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 MASA2013032125455Engine · damagedIN CRUISE CREW FELT STRONG AIRFRAME VIBRATION FOLLOWED BY EICAS INDICATION OF FLAME OUT AND ENGINE DEGRADED MESSAGES. THE SYSTEM THEN PERFORMED AN AUTOMATIC RELIGHT. THIS SEQUENCE OF EVENTS OCCURED TWICE. AFTER SECOND RELIGHT THE CREW RETARDED THROTTLE LEVEMar 21, 2013 · N956LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA130321002Wire · chafed(CAN) DURING MAINTENANCE INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE OTBD TELESCOPIC DUCT OF THE RT WING L/E. THE SAME WAS FOUND AT THE LT WING OTBD LOCATION. BOTH SPIRAL CORDS TO BE REPLACED IAW CMM 30-11-07.Mar 21, 2013 · Cndair CL600* · Wing System WiringSDR CA130320001Baffle · fractured(CAN) DURING A SCHEDULED BOROSCOPE INSPECTION OF THE LT ENGINE COMBUSTION LINER AND STAGE 1 NOZZLE ASSY, A SECTION OF BAFFLE WAS FOUND MISSING. FURTHER INSPECTION REVEALED SIGNIFICANT DAMAGE TO SOME OF THE HP TURBINE FIRST STAGE BLADES. ENGINE CHANGE CURRENTLYMar 19, 2013 · Cndair CL600* · Turbine Engine Combustion SectionSDR CA130308003Pin · broken(CAN) AFTER GAINING ACCESS INSIDE THE COCKPIT, THE F/A COULDN`T REOPENED THE DOOR. AFTER MANY UNSUCCESSFUL ATTEMPTS TO UNLOCK/OPEN THE DOOR, F/A STAYED INSIDE THE COCKPIT FOR THE REMINDER OF THE FLIGHT. CABIN DUTIES WERE PERFORMED BY THE OTHER F/A. UPON ARRIMar 8, 2013 · Cndair CL600* · Fixed Inner DoorsSDR CA130307006Pitch Control · malfunctioned(CAN) UNCOMMANDED PITCH UP. AUTOPILOT HAS BEEN DISCONNECTED AUTOMATICALLY WITH NO POSSIBILITY TO RE-ENGAGE.Mar 7, 2013 · Cndair CL6002D24 · Elevator Control SystemSDR CA140728013Line · cracked(CAN) AFTER OPENING AN RFC 3000069664, AS A RESULT OF A CUSTOMER QUALITY INVESTIGATION REQUEST, QIR SROS-NDAR-13-00052 DATED MARCH 6TH 2013, REGARDING THE OXYGEN BOTTLE FILL LINE LEAKING, CONDUCTED A FRACAS REPORT AND IDENTIFIED 78 CASES IN SERVICE WHICH MAY RMar 6, 2013 · Cndair CL6002C10 · Crew Oxygen SystemSDR CA130225012Wire · chafed(CAN) DURING MAINTENANCE INSPECTION, CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE INBD TELESCOPIC DUCT OF THE LT WING L/E. THE SAME WAS FOUND AT THE INBD AND OTBD RT WING L/E LOCATIONS. THE CHAFED SPIRAL CORDS WILL BE REPLACED IAW CMM 3Feb 25, 2013 · Cndair CL600* · Wing System WiringSDR CA130219002Pump · leaking(CAN) DURING DESCENT THROUGH 10,000 FT, THE NR 2 EDP HYDRAULIC PUMP CAUTION BEGAN CYCLING. NR 2 HYDRAULIC SYS PRESSURE WAS RESTORED WITH THE 2B ACMP HOWEVER THE FLUID QTY DROPPED TO 5 PERCENT AT WHICH POINT NR 2 HYDRAULIC SERVICES WERE LOST. THE NR 2 EDP WAS Feb 17, 2013 · Bombdr CL6002D15 · Hydraulic Pump (Electric/Engine), MainSDR SWIA201332811Torque Shaft · crackedUPON STOWING THRUST REVERSER RT ENGINE FLAMEOUT MESSAGE ILLUMINATED AND ITT SPIKED. AFTER CLEARING AND ITT RETURNED TO NORMAL. RT ENGINE REMAINED FLAMED-OUT. (FLT 4605) REPLACED THE RT ENGINE I/B AND O/B VG TORQUE SHAFTS IAW AMM.Feb 14, 2013 · N807SK · Cndair CL6002D24 · Compressor Bleed ControlSDR CA130214005Feeder Cable · chafed(CAN) DURING MAINTENANCE INSPECTION CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE INBD TELESCOPIC DUCT OF THE RT WING L/E. THE SAME WAS FOUND AT THE LT WING OTBD LOCATION. BOTH SPIRAL CORD HARNESSES WERE REPLACE IAW CMM 30-11-07.Feb 14, 2013 · Bombdr CL6002D15 · Wing System WiringSDR CA130220004Link · failed(CAN) UPON STOWING THRUST REVERSER RT ENGINE FLAME OUT MESSAGE ILLUMINATED AND ITT SPIKED, AFTER CLEARING ACTIVE RUNWAY MESSAGE CLEARED AND ITT RETURNED TO NORMAL. RIGHT ENGINE REMAINED FLAMED-OUT. MAINTENANCE R & R THE RT ENGINE INBD AND OTBD VG TORQUE SHAFTFeb 14, 2013 · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR CA130214016Oil System · overheated(CAN) HIGH RIGHT OIL TEMP FOLLOWED QRH PERFORMED IN-FLIGHT ENGINE SHUTDOWN.Feb 10, 2013 · Cndair CL6002D24 · Engine Oil System (Airframe Furnished)SDR CA130201003Cable · broken(CAN) WHILE CARRYING OUT MAINTENANCE TASK RJ9-52-830-101, DETAILED INSPECTION OF THE PASSENGER DOOR LATCH MECHANISM THE PRESSURE VENT FLAP ICE BREAKER CABLE WAS FOUND TO BE DAMAGED. APPROXIMATELY 90 PERCENT OF CABLE STRANDS FRAYED/BROKEN. CABLE TO BE REPLACEDFeb 1, 2013 · Cndair CL600* · Passenger/Crew DoorsSDR CA130204009Compressor · damaged(CAN) THE FOLLOWING LANDING EVENT OCCURRED: RECEIVED LT ENGINE BLEED CAUTION MSG FOLLOWED BY LEFT ENGINE DEGRADED CAUTION MSG DURING FINAL, UPON LDG LT ENG FLAMED OUT, FLAMEOUT, CAUTION MSG WAS RECEIVED. THE CAPTAIN REPORTED THAT DURING APPROACH FLIGHT, THEY Jan 30, 2013 · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR MASA2013012752392Engine · dirtyFOUL ODOR DURING TAKEOFF AT FULL THRUST. PERFORMED ENGINE WATER WASH. RAN ENGINE FOR PERFORMANCE, ODOR AND OIL CONSUMPTION. NO FAULTS NOTED, ALL PARAMETERS WITHIN LIMITS.Jan 27, 2013 · N918FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA130124018Window · cracked(CAN) 4000 FT, RT SIDE WINDOW CRACK APPEARS FOLLOWED BY R WINDOW HEAT, C, ON ED1. RT SIDE WINDOW WINDOW: NP139322-12, RT SIDE WINDOW CONTROLLER 1659-1-1.Jan 22, 2013 · Cndair CL6002D24 · Flight Compartment WindowsSDR CA130122002Turbine · damaged(CAN) DURING THE CLIMB THROUGH 8600 FT THE CREW HEARD A POPPING SOUND AND FELT CONSIDERABLE ENGINE VIBRATION. THE EICAS SHOWED FLAMEOUT FOR THE RT ENGINE AND THE CREW COMPLETED THE SHUTDOWN CHECKLIST AND RETURNED TO THE DEPARTURE AIRPORT. INITIAL INVESTIGATIOJan 18, 2013 · Cndair CL600* · Turbine SectionSDR CA130118010Blades · damaged(CAN) RT ENGINE APR ON N1 GAUGE MESSAGE ON TAKEOFF ROLL, REJECTED TAKEOFF AT BETWEEN 80-100 KNOTS, WAS A NOTICABLE SHUTTER IN THE AIRFRAME WHEN MESSAGE OCCURRED, NO OTHER ABNORMALITIES WITH PARAMETERS NOTED BY CREW, DAMAGE FOUND ON COMPRESSOR BLADES, ENGINE RJan 14, 2013 · Cndair CL600* · Turbine Engine Compressor SectionSDR CA130118005Cabin Pressure · failed(CAN) AFTER THE TAKEOFF, CABINE PRESSURE CLIMBING TO 2,700 CABIN RATE FT/MIN AND FLIGHT LEVELED AT 100FL, CABIN ALT WARNING APPEARS ASSOCIATED WITH PRIOR EICAS MESSAGE ODOR OF SMOKE IN THE COCKPIT.Jan 2, 2013 · Cndair CL6002D24 · Cabin Pressure Control SystemSDR CA121211016Windshield · cracked(CAN) LEFT CRACKED WINDSHIELD.Dec 8, 2012 · Cndair CL6002D24 · Flight Compartment WindowsSDR CA121130001Fan · failed(CAN) DURING TROUBLESHOOTING OF A DEFERRED DEFECT RECIRCULATING FAN FAULT MESSAGE. DEBRIS WAS DISCOVERED BLOCKING A SCREEN IN A UNDERFLOOR SUPPLY DUCT AT FS 677-682, ABOUT MID CABIN AND RESTRICTING AIRFLOW. THE FOD WAS REMOVED AND THE SYS WAS FUNCTION CHECKENov 30, 2012 · Bombdr CL6002D15 · Air Distribution FanSDR CA121130002Turbine Blades · damaged(CAN) CLIMBING THROUGH 8000 FT, FLIGHT CREW HEARD A LOUD NOISE FOLLOWED BY A YAW TO THE RT. RT ENGINE PARAMETERS INDICATED THE ENGINE WAS SPOOLING DOWN. FLIGHT CREW SECURED THE ENGINE, DECLARED AN EMERGENCY, TURNED BACK AND LANDED WITHOUT FURTHER INCIDENT. Nov 29, 2012 · Bombdr CL6002D15 · Turbine SectionSDR CA121109008Line · leaking(CAN) WHILE APPLYING TO POWER AT THE START OF THE TO ROLL THE 1 EDP CAUTION MESSAGE CAME ON AND THE NR 1 HYDRAULIC QTY WENT TO ZERO. MAINTENANCE INVESTIGATION FOUND A CHAFED HYDRAULIC LINE IN THE AFT EQUIPMENT BAY THAT WAS LEAKING. THE LINE HAD CHAFED AGAINST Nov 7, 2012 · Bombdr CL6002D15 · Hydraulic System, MainSDR CA121102004Feeder Cable · chafed(CAN) DURING MAINTENANCE INSPECTION CHAFING WAS DISCOVERED ON THE SPIRAL ELECTRICAL CORD LOCATED IN THE O/B TELESCOPIC DUCT OF THE L/H WING LEADING EDGE. THE SAME WAS FOUND AT THE LH IB LOCATION AND THE RT IB LOCATION. ALL HARNESSES WERE REPLACED IAW CMM 30-1Nov 2, 2012 · Cndair CL600* · Ice/Rain Protection System WiringSDR CA121024002Skin · dented(CAN) ON APPROACH, THE ACFT SUSTAINED SEVERAL BIRD STRIKES. AFTER LANDING THE ACFT WAS INSPECTED AND A LARGE DENT WAS FOUND JUST BELOW THE F/O SIDE WINDOW. THE DAMAGE AREA WAS MAPPED AND ALLEVIATION WAS RECEIVED FROM THE OEM. THE ACFT WAS RETURNED TO SERVIOct 23, 2012 · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR SWIA201231984Engine · flamed outRIGHT ENGINE FLAMED OUT IN FLIGHT. (FLT 4469) REPLACED RIGHT ENGINE ASSEMBLY IN REFERENCE TO AMM. PN OFF: CF34-8C5 SN OFF 194594.Oct 18, 2012 · N679CA · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR ASOA2012101802376Connector · damagedEXPERIENCED FUMES IN THE COCKPIT. DECLARED AN EMERGENCY, RAN QRH, RETURNED TO DEPARTURE. FOUND ELECTRICAL DAMAGE TO PL116P1 AND PL116J1, SEE WO 267716, FOR DETAILS OF REPAIR, PERFORMED OPS CK OF DC PWR IAW AMM 24-61-00-710-806, NO FAULTS FOUND AT THIS TIME.Oct 15, 2012 · N691CA · Cndair CL6002D24 · Electrical Power System WiringSDR CA121017008Bearing · failed(CAN) AILERONS DIFFICULT TO MOVE IN FLIGHT. FOUND BEARING FAILED.Oct 5, 2012 · Cndair CL6002D24 · Aileron Control SystemSDR CA121003013Window · cracked(CAN) IN THE CLIMB, AFTER DEPARTURE, THE F/O SIDE WINDOW CRACKED. THE CREW ELECTED TO RETURN TO THE DEPARTURE AIRPORT. CONTRACTED MAINTENANCE, DETERMINED THAT THE CENTER PLY WAS CRACKED. THE ACFT WAS FERRIED TO A MAINTENANCE BASE IAW SL 56-002. THE F/O SIDEOct 2, 2012 · Bombdr CL6002D15 · Flight Compartment WindowsSDR CA121012013Generator · failed(CAN) ACFT TOOKOFF WITH APU OFF. APPROXIMATELY 40NM OUT, THE NR 2 GENERATOR WENT OF LINE AND SHOWED NR 2 GEN CAUTION LIGHT. DURING THE HANDLING OF THE QRH PROCEDURE, NR 1 GENERATOR WENT OFF LINE. DUE TO TOTAL AC-POWER LOSS THE ADG DEPLOYED AUTOMATICALLY. NOct 2, 2012 · Cndair CL6002D24 · AC Generator-AlternatorSDR CA121002003Brake · failed(CAN) AFTER TAKEOFF AND DURING THE LANDING GEAR RETRACTION THE AURAL WARNING BRAKE OVERHEAT RINGS IN THE COCKPIT WITH THE EICAS MESSAGE BRAKE OVERHEAT. THE INDICATION OF THE BTMS NR 2 WAS OF LEVEL 20, MAXIMUM LEVEL. ONCE ON GROUND, THE PILOT INSPECTED THE AFFSep 29, 2012 · Cndair CL6002D24 · Brake Anti-Skid SectionSDR CA120918017Line · split(CAN) AFTER ENGINE START THE NR 2 HYD QTY WENT TO 0 AND RAMP REPORTED SEEING MIST FROM THE NR 2 ENGINE. PN CN627-2005-001, FOUND SPLIT. REPLACED. ALSO FOUND QUICK DISCONNECT UNION SPLIT, PN AE99118H.Sep 16, 2012 · Bombdr CL6002D15 · Hydraulic System, MainSDR CA120918019Coupling · split(CAN) AFTER ENGINE START THE NR 2 HYD QTY WENT TO 0 AND RAMP REPORTED SEEING MIST FROM THE NR 2 ENGINE. FOUND QUICK DISCONNECT UNION SPLIT, PN AE99118H, REPLACED. ALSO FOUND EDP HYD SUCTION LINE SPLIT SDR 20120918017.Sep 16, 2012 · Bombdr CL6002D15 · Hydraulic System, MainSDR ASOA2012091402222Connector · disconnectedLT SIDE EXIT LIGHT OUTSIDE INOPERATIVE. RECONNECTED LIGHT BEHIND PASSENGER SIDE WALL, OPS CHECKED GOOD IAW AMM 33-51-00-710-801.Sep 13, 2012 · N606LR · Cndair CL6002D24 · Light System WiringSDR ASOA2012091402221Light · inoperativeRT OVERWING EMERGENCY EXIT LIGHT NOT WORKING. R & R EMERGENCY LIGHT ASSY IAW ESPM 20-16-05. OPS CHECKED GOOD, NO DEFECTS. OK FOR SERVICE.Sep 12, 2012 · N132EV · Cndair CL6002D24 · Emergency LightingSDR CA120906006Duct · cracked(CAN) DURING ENGINE OIL SERVICING A BLEED LEAK WAS DISCOVERED. INSPECTION REVEALED A CRACKED BLEED-AIR CROSSOVER DUCT. RESOLVED ON W/O: 351549, TASKCARD: NR-00001, NEW DUCT INSTALLED AND LEAK TESTED IAW AMM TASK NO 36-19-09-400-801, PN GG670-80301-1, SN OFF:Sep 1, 2012 · Bombdr CL6002D15 · Pneumatic Distribution SystemSDR ASOA2012082802122Wire · brokenRIGHT WING AFT EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE IAW ESPM 20-33-00.Aug 24, 2012 · N133EV · Cndair CL6002D24 · Emergency LightingSDR ASOA2012082702110Charger · inoperativeRT WING AFT EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER ASSY IAW AMM 33-51-17. OPS CHECKED GOOD. NO DEFECTS NOTED.Aug 23, 2012 · N133EV · Cndair CL6002D24 · Emergency LightingSDR ASOA2012082702108Circuit Breaker · trippedCIRCUIT BREAKER P2 U3 "EMERGENCY LIGHTS" TRIPPED IN FLIGHT WITH ASSOCIATED "EMERGENCY LIGHTS ON" STATUS MESSAGE, ALL CABIN EMERGENCY LIGHTS WENT DARK AFTER 30 MINUTES LATER. RESET CIRCUIT BREAKER P2 U3 IAW FIM. NO FURTHER ACTION IS REQUIRED.Aug 22, 2012 · N132EV · Cndair CL6002D24 · Light System WiringSDR ASOA2012082702106Circuit Breaker · trippedBREAKER BB2 U3 "EMERGENCY LIGHTS" TRIPPED IN FLIGHT WITH ASSOCIATED "EMERGENCY LIGHTS ON" STATUS MESSAGE RESET CIRCUIT BREAKER. PERFORMED OPERATION TEST OF THE EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00. OPS CHECKED GOOD.Aug 21, 2012 · N132EV · Cndair CL6002D24 · Light System WiringSDR CA120917024Overheat Loop · failed(CAN) DURING A SCHEDULED FLIGHT AND ON CLIMBOUT, PASSING THROUGH 30,000 FT, THE FLIGHT CREW REPORTED A LT BLEED DUCT WARNING MESSAGE AND THEN FOLLOWED BY THE LOSS OF CABIN PRESSURE CONTROL. THE FLIGHT CREW DIVERTED AND LANDED UNEVENTFULLY WITHOUT DECLARING AAug 19, 2012 · Cndair CL6002D24 · Overheat DetectionSDR CA120917023Duct · failed(CAN) DURING A SCHEDULED FLIGHT AT CRUISE ALTITUDE, THE FLIGHT CREW REPORTED A LT BLEED DUCT WARNING MESSAGE ANNUNCIATED AND THEN FOLLOWED BY A LOSS OF CABIN PRESSURE CONTROL. THE FLIGHT CREW DID NOT DECLARE AN EMERGENCY AND LANDED UNEVENTFULLY.Aug 16, 2012 · Cndair CL6002D24 · Pneumatic Distribution SystemSDR ASOA2012081702075Light · inoperativeSTATUS MESSAGE: EMERGENCY LIGHTS ON, BREAKER U3 TRIPPED. R & R K198 RELAY IAW ESPM 20-39-00 AND R & R PS37, PS38 AND PS43 BATTERY CHARGERS AND PS37 BATTERY IAW AMM 33-51-17-000/400-801. PERFORMED OPERATIONAL TEST OF THE EPSU IAW AMM 33-51-17-710-801 NO DEFECAug 13, 2012 · N132EV · Cndair CL6002D24 · Emergency LightingSDR CA120809003Bpsu · failed(CAN) ON APPROACH, THE FLAPS STOPPED MOVING AT 30 DEGREES AND THE FLAP FAIL CAUTION MESSAGE WAS POSTED. AN UNEVENTFUL FLAP 30 LANDING WAS CARRIED OUT. THE LT BPSU WAS REPLACED AND THE SYS TESTED SERVICEABLE. PN 5913000, S/N A0508, IPC 27-52-03, FIG 1-5.Aug 3, 2012 · Bombdr CL6002D15 · Trailing Edge Flap Control SystemSDR ASOA2012080302030Glowstrip · brokenPHOTO LUMINESCENT AROUND SERVICE DOOR IS BROKEN OFF. R & R TRIM PANEL ON LT SIDE OF SERVICE DOOR IAW AMM 25-26-07. NO FURTHER DEFECTS NOTED, ACFT OK FOR SERVICE.Jul 31, 2012 · N138EV · Cndair CL6002D24 · Emergency EquipmentSDR CA120801008Tube · cracked(CAN) DURING TROUBLESHOOTING OF AN AIR CONDITIONING PROBLEM, MAINTENANCE FOUND THE RT RAM AIR WATER SPRAYER TUBE PART NR MM670-97132-001, IPC 21-52-02-01-030, LOOSE. FURTHER TROUBLESHOOTING REVEALED THAT 2 BRACKETS AND 1 CLAMP SECURING THE TUBE IN PLACE WERE BJul 30, 2012 · Bombdr CL6002D15 · Cabin Cooling SystemSDR CA120801006Fuel/Oil Cooler · failed(CAN) IN THE CLIMB THE RT OIL TEMP WENT TO 171C IN THE RED. THE CREW REDUCED POWER TO LOWER THE OIL TEMP AND THE ACFT RETURNED TO THE DEPARTURE AIRPORT. MAINTENANCE T/S DETERMINED THAT THE RT FUEL OIL COOLER WAS AT FAULT AND REPLACED THE UNIT. PN 4119T36P03Jul 27, 2012 · Bombdr CL6002D15 · Engine Oil CoolerSDR CA120830001Blades · broken(CAN) DURING CLIMB OUT THROUGH APPROXIMATELY 30000` A LOUD BANG WAS HEARD WHICH WAS FOLLOWED BY A YAW AND RT ENGINE INDICATIONS SPOOLED DOWN. ADDITIONALLY, AN AMBER RT ENGINE FLAME OUT MESSAGE WAS RECEIVED. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED AJul 26, 2012 · Bombdr CL6002D15 · Turbine SectionSDR CA120723014Holder · shorted(CAN) DURING CRUISE FLIGHT AT FL350 THE F/O CHART HOLDER BEGAN TO SMOKE AND SPARK. CB 2G6 TRIPPED AND THE SMOKE DISSIPATED ALMOST IMMEDIATELY. THE FLIGHT CONTINUED TO DESTINATION. MAINTENANCE INVESTIGATION FOUND A SMALL SCREW BEHIND THE LIGHT ASSY ON THE CHAJul 22, 2012 · Cndair CL600* · Flight Compartment EquipmentSDR CA120723012Ballast · failed(CAN) DURING INITIAL CLIMBOUT FLIGHT CREW NOTICED AN ELECTRICAL BURNING ODOR AND ELECTED TO RETURN AND LAND. THE ACFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE COCKPIT ENTRANCE LIGHT BALLAST, PS91, AT FAULT. THE BALLAST WAS REPLACED, TESTED AND Jul 20, 2012 · Bombdr CL6002D15 · Flight Compartment Lighting
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