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 CA190524020Skin · corroded(CAN) MINOR CORROSION UNDER THE ANTENNA AT F.S 1031 TO F.S 1051 BETWEEN STRINGERS 26R AND 27 CENTER. (TC# 20190524020)May 23, 2019 · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR CA190527019Longeron · corroded(CAN) UPON REMOVAL OF STANDOFF (WSI), CORROSION DAMAGE LOCATED @ LH UPPER LONGERON FS485.00 FS501.00 BETWEEN STR 18L STR 19L. (TC# 20190527019)May 22, 2019 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR CA190524014Fmu · faulted(CAN) DIVERTED DUE TO #2 ENGINE NOT MAKING N1 POWER. CORRECTIVE ACTION: REPLACED THE FMU (TC# 20190524014)May 22, 2019 · Cndair CL6002D24 · Fuel Controlling SystemSDR CA190517011Wire · abnormal(CAN) ON A MODSUM THAT MODIFIES THE LH AND RH REVERSIONARY PANELS, ONE OF THE WIRES HAS A SMALLER GAUGE SIZE. THE WIRE HAS A 22 GAUGE INSTEAD OF 18 GAUGE IN A 10 AMPS CIRCUIT BREAKER. THIS ISSUE IS BEING INVESTIGATED UNDER THE CAW PROCESS (REF: RJX-CA-24-0049)May 16, 2019 · Cndair CL6002C10 · Navigation System WiringSDR CA190531002Floor Support · corroded(CAN) DURING SCHEDULED MAINTENANCE A CARGO FLOOR STRUCTURAL I-BEAM ON THE LH SIDE, AT FS1000-FS1031 WAS FOUND TO HAVE LEVEL TWO CORROSION, WITH A HOLE CORRODED COMPLETELY THROUGH THE BEAM AT ONE LOCATION. THE BEAM SECTION TO BE REPLACED IAW APPROVED REPAIR DATMay 15, 2019 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR CA190521002Shutoff Valve · failed(CAN) RTO FOR R ENG BLEED CAUTION MESSAGE ON INITIAL POWER UP FOR TAKE-OFF. CORRECTIVE ACTION: REMOVED AND REPLACED THE RH ENGINE HPSOV. (TC# 20190521002)May 15, 2019 · Cndair CL6002D24 · Engine Bleed Air SystemSDR CA190514015Door Sill · corroded(CAN) DURING SCHEDULED MAINTENANCE LEVEL TWO CORROSION WAS OBSERVED BELOW THE PASSENGER DOOR SILL AT STRINGER 21P BETWEEN STATION X310 - X319. MAINTENANCE CARRIED OUT REPAIR/REPLACEMENT OF THE AFFECTED PARTS, BACK-UP SILL FRAME, & INTERCOSTAL.May 14, 2019 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR CA190521015Antenna · faulted(CAN) DIVERTED FOR A WEATHER RADAR FAULT. WITH THE WEATHER RADAR INOPERABLE THE FLIGHT COULDN`T CONTINUE DUE TO THUNDERSTORMS IN THE DESTINATION AREA. CORRECTIVE ACTION: REMOVED AND REPLACED WEATHER RADAR ANTENNA (TC# 20190521015)May 9, 2019 · Cndair CL6002D24 · Weather Radar SystemSDR MASA2019050711844Oil System · low pressureENGINE 2 SHUTDOWN IN FLIGHT- LOW OIL PRESSURE. STILL IN WORK.May 7, 2019 · N946LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA190527002Floorbeam · corroded(CAN) INSPECTION FOUND CORROSION DAMAGE ON CROSS BEAM LOCATED AT FS1000.00 AND RBL41.00. (TC# 20190527002)May 3, 2019 · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR CA190522008Skin · corroded(CAN) CORROSION IN FWD CARGO (FWD BACKING SKIN, FRAME AT FS485.00 AND FS661.00+90) (TC# 20190522008)Apr 29, 2019 · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR CA190430004Frame · corroded(CAN) CUSTOMER REPORTS 3 AREAS OF BLENDED CORROSION DAMAGE TO LOWER FRAME SECTORS AT FS 942.00 AND FS 969.00 (TC# 20190430004)Apr 28, 2019 · Cndair CL6002D24 · Fuselage Main, FrameSDR CA190430008Shear Panel · corroded(CAN) CORROSION IN AFT CARGO COMP. FLOOR STRUCTURE. IAW SRM 53-61-43-101-001-A02, NO DAMAGE ALLOWED AT REPORTED LOCATIONS. SHEAR PANEL (TC# 20190430008)Apr 27, 2019 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR CA190429014Reservoir · leaking(CAN) DIVERSION DUE TO SMOKE SMELL COMING FROM COCKPIT GASPERS. TURNED OFF RECIRCULATION FANS AND SMELL WENT AWAY. CORRECTIVE ACTION: FOUND #1 HYD RESERVOIR LEAKING ON ACM, RESERVOIR REPLACED. (TC# 20190429014)Apr 25, 2019 · Cndair CL6002D24 · Hydraulic Reservoir, MainSDR CA190424002Frame Angle · corroded(CAN) DURING MAINTENANCE INSPECTION LEVEL 2 CORROSION WAS OBSERVED ON THE AFT FACE OF FRAME FS295, BETWEEN STRINGERS 26L AND 25R. FRAME SECTION REPLACED IAW THE MANUFACTURER`S SRM. (PN SH670-31353-1) (TC# 20190424002)Apr 24, 2019 · Cndair CL6002D24 · Fuselage Main, FrameSDR CA190423015Intercostal · corroded(CAN) DURING SCHEDULED INSPECTION, LEVEL 2 CORROSION FOUND ON L//H INTERCOSTAL BETWEEN FS 349 AND 364, STRINGER 27. PART REPLACEMENT CARRIED OUT IAW MANUFACTURER SRM. PN (TC# 20190423015)Apr 23, 2019 · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR CA190423017Stringer · corroded(CAN) DURING SCHEDULED MAINTENANCE, LEVEL 2 CORROSION WAS OBSERVED ON STRINGERS 25R & 26R AT FS 280-349. PARTS REPLACED IAW THE MANUFACTURER SRM. PN SH670-31212-2 (TC# 20190423017)Apr 23, 2019 · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR CA190425019Engine · fire(CAN) THERE WAS EVIDENCE OF A FIRE IN THE #1 ENGINE. INITIAL INSPECTIONS INDICATE THE POSSIBLE ORIGIN BEING BETWEEN THE ENGINE DRIVEN FUEL PUMP AND THE FUEL LINE FITTING. THE DAMAGES ARE AS FOLLOWS: THERE WAS DISCOLORATION ON THE W2 BLUE ENGINE HARNESS - CONTIApr 17, 2019 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA190412003Diffuser · separated(CAN) DURING UNRELATED MAINTENANCE IN THE AFT EQUIPMENT COMPARTMENT AN AME OBSERVED THAT THE LEFT AND RIGHT HEAT EXCHANGER DIFFUSERS WERE SEPARATED FROM THEIR RESPECTIVE HEAT EXCHANGERS. THE DIFFUSER MATING SURFACES HAD PULLED THROUGH THE ATTACHING HARDWARE. (Apr 12, 2019 · Cndair CL6002D24 · Cabin Cooling SystemSDR CA190409006Fan · seized(CAN) MTC REPORTED ELECTRICAL SMELL AND SMOKE IN A CABIN DURING AN A1 CHECK. UPON TROUBLESHOOTING, THEY DISCOVERED THE ELECTRICAL ODOR AND SMOKE WAS COMING FROM THE AFT LAV`S EXHAUST FAN, THE EXHAUST FAN IS FOUND SEIZED. MTC REPLACED THE AFT LAV FAN ASSEMBLY AApr 9, 2019 · Cndair CL6002D24 · Air Distribution FanSDR MASA2019040511799Warning Light · illuminatedENG 1 VIBE ICON IN FLT AT CRUISE SETTING- RTF.Apr 5, 2019 · N920FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA190403009Sensor · defective(CAN) JUST AFTER LEVELING OFF, THE CREW RECEIVED A BRAKE OVERHEAT WARNING MESSAGE. THE MESSAGE FLICKERED A FEW TIMES AND THEN REMAINED ON. THE CREW ELECTED TO RETURN TO THE DEPARTURE AIRPORT AND AN EMERGENCY WAS DECLARED. ON LANDING ARFF CONFIRMED BRAKE TEMPS Apr 2, 2019 · Cndair CL6002D24 · Landing Gear Brake SystemSDR CA190320014Line · cracked(CAN) PILOT REPORT THAT THE RH ENG BLEED CAUTION LIGHT CYCLES ON AND OFF. NO BLEED PRESSURE INDICATION ON THE RH SIDE AND RH PACK WILL NOT COME ONLINE. AIRCRAFT RETURNED TO GATE. MAINTENANCE ASSESSMENT FOUND THE #2 PACK INLET PRESSURE SENSOR (PIPS) SUPPLY LINEMar 17, 2019 · Cndair CL6002D24 · Cabin Cooling SystemSDR CA190313002Channel · corroded(CAN) DURING SCHEDULED MAINTENANCE LEVEL TWO CORROSION WAS OBSERVED WITHIN THE PASSENGER DOOR STRUCTURE BELOW THE DOOR HANDLE CUT-OUT. REPAIRS CARRIED OUT IAW THE SRM INCLUDING REPLACEMENT OF CHANNEL (TC# 20190313002)Mar 13, 2019 · Cndair CL6002D24 · Passenger/Crew DoorsSDR CA190311028Hinge Fitting · corroded(CAN) DURING SCHEDULED MAINTENANCE DEEP LEVEL TWO PITTING CORROSION WAS IDENTIFIED ON THE RUDDER CENTER HINGE ASSEMBLY. THE DAMAGE HAS BEEN MAPPED AND THE MANUFACTURER HAS PROVIDED AN REPAIR ENGINEERING ORDER TO ADDRESS THE DAMAGE.Mar 11, 2019 · Cndair CL6002D24 · Rudder StructureSDR CA190319016Probe · faulted(CAN) ON DESCENT, LEFT AND TOTAL FUEL QTY INDICATORS ON PRIMARY DISPLAY PAGE SHOWING AMBER DASHES. FLIGHT CONTINUED AND LANDED SAFELY. EMERGENCY WAS DECLARED AS A PRECAUTION. CORRECTIVE ACTION: REMOVED AND REPLACED LH FUEL QUANTITY PROBE #4.Mar 9, 2019 · Cndair CL6002D24 · Fuel Quantity SensorSDR CA190318019Dcu · failed(CAN) CONFIG AILERON WARNING WHEN BRINGING POWER UP FOR TAKEOFF.Mar 5, 2019 · Cndair CL6002D24 · Aileron Control SystemSDR CA190314009Sump · failed(CAN) A/C WAS ACCELERATING FOR TAKEOFF WHEN THE CREW REJECTED TAKEOFF DUE TO SMOKE ON BOARD. THE AIRCRAFT STOPPED ON THE RUNWAY AND WAS EVACUATED. THE A SUMP WAS LEAKING OIL FROM LEFT ENGINE. LEFT ENGINE REPLACEMENT IN PROGRESS.Mar 3, 2019 · Cndair CL6002D24 · Turbine Engine Oil SystemSDR SWIA2019030545589Engine · smokeDURING TAKEOFF ROLL, VISIBLE SMOKE IN THE COCKPIT AND CABIN, LAV SMOKE WARNING MSG DISPLAYED ON EICAS. ABORTED TAKEOFF. EMERGENCY DECLARED. (FLT#7335) FO: 03/04/2019 CLOSED REMOVED AND REPLACED LT ENGINE.Mar 1, 2019 · N549CA · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA190220018Engine · damaged(CAN) EN ROUTE, FLIGHT CREW REPORTED AN ACRID OIL SMELL ON TAKE OFF AFFECTING THE CABIN AIR QUALITY, NO SMOKE OR HAZE WAS OBSERVED. ALL CREW MEMBERS DONNED THEIR OXYGEN MASKS. AN EMERGENCY WAS DECLARED, THE AIRCRAFT RETURNED AND LANDED OVERWEIGHT WITHOUT FURTHFeb 18, 2019 · Cndair CL6002D24 · Turbine Engine Oil SystemSDR MASA2019011011655Engine · vibrationLEFT ENGINE VIBE REACHED 2.5 ON CLIMBOUT. CURRENTLY OUT OF SERVICE.Jan 10, 2019 · N925FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA2018103101005Compressor · dirtyHAD SMOKE IN THE COCKPIT ON TAKE-OFF ROLL, AT 110KTS, ABORTED TAKE-OFF ALSO SMOKE IN AFT OF CABIN REPORTED BY FLT ATTENDANTS NO BRAKE OVERHEAT, AT 1 AND 2 WHEN STOPPED. THRUST REVERSERS DEPLOYED AT APPROX 50% N1 COMPLETED TS 00737, NO BRAKE OVERTEMP/ OR FUSE POct 28, 2018 · N925XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA181015008Skin · corroded(CAN) DURING INSPECTION, CORROSION FOUND ON BUTT STRAP JOINT AT FS 977.00 BETWEEN STR 22 RH & STR 27. (TC# 20181015008)Oct 12, 2018 · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR CA180723017Windshield · cracked(CAN) IN CRUISE, FLIGHT CREW REPORTED RIGHT WINDSHIELD HAS CRACKED. WINDSHIELD ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (TC# 20180723017)Jul 14, 2018 · Cndair CL6002D24 · Flight Compartment WindowsSDR CA180530012Adc · malfunctioned(CAN) RUDDER LIMIT FAULT STATUS FOLLOWED BY STALL FAIL CAUTION, AS WELL AS, EFIS COMP MON/IAS LEAD 2 MACH TRIM CAUTION MSG. FOUND P3 DRAIN TUBE 2/3 FULL WITH WATER. WATER DRAINED AND LEAK TEST CARRIED OUT, IAW MM 34-11-00-790-803. CHECKED SERV. CREW REPORTMay 17, 2018 · Cndair CL6002D24 · Air Data ComputerSDR CA180511007Computer · faulty(CAN) DURING CLIMB, THE AIRCRAFT STARTED AN UN-COMMANDED ROLL TO THE RIGHT REACHING AN ESTIMATED 35 BANK ANGLE. FLIGHT CREW DISENGAGED THE AUTOPILOT AN AIRCRAFT ATTITUDE RE-ESTABLISHED. THE AUTOPILOT WAS DEFERRED UNDER MEL AND THE AIRCRAFT REMAINED IN SERVICMay 8, 2018 · Cndair CL6002D24 · Autopilot ComputerSDR REXA2018042600322O-Ring · cutWHILE TAKING THE RUNWAY FOR DEPARTURE, THE LT OIL LEVEL LOW STATUS MESSAGE POSTED. AT THE TIME L ENG OIL WAS AT 47%. OVER 15 MINUTES THE OIL QUANTITY ON THE LEFT ENGINE DROPPED TO 15%. THE LEFT OIL PRESSURE THEN DROPPED TO 5PSI OVER 5 MINUTES. RAN THE QRH Apr 26, 2018 · N336PQ · Cndair CL6002D24 · Turbine Engine Oil SystemSDR SWIA2018042044570Fadec · failedAPPROXIMTELY 10 KTS PRIOR TO V1, CREW HEARD A LOUD POP, FELT A SLIGHT YAW AND RECEIVED A LEFT ENGINE FLAME OUT CAUTION MESSAGE. ABORTED THE TAKE-OFF AND TAXIED BACK TO GATE. REMOVED AND REPLACED LT FADEC IAW AMM. OPS CHECKED GOOD.Apr 19, 2018 · N816SK · Cndair CL6002D24 · Fuel Controlling SystemSDR REXA2018041300284Engine · contaminatedODOR OF SMOKE IN CABIN AFTER TAKEOFF, THE ODOR WAS LIKE BURNED RUBBER IN FOR AND AFT OF CABIN. PERFORMED INSPECTION IAW FIM 21-22-00, AND DETERMINED ABNORMAL ODOR IN CABIN TO BE FROM RT ENGINE COMPRESSOR WASH PERFORMED THE PREVIOUS NIGHT. RISE ENGINE IAW AMMApr 13, 2018 · N330PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR SWIA2018021944307Inlet · damagedLEFT ENGINE INLET HAD A PERFORATED ACOUSTIC LINER AT THE 5 O'CLOCK POSITION. REPAIRED THE DAMAGE IAW SRM AND REO.Feb 10, 2018 · N822SK · Cndair CL6002D24 · Turbine Engine Air Inlet SectionSDR CA180103003Tru · failed(CAN) WHILE WORKING ON A DEFECT IN THE COCKPIT, MTC RECEIVES A TRU FAN FAIL MESSAGE ON THE ICAS. SHORTLY AFTER, SMOKE IS SEEN COMING OUT THROUGH THE NOSE PANEL OF THE AC. IT WAS NOTED THAT NO C/B ARE POPPED. THE AC HAD TO BE POWERED DOWN TO STOP THE SMOKE AJan 3, 2018 · Bombdr CL6002D15 · DC Rectifier/ConverterSDR VNAA2017111211101Engine · odorFLIGHT CREW REPORTED AC ESSENTIAL BUSS CAUTION MESSAGE AND GENERATOR 1 FAULT IN FLIGHT. CREW RAN QRH AND ATTEMPTED TO START APU WHICH TOOK THREE ATTEMPTS. FLT DIVERTED, AND DECLARED EMERGENCY. LANDED SAFELY. LT & RT ENGINES HAD COMPRESSOR WASHES DURING OVENov 12, 2017 · N581NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2017102512722Engine · power lossRIGHT ENGINE HAD A MOMENTARY FAILURE IN FLIGHT.Oct 25, 2017 · N927LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA2017080611101Dcu · contaminatedAFTER TAKEOFF, CREW REPORTED A RIGHT HAND ENGINE OIL PRESSURE MESSAGE ALONG WITH COWL ANTI-ICE, RIGHT HAND FADEC, LEFT HAND FADEC, LEFT HAND FUEL PRESSURE AND RIGHT HAND OIL PRESSURE MESSAGES. THE CREW SHUT DOWN THE ENGINE IN FLIGHT AND COMPLIED WITH AN IN FLIAug 6, 2017 · N598NN · Cndair CL6002D24 · Turbine Engine Oil SystemSDR MASA2017071612465Engine · overtempRIGHT ENGINE HIGH ITT ON TAKE OFF ROLL, 963 DEGREES FOR 14 SECONDS. COMPLIED WITH HIGH ENERGY STOP INSPECTION.Jul 16, 2017 · N904FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR WVER2017062100007Frame · crackedRIGHT FUSELAGE BS 220 FRAME HAS A CRACK INDICATION .1 INCH LONG ON THE FWD FACE, STRINGER 13AR. FAILED NDT INSPECTION.Jun 21, 2017 · N942LR · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2017032300397Engine · damagedDURING TAKEOFF ROLL, AIRCRAFT PULLED TO THE RIGHT TWICE PRIOR TO ROTATION, NR 2 ENGINE WENT OUT OF FLEX THRUST, ACCOMPLANIED BY NOISE, AND VIBRATION. REMOVED AND REPLACED THE RT ENGINE. OPS CHECKED GOOD.Mar 23, 2017 · N907XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR SWIA201743129Engine · power lossAFTER DEPARTURE, THE LT ENGINE LOST POWER MOMENTARILY. RETURNED TO FIELD WITH LT ENGINE SET AT IDLE. FLIGHT LANDED SAFELY. REMOVED AND REPLACED LT ENGINE ASSY IAW AMM. OPS CHECKED GOOD.Mar 21, 2017 · N162PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR WVER2017012300005Beam · damagedRIGHT ENGINE THRUST REVERSER UPPER OTBD NYLON INSERT IS DAMAGED AND LATCH BEAM HAS ELONGATED HOLES.Jan 23, 2017 · N915FJ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2017012100072Engine · contaminatedDURING DEPARTURE, A STRONG ODOR OF SMOKE IN THE COCKPIT AFTER AIRBORNE, 10 SEC SMOKE AFT LAVATORY WARNING MESSAGE ON EICAS. RAN QRH LANDED. INSPECTED AFT LAV FOR SMOKE ODOR IAW FIM TASK 21-21-00-810-806. NO DEFECT NOTED. THE COMPRESSOR WASH CHEMICAL FLUIDJan 21, 2017 · N304PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
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