHES TO THE PRESSURE VENT FLAP ON THE DOOR. SHOULD THIS CABLE BREAMay 18, 2012 · Bombdr CL6002D15 · Passenger/Crew DoorsSDR CA120516002Cable · broken(CAN) CREW COULDN`T OPEN THE MAIN CABIN DOOR. MAINTENANCE WAS DISPATCHED TO THE ACFT, UPON ARRIVAL THE DOOR HAD BEEN OPENED. INITIAL INSPECTION OF THE MCD REVEALED THE ICE CABLE 601R318127-3 WAS BROKEN. FURTHER TROUBLESHOOTING INDICATED THE MCD PRESSURE VENTMay 15, 2012 · Bombdr CL6002D15 · Passenger/Crew DoorsSDR CA120501001Drag Angle · cracked(CAN) DURING A VISIT TO A PAINTING FACILITY, CRACKS WERE FOUND ON THE LT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE BRACKETS, FORWARD AND AFT. THE ACFT WAS FLOWN IAW GREO 690-55-31-010. REPAIR BEING ACCOMPLISHED IAW DWG 670-51-00-066.Apr 30, 2012 · Bombdr CL6002D15 · Vertical StabilizerSDR CA120502003Adc · failed(CAN) ON TAKEOFF, 10 KTS DIFFERENCE BETWEEN IAS INDICATORS.Apr 23, 2012 · Cndair CL6002D24 · Air Data ComputerSDR CA120423019Starter · inoperative(CAN) NR 2 ENGINE NOT STARTING. START VALVE DOES NOT OPEN WITH APU AIR AT 43PSI OR WITH CROSSBLEED START AT 48PSI. MAINTENANCE TRIED TO DO A MANUAL START IN ORDER TO DEFER THE VALVE, BUT VALVE WAS OUT OF ALIGNMENT. OPENED COWLS TO REALIGN VALVE FOR MANUAL STApr 21, 2012 · Bombdr CL6002D15 · Engine StarterSDR CA120424002Servo · failed(CAN) WHILE IN CRUISE WITH AUTOPILOT IN NAV MODE, A/P INITIATED A LT TURN AND ACFT BANKED TO THE LT FURTHER THAN REQUESTED. "A" WAS DISPLAYED IN THE CAPT`S PFD. CREW HAD TO DISENGAGE AUTOPILOT TO CORRECT BANK. CREW RE-ENGAGED AUTOPILOT AFTERWARDS, SYS WORKEApr 18, 2012 · Bombdr CL6002D15 · Autopilot Main ServoSDR REXA2012040300475Blade · lack of lubeNR 1 ENGINE FAN VIBRATION, 1.8 IN CAUTION RANGE AT FLT LVL 320. PERFORMED FAN BLADE TANG LUBRICATION IAW AMM 72-21-02. PERFORMED HIGH POWER ENGINE RUN. OPS CHECKED GOOD. OK FOR SERVICE.Apr 3, 2012 · N176PQ · Cndair CL6002D24 · Turbine Engine Air Inlet SectionSDR CA120323001Bearing · lack of lube(CAN) DURING THE TAXI CONTROL MOVEMENT CHECK IT WAS NOTED BY THE FLIGHT CREW THAT THE ELEVATOR CONTROL REQUIRED AN UNUSUALLY HIGH AMOUNT OF FORCE TO MOVE IT. THE STIFFNESS WAS ALSO NOTED DURING ROTATION AND FLARE ON THE PREVIOUS FLIGHT. MAINTENANCE INVESTIGAMar 20, 2012 · Bombdr CL6002D15 · Elevator Control SystemSDR CA120312017Duct · ruptured(CAN) RT BLEED DUCT IN FLIGHT AT FL 300 ACTION: FLIGHT CREW COMPLIED WITH PROCEDURE. CRACKED BLEED CROSSOVER DUCT REPLACED CROSSOVER DUCT. CROSSOVER DUCT ASSY GG670-80301-1.Mar 5, 2012 · Cndair CL6002D24 · Pneumatic Distribution SystemSDR CA120306003Anti-Skid Sys · failed(CAN) BRAKE OVERHEAT, APPEARS ON ED1. RTO, RETURN TO PARKING. MAINTENANCE FOUND BTMS NR 2 INDICATION AT 14 AND COLD. MAINTENANCE REPLACED ANTI-SKID CONTROL UNIT (ASCU), TEST OK, ACFT RTS.Mar 4, 2012 · Cndair CL6002D24 · Brake Anti-Skid SectionSDR REXA2012030300293Blade · lack of lubeAIR RETURN L FAN VIB IN YELLOW AT FL 340 L FAN VIB INDICATIONS WERE 2.1-2.3 OIL TEMP/PRESSURE NORMAL ENTIRE FLIGHT INITIAL DESCENT AT FL 340 VIB RANGED FROM 2.3-2.8 AT 16000 N1-67.9 L FAN VIB GREEN AT 1.7 AT 10000 N1 67.3 L FAN VIB-1.5 TURNED ON COWLS-NO ICE. Mar 3, 2012 · N197PQ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR CA120302001Wire · chafed(CAN) DURING MAINTENANCE INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD AT EACH OF 4 LOCATIONS IN THE L/E OF THE LT AND RT WINGS, 2 PER SIDE. THE SPIRAL ELECTRICAL CORD MAKES THE REQUIRED ELECTRICAL CONNECTIONS BETWEEN THE SLAT AND THE WING. Mar 1, 2012 · Bombdr CL6002D15 · Ice/Rain Protection System WiringSDR CA120314003Aileron Sys · binding(CAN) DURING APPROACH THE FLIGHT CREW RECEIVED A AP RIGHT WING DOWNÏ¿½ CAUTION MESSAGE AND THE A/C CONTINUED IN THE LH TURN. THE CREW RETRACTED THE FLIGHT SPOILERS AS THEY WERE DEPLOYED AT THE TIME AND THEN THE AP DISENGAGED ITSELF. AT THIS POINT THE CREW NOTEFeb 29, 2012 · Cndair CL600* · Autopilot Main ServoSDR REXA2012022000041Engine · contaminatedAFTER TAKEOFF, FLIGHT ATTENDANT SMELLED BURNING PLASTIC. PILOTS CONFIRMED AN ODOR. RETURN TO DEPARTURE. IDENTIFIED ODOR AS ENGINE WITH SOAP, RESIDUAL FROM ENGINE WASH ON RT ENGINE. RAN ENGINES TO 85 OIL TEMP WITH PACKS ON FULL HOT UNTIL ODOR DISSIPATED. Feb 20, 2012 · N936XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA120217005Feeder Cable · chafed(CAN) DURING INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE OTBD TELESCOPIC DUCT IN THE LT L/E. THE SPIRAL ELECTRICAL CORD MAKES THE CONNECTIONS FOR THE SLAT DISCONNECT SENSORS, THE ANTI-ICE TEMPERATURE SENSORS, AND THE BLEED Feb 17, 2012 · Bombdr CL6002D15 · Wing System WiringSDR CA120220002Fadec · malfunctioned(CAN) RT FADE CAUTION MSG ON GROUND. AFTER TAKEOFF ITT REMAINDED AT 915-929 DEGREES UNTIL 5000 MSL. ENGINE WOULD NOT SYNC RT ENGINE WOULD NOT STABLILIZE UNTIL 5000 FT. N1 WAS SYNC N2 WAS .7 PERCENT FASTER ON RT SIDE. THE PROBLEM WAS ORIGINALLY ON THE LT SIFeb 15, 2012 · Cndair CL6002D24 · Fuel Controlling SystemSDR REXA2012021400224Blade · lack of lubeUNSCHEDULED LANDING FOR R ENGINE FAN VIBE 1.8 IN AMBER CAUTION RANGE AT FL 300. RAN QRH. BROUGHT IT BACK TO NORMAL WITH THRUST MANAGEMENT. PERFORMED FAN BLADE TANG LUBE ON RT ENGING IAW AMM 72-21-02. OP CHECK GOOD.Feb 14, 2012 · N228PQ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR ASOA201200368Drag Angle · crackedSUSPECTED CRACK ON AFT DRAG ANGLE. COMPLIED WITH INSPECTION ON AFT DRAG ANGLE IAW REO 690-52-11-026, REV B. NO FURTHER DAMAGE NOTED.Feb 2, 2012 · N134EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR CA120126012Link · cracked(CAN) WING TO FUSELAGE PICKUP LINK REF, PN: SH670-35639-1. ACFT CAME IN WITH DEFECT ATTACHED FOR THE LT LINK BEING ROTATED OR TILTED, TEMP REO 690-53-41-0011 HAD BEEN PREVIOUSLY APPLIED FOR THIS. DURING INSPECTION AT HEAVY MULTIPLE CRACKS WERE FOUND IN THE LJan 26, 2012 · Bombdr CL6002D15 · Wing, Attach FittingsSDR SWIA201229400Engine · failedAT TAKEOFF ROTATION RIGHT ENGINE N1 DROPPED TO 79.37. LEFT ENGINE APR FIRED FOR APPROXIMATELY 5 SECONDS. SHORTLY AFTER TAKEOFF ALL ENGINE INDICATIONS RETURNED TO NORMAL. RIGHT ENGINE OIL LOW PRESSURE STATUS MESSAGE ALSO APPEARED SHORTLY THEN WENT AWAY. (FLJan 19, 2012 · N814SK · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA120126006Compressor · stalled(CAN) CREW REPORTED COMPRESSOR STALL DURING CLIMB OUT. LOAD BANG, VIBRATION, AND N1 SPEED LOSS CAUSING APR ACTIVATION. CREW ELECTED TO RETURN TO FIELD.Jan 19, 2012 · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR CA120130003Heater · malfunctioned(CAN) THE FLIGHT ATTENDANT NOTICED THAT THE GALLEY HEATER SWITCH OVERHEAT CONDITION LIGHT WAS ILLUMINATED. THE SWITCH WAS DESELECTED AND THE SYSTEM DEFERRED IN ACCORDANCE WITH THE MEL. DURING TROUBLESHOOTING, MAINTENANCE FOUND THE HEATER ASSEMBLY INTERNAL ELEMJan 19, 2012 · Cndair CL600* · Buffet/GalleysSDR CA120113002Fan · failed(CAN) DURING THE APPROACH, THE FLIGHT CREW SMELLED SMOKE, THE F/A REPORTED SMOKE IN THE CABIN FOLLOWED BY A RECIRC FAN FAULT STATUS MESSAGE. THE RECIRCULATION, RECIRCULATING FANS WERE TURNED OFF AND THE SMOKE QUICKLY DISSIPATED. AN EMERGENCY WAS DECLARED ANDJan 9, 2012 · Bombdr CL6002D15 · Air Distribution FanSDR CA120118004Bleed Valve · failed(CAN) TOWER REPORTED SMOKE FROM LT ENGINE ON SHORT FINAL. CREW NOTED A LITTLE HIGHER THEN NORMAL FUEL FLOW. CREW CONTINUED LANDING AND ON TAXIWAY NOTED INCREASED SMOKE AND FUMES WITH STRONG ODOR OF FUEL. CREW ELECTED TO SHUT DOWN LT ENGINE AND LT FUEL SOV. MAIJan 3, 2012 · Cndair CL6002C10 · Compressor Bleed ValveSDR CA120103001Filter · collapsed(CAN) A COLLAPSED FILTER WAS FOUND DURING SCHEDULED REPLACEMENT OF THE AUXILIARY POWER UNIT OIL FILTER ELEMENT IAW TASK 000-49-360-714, 2000 HOURS INTERVAL. THE FILTER WAS REPLACED, LEAK CHECKED AND THE ACFT RELEASED FOR SERVICE. THE FILTER HAS NO TRACE OF CODec 28, 2011 · Cndair CL6002C10 · APU Oil SystemSDR MALA110297Engine · contaminatedAFTER TAKEOFF, AFT LAVATORY WARNING LIGHT CAME ON AND ENTIRE CREW COULD DETECT SMOKE. PERFORMED CHECKLIST AND RETURNED TO DEPARTURE. FOUND ODOR TO BE COMPRESSOR WASH SOLUTION. PERFORMED PACK RUN IAW AMM 21-00 AND ENGINE RUNS IAW 71-00.Dec 26, 2011 · N913XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA201101001Blade · lack of lubeNR 1 ENG N1 VIB AT POWER SETTINGS ABOVE 75 PERCENT N1 AND 280 KNOTS. PERFORMED FAN BLADE TANG LUBRICATION IAW CRJ900 AMM 72-21-02 AND CRJ900 AMM 12-20-72 VIB CHECK GOOD. PERFORMED HIGH POWER RUN REF CRJ900 AMM 71-00-00.Dec 22, 2011 · N162PQ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR REXA201101003Blade · lack of lubeLEFT N1 FAN VIBRATION AT 1.9 AT 33,000FT. REDUCED POWER AND UNABLE TO CONTROL VIBRATION. DESENDED 31,00FT. ABLE TO CONTROL FAN VIBRATION AT 1.5-1.7. NO ICE AND FLYING IN CLEAR WEATHER. VERIFIED DISCREPANCY. PERFORMED FAN BLADE TANG LUBRICATION ON LEFT ENGDec 22, 2011 · N176PQ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR CA111216004Torque Tube · chafed(CAN) DURING A ROUTINE SERVICE CHECK, CIRCUMFERENCIAL DAMAGE WAS FOUND ON THE LT FLAP DRIVE TQ TUBE AT WS 128 TO 97. IT APPEARS THAT THE TQ TUBE HAS BEEN RUBBING ON THE PLASTIC CONTAINMENT RING AT THIS LOCATION, THE CLEARANCE ON THE FWD SIDE OF THE TUBE TO THDec 16, 2011 · Cndair CL600* · Trailing Edge Flap Control SystemSDR CA111215002Shutoff Valve · failed(CAN) DURING CLIMB THE CREW RECEIVED A RT ENG BLEED CAUTION MSG. DUE TO FUEL CONSIDERATION CAUSED BY THE ALTITUDE RESTRICTION, DECISION WAS TAKEN TO TURN BACK. THE RT BLEED PRESS & REGULATING SHUT OFF VLV PRSOV PN CG670-80002-9, REFERENCE IPC 36-12-01-01-005Dec 12, 2011 · Bombdr CL6002D15 · Pneumatic Distribution SystemSDR CA111212011Lens · cracked(CAN) DURING A WALK AROUND THE REMAINS OF A BIRD STRIKE WERE NOTED ON THE RT LANDING LIGHT LENS. THE LANDING LIGHT LENS WAS CRACKED. THE ACFT WAS INSPECTED IAW THE AMM & THE LENS WAS REPLACED.Dec 11, 2011 · Bombdr CL6002D15 · Exterior LightingSDR MASA2011112264087Engine · flamed outRT ENG FLAME-OUT FOLLOWING POSS L/S RT ENG FLAME-OUT FOLLOWING POSS L/S. ENGINE OPERATED NORMALLY AFTER 3 STARTS AND POWER RUN CONTRACT MX.Nov 21, 2011 · N915FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA111123001Spring · broken(CAN) DURING SERVICE CHECK FOUND LT MLG SIDE STAY LOWER TENSION SPRING BROKEN.Nov 21, 2011 · Bombdr CL6002D15 · Main Landing GearSDR COMA2011110290034Linkage · brokenON DESCENT INTO MEM RECEIVED RT FADEC CAUTION MSG. EMERGENCY DECLARED, FOLLOWED QRH PROCEDURE, PERFORM IFSD ON RIGHT ENGINE. NO ABNORMAL ENGINE INDICATIONS PRIOR TO SHUTDOWN, A/C LANDED SAFELY IN MEM. FOUND RIGHT ENGINE O/B VG LINKAGE BROKEN. REMOVED AND RNov 1, 2011 · N548CA · Cndair CL6002D24 · Fuel Controlling SystemSDR CA111102004Seal · bent(CAN) HARD CHAFING CONDITION AND DAMAGED MOVING PART HAVE BEEN FOUND BY MX PERSONNEL WHILE PERFORMING POST FLIGHT CHECK FOLLOWING ACFT FIRST FLIGHT. RT AILERON OTBD LOWER L/E PANEL HAD SEVERELY COME INTO CONTACT WITH RT AILERON OTBD LOWER GAP SEAL. INTERFERENov 1, 2011 · Cndair CL6002A12 · AileronsSDR CA111101004Line · chafed(CAN) ABOUT AN HOUR INTO THE FLIGHT, THE CREW RECEIVED A HYD 2 LOW CAUTION MESSAGE. THE NR 2 HYD SYS QTY WAS READING ZERO. THE FLIGHT RETURNED TO THE DEPARTURE AIRPORT SAFELY. INVESTIGATION FOUND A CHAFED HYD LINE IN THE CARGO COMPARTMENT AREA. THE LINE WASOct 28, 2011 · Cndair CL600* · Hydraulic System, MainSDR REXA201100641Blade · lack of lubeLT ENGINE FAN VIBE. LUBE FAN BLADES IAW AMM PERFORM GROUND FAN VIBE, OPS CHECK GOOD.Sep 29, 2011 · N147PQ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2011090563639Pin · defectiveNR 2 ENGINE 1.9 VIBE CRUISE FL 350. R2 ALL BLAD PINS AND PERFORMED FAN BLADE LUBE.Sep 5, 2011 · N917FJ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2011082903594Engine · vibrationLT ENG TRANSIENT VIB 1.7 - 1.9 IN FLT. PERFORMED INSP & BLADE SHAKE RUNS IN LIMITS, RO APPLIED RO# CRJ9-72-0112 APPLIED TO AIRCRAFT TO PERFORM FAN BLADE LUBE WITH IN 50 FLIGHT CYCLES.Aug 28, 2011 · N938LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011082903595Pump · faultyLEFT ENG LOW OIL QTY IND 15 PERCENT. R2 NR 1 EDP AND SERVICED OIL TO FULL.Aug 28, 2011 · N956LR · Cndair CL6002D24 · Turbine Engine Oil SystemSDR MASA2011082903593Fan Blade · lack of lubeENG 2 FAN VIBE 1.8 AT FL340;C/W FAN BLADE, TANG & PIN LUBE, OPS CHECK AT MAX PWR IS 0.1.Aug 27, 2011 · N912FJ · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2011082503570Engine · vibrationNR 1 ENG N1 VIB REACHED 1.8 IN FLT. SHOOK BLADES AND COMPLIED WITH THE RO CRJ9-72-0111.Aug 24, 2011 · N916FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MALA110200Glowstrip · missingFLOOR GLOWSTRIP IN FRONT OF FWD WASTE BASKET IS MISSING. INSTALLED SMALL SECTION OF GLOW STRIP ON FLOOR FRONT OF WASTE BASKET. PN PL88-900LH00 BASE; FILM PN PL88-930LH05 & CLIP PN PL88-910LH00.Aug 13, 2011 · N917XJ · Cndair CL6002D24 · Emergency EquipmentSDR MASA2011080903436Engine · vibrationLEFT ENGINE VIBE 1.9 IN CRUISE. C/W RO 017382.Aug 8, 2011 · N928LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011080803427Blade · lack of lubeE1 VIBE AT 1.7 DURING CLIMB. C/W BLADE LUBE.Aug 7, 2011 · N908FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2011080803413Engine · vibrationNR 1 ENGINE VIBE AT 2.3 ON CLIMB. C/W RO CRJ9-72-0109, ENGINE RUN WITHIN LIMITS 0.9 MILS. STS - MEM.Aug 5, 2011 · N908FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
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