GE CF34-8C5B1

Service difficulty reports · 418

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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 = 'CF348C5B1'
  ORDER BY difficulty_date DESC"

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SDR VNAA2018111111101Engine · vibrationON INITIAL CLIMB OUT OF JFK THERE WAS A SEVERE ENGINE VIBRATION. EMERGENCY DECLARED AND RETURN TO FIELD IMMEDIATELY. EMERGENCY CANCELED AFTER EXITING RUNWAY. EMERGENCY EQUIPMENT WAS STANDING BY BUT DID NOT RESPOND TO AIRCRAFT. THE AIRCRAFT TAXIED TO THE GATENov 11, 2018 · N530EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA20181109601Disk · crackedWAS INITIALLY WRITTEN UP FOR N1 VIBES AND LATER FOUND OIL POOLING IN THE FAN CASE. DURING LTP DISMANTLE FOR REPAIR FOUND A CRACKED STAGE 5 DISK AT THE FORWARD FLANGE. THIS CRACK ENCOMPASSES MORE THAN 180 DEGREES OF THE FORWARD FLANGENov 6, 2018 · N160GJ · Cndair CL6002C10 · Turbine SectionSDR SIMA2018092625001Oil System · low pressureDVT ALB LOW OIL PRESS (NO 1 ENG) EMERGENCY DECLARED. FLIGHT CXLD.-C/A-PENDING CORRECTIVE ACTIONS. REMOVED AND REPLACED LH ENG ASSY IAW WC-71-001 AND WC-71-002. SEE AML#4373191. NEW ENG CAME WITH ITS OWN HARNESS.Sep 25, 2018 · N538EG · Cndair CL6002C10 · Engine Oil PressureSDR VNAA2018033111101Fadec · faultyRIGHT ENGINE STUCK AT IDLE DURING FLIGHT, ALSO G OR A RIGHT FADEC CAUTION MESSAGES. MX R & R THE RT FADEC UNIT OPS CHECKED GOOD.Mar 31, 2018 · N553NN · Cndair CL6002D24 · Fuel Controlling SystemSDR ASOA201802095047Engine · failedPILOT REPORTED THE RT ENGINE FAILED AFTER TAKEOFF. SECURED THE ENGINE AND LANDED. MX REMOVED AND REPLACED THE RIGHT ENGINE. ACFT APPROVED FOR RETURN TO SERVICE.Feb 9, 2018 · N754EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20171213002Bleed Valve · failedL ENG BLEED CAUTION MSG ENCOUNTERED DURING CLIMBOUT IN ICING COND-C/A-REMOVED AND REPLACED PRSOV VALVE ENG #1 & HIGH STAGE HPRSOV VALVE IAW AMM 36-12-05-000-801 /36-12-01-000-801 OPS CHECK GOOD FCF SATATISFACTORY. PRESSURE REGULATION SHUTOFF VALVE P/N GG670-8Dec 13, 2017 · N527EA · Cndair CL6002C10 · Compressor Bleed ValveSDR SIMA20171212001Shutoff Valve · failedL ENG BLEED CAUTION-C/A-REMOVED AND REPLACED LH PRSOV IAW CRJ AMM TASK 36-12-01. OPS CHECK GOODDec 12, 2017 · N527EA · Cndair CL6002C10 · Engine Bleed Air SystemSDR N6WA2017120701Fan · icedN1 FAN VIBRATION IN THE YELLOW, NOT CONTROLLABLE, LEFT ENGINE SHUT DOWN. AFTER AC LANDED FOUND ICE ON SEVERAL FAN BLADES. RAN ENGINE FOR VIBE TEST , AC PASSED VIBE TEST . VIBE WAS BELOW 0.1. INSPECTED FWD AND AFT FAN NO DEFCTS NOTED REF TO CRJ700 AMM 30-22Dec 7, 2017 · N168GJ · Cndair CL6002C10 · Turbine Engine Air Inlet SectionSDR SWIA2017120543921Engine · flamed outLEFT ENGINE ITT SPIKE. LEFT ENGINE FLAME OUT MESSAGE. LEFT ENGINE SHUT DOWN. EMERGENCY DECLARED. (FLT 5240). REMOVED AND REPLACED LT ENGINE.Oct 25, 2017 · N797SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA2017070411103Fadec · failedFLIGHT DIVERTED DUE TO AN AMBER LEFT FADEC CAUTION MESSAGE. WAS ABLE TO TAXI TO A GATE. MX REPLACED THE FADEC.Jul 4, 2017 · N534AE · Cndair CL6002C10 · Fuel Controlling SystemSDR SWIA2017061243374Compressor · stalledRETURNED TO FIELD, AFTER ROTATION SEVERAL LOUD BANGS WERE HEARD FROM THE RT ENGINE, COMPRESSOR STALL. REPLACED THE RIGHT ENGINE ASSY.Jun 12, 2017 · N788SK · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SWIA201743375Engine · malfunctionedAFTER ROTATION, CREW REPORTED A LOUD BANG, FOLLOWED BY ERRATIC LEFT ENGINE INDICATIONS AND THEN A LEFT ENGINE FIRE INDICATION. ONE FIRE BOTTLE WAS DISCHARGED AND MESSAGE CLEARED. SHUT DOWN THE LEFT ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. CREW ALJun 10, 2017 · N715SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA201743202Fairing · chafedTHRUST REVERSER HINGE LINE FAIRING 433BB IS CHAFED. INSTALLED A REPLACEMENT HINGE LINE FAIRING SKIN IAW SRM.Mar 19, 2017 · N765SK · Cndair CL6002C10 · Engine Thrust ReverserSDR N6WA2016102001Engine · flamed outRIGHT ENGINE FLAMED OUT DURING V1. R & R THE ENGINE IAW AMM 71-00-00. LEAK AND OPS CHECKED GOOD.Oct 20, 2016 · N374CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2016100701Engine · failedRIGHT ENGINE FAILED. R & R THE NR 2 ENGINE IAW AMM 71-00-00. OPS AND LEAK CHECKED GOOD.Oct 7, 2016 · N653CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20161002001Fadec · faultedDURING CLIMB CREW RECEIVED R FADEC CAUTION MESSAGE. CREW COMPLIED WITH AOM VOL 1 PROCEDURES AND RETURNED TO STL WITHOUT INCIDENT. REMOVED AND REPLACED RT ENGINE FADEC IAW AMM 73-21-01. GROUND RAN AIRCRAFT NO FAULTS NOTED AT THIS TIME. ALSO NO CURRENT FAULTOct 2, 2016 · N531EG · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR VNAA2016091100008Retaining Ring · not seatedLT ENGINE VIBE OF 4.7 AND AN INTENTIONAL ENGINE SHUTDOWN AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FORWARD BLIND CAP, RETAINING RING, AFT SPINNER AND FORWARD SPINNER, AND PSep 11, 2016 · N509AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20160809002Engine · vibrationN1 FAN VIBRATION REMAINED IN AMBER DURING CLIMBOUT. COULD NOT GET ENGINE BACK TO GREEN RANGE DURING CLIMB MODE. PERFORMED FIM TASK 72-00-00, & FOUND NO MESSAGES IN CURRENT FAULTS & FAULT HISTORY. PERFORMED INSPECTION OF THE FAN BLADES FOR STIFFNESS IAW 72Aug 9, 2016 · N535EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA201607260001Engine · shutdownNR 2 ENGINE SHUTDOWN INFLIGHT. R & R THE NR 2 ENGINE IAW AMM 71-00-00.Jul 22, 2016 · N656CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20160602006Engine · malfunctionedAFTER TAKEOFF CREW HEARD A BANGING NOISE ON ROTATION. CREW DECLARED EMERGENCY & RETURNED WITHOUT INCIDENT. SUSPECT, ENGINE COMPRESSOR STALL AFTER TAKEOFF ROTATION, LOUD BANDING NOISE ACFT SWAY TO LT AND RT. R & R LT ENGINE IAW WORK CARD 71-001 AND 71-002, OJun 2, 2016 · N523AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20160411004Cooling Fan · failedDISPLAY FAN FAILED, FOLLOWED BY BURNING SMELL IN COCKPIT. VERIFIED DISPLAY COOLING FAN NR 2 FAILED. SOURCE OF ODOR. DEFERRED COOLING NR 2. M PROCEDURE COMPLIED WITH. R & R NR 2 COCKPIT DISPLAY FAN IAW AMM 21-24-12. OPERATIONS CHECKED GOOD. MEL RESTORED.Apr 11, 2016 · N535EA · Cndair CL6002C10 · Air Distribution FanSDR N6WA201602280001Structure · damagedDAMAGE FOUND TO LT ENGINE COWLING AT THE 6 O CLOCK POSITON. PERFORMED MAJOR REPAIR IAW REO 670-54-14-1129.Feb 28, 2016 · N152GJ · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR N6WA2016022600065Floor Support · corrodedCORROSION ON FLOORBEAM AT LBL 9.0 BETWEEN FS 1015.00 AND FS 1031.00. COMPLIED WITH REO 670-53-00-029, REV -A.Feb 26, 2016 · N668CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR V0XD20160211026Fireshield · gougedRIGHT LOWER FWD CORE COWL FIRE SHIELD GOUGED. DRESSED DAMAGED AREA, FABRICATED & INSTALLED REPAIR PATCH IAW REO 670-54-23-959 REV B DATED 2013 10 11.Feb 6, 2016 · N155GJ · Cndair CL6002C10 · Engine FiresealsSDR SIMA20160201003Blade · stuckDURING CLIMB OUT, LT ENG VIBRATION WAS IN AMBER RANGE. MAX READING NOTED WAS 1.8 MIL. AFTER SUBSTANTIAL REDUCTION IN THRUST IT CAME BACK TO NORMAL RANGE. DURING TROUBLESHOOTING FOUND TWO STUCK FAN BLADES ON NR 1 ENG. COMPLIED WITH FIM TASK 72-00-00-810-815Feb 1, 2016 · N539EA · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR VNAA2016011500013Seal · leakingCREW REPORTED RT BLEED DUCT WARNING MESSAGE FOLLOWED BY RT BLEED DUCT AMBER MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND INSPECTED AND FOUND RT PYLON BLEED AIR SUPPLY STUB DUCT OUTER SLEEVE DAMAGED AND SEAL LEAKINGJan 15, 2016 · N503AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR SWIA201541702Control Handle · failedGEAR DISAGREE ON TAKEOFF. R & R THE MLG CONTROL HANDLE AND LANDING GEAR SELECTOR VALVE, OPS CHECKED GOOD IAW AMM. PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW AMM. OPS CHECK GOOD.Dec 24, 2015 · N773SK · Cndair CL6002C10 · Landing Gear SelectorSDR N6WA2015120501Compressor Blade · damagedRIGHT ENG FLAME OUT ON SHORT FINAL. INSPECTED 6TH STAGE CHECK VLV, FOUND TO BE WORN. R & R CHECK VLV IAW AMM 36-11-03. BORESCOPE INSPECTION OF NR 2 ENG REQUIRED. PERFORMED BORESCOPE INSPECTION OF NR 2 ENG IAW AMM 72-32-00. FOUND DAMAGE TO 5TH STAGE COMPREDec 5, 2015 · N367CA · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR VNAA2015112300012Shutoff Valve · failedCREW REPORTED CABIN PRESSURE POPPING AND VERY UNCOMFORTABLE ON CLIMBOUT WITH APU OFF AND USING ENGINES AS BLEED SOURCE. LEFT PRESSURE REGULATING SHUTOFF VALVE CYCLING NONSTOP. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & RNov 23, 2015 · N709PS · Cndair CL6002C10 · Pneumatic Distribution SystemSDR SIMA20151110001Pin · lack of lubeRIGHT AFTER TAKEOFF, RT ENG VIBRATION, N1 WENT TO 1.9. WE READ THE CHECKLIST AOM VOL 1 & INITIALLY WE WERE ABLE TO CONTROL THE VIBRATION TO 1.7, GREEN, BUT AS WE CLIMBED TO FL270 VIBRATION GOT WORSE UP TO 2.1, AMBER, & WE WERE NOT ABLE TO CONTROL IT WITH POWENov 10, 2015 · N537EA · Cndair CL6002C10 · Turbine Engine Air Inlet SectionSDR VNAA2015102600022Check Valve · brokenCREW REPORTED LT ENGINE DEGRADED MESSAGE FOLLOWED BY LT ENGINE FLAMEOUT AT FL 360. CREW DECLARED AN EMERGENCY, DIVERTED AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, R & R LT ENGINE 6TH STAGE BLEED AIR CHECK VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOROct 26, 2015 · N514AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR CA151007017Rod End · broken(CAN) RIGHT FADEC CAUTION ILLUMINATED IN FLIGHT. B1 CODE 006794 FIM TASK 73-21-03-810-826, REMOVED AND REPLACED #2 ENGINE FMU IAW AMM 73-21-03 OPS/LEAK CHECK GOOD IAW CRJ900 71-00-00. FAA SDR ATTACHED. VG SLAVE ACTUATOR ROD END FOUND BROKEN,Oct 1, 2015 · Cndair CL6002D24 · Fuel Controlling SystemSDR V0XD20150929200Baffle · crackedLEFT UPPER THRUST REVERSER, CTR BAFFLE IS CRACKED. R & R LT UPPER THRUST REVERSER CTR BAFFLE PN:CN624-2057-201 IAW SRM 51-42-06.Sep 29, 2015 · N161GJ · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20150730004Warning System · false activationNUMBER 2 ENGINE N1 VIBRATION WENT INTO AMBER RANGE DURING CLIMB THROUGH FL 270. INSPECTED FAN BLADES FOR FREEDOM OF MOVEMENT WITH NO DEFECTS NOTED AND MAX VIBE AT .3 IPS AT TAKE OFF POWER. R & R BLADES IAW NRWC 9AE-DFW-01612.Jul 30, 2015 · N529EA · Cndair CL6002C10 · Engine Vibration AnalyzerSDR SIMA20150719002Engine · vibrationDIVERTED EMER DUE TO UNCONTROLLABLE EXCESSIVE NR 1 ENG VIBRATION AT 17000, NR 1 1.5%, NR 2 .3%, ABOVE FL 250 NR 1 1.8 - 2.0. PULLED NR 1 THRUST LEVER BACK TO KEEP IN GREEN. AT FL 340 UNABLE TO MAINTAIN AIRSPEED & ALT WITH NR 1 THRUST LEVER & NR 2 NEEDED TO BJul 19, 2015 · N530EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA2015062800039Fadec · failedCREW REPORTED LT FADEC FAULT 2 WHITE STATUS MESSAGE. CREW FOLLOWED QRH. SHORTLY THEREAFTER, MESSAGE DISAPPEARED AND LT FADEC AMBER MESSAGE APPEARED. AFTER BEING UNABLE TO MAINTAIN ALTITUDE DUE TO DECREASING AIRSPEED, CREW DECLARED AN EMERGENCY AND LANDED ATJun 28, 2015 · N703PS · Cndair CL6002C10 · Fuel Controlling SystemSDR N6WA2015062402Engine · overtempITT ON RT ENG EXCEEDED LIMITS ON TAKEOFF. PERFORMED INSPECTION & MX ACTIONS FOR ITT OVER TEMP EVENT. PERFORMED POWER ASSURANCE RUN IAW AMM 71-00-00. FOUND TO BE WITHIN LIMITS AT THIS TIME.Jun 24, 2015 · N172GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA201541256Skin · dentedDENT ON LT ENGINE LOWER COWL JUST AFT OF THE FAN COWL, OUT OF LIMITS. REPAIRED IAW SRM.Jun 9, 2015 · N784SK · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR N6WA2015022202Engine · vibrationLEFT ENG VIBRATION IT, YELLOW, STARTED AT 8000 FEET COULDN'T MAINTAIN CLIMB THRUST. INSPECTED NR 1 ENG FAN BLADES FOR FREE & FOR DEFECTS. PERFORMED THE VIBRATION CHECK IAW AMM 71-00-00-720-806. NR 1 ENG OPERATED WITHIN LIMITS.Feb 22, 2015 · N156GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2015021801Engine · failedBANG HEARD DURING TAKEOFF ON LT SIDE OF ACFT. ALSO, BRIEF APR INDICATION ON LT ENGINE AT ROTATION IN WIND SHEAR CONDITIONS. R & R NR 1 ENGINE IAW AMM 71-00-00.Feb 18, 2015 · N152GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2015021804Engine · malfunctionedBANG HEARD ON TAKEOFF ON LT SIDE OF ACFT. ALSO, BRIEF APR INDICATION ON LT ENG AT ROTATION IN WIND SHEAR CONDITIONS. R & R NR 1 ENG IAW AMM 71-00-00.Feb 18, 2015 · N152GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2015020402Actuator · failedNUMBER 2 ENG FLAMEOUT DURING CLIMB. R & R BOTH MASTER & SLAVE VG ACTUATORS IAW AMM 75-30-03 & 75-30-01. OPERATIONS CHECKED GOOD, NO MSGS AT THIS TIME.Feb 4, 2015 · N154GJ · Cndair CL6002C10 · Compressor Bleed ControlSDR N6WA2015020301Engine · power lossHIGH N1 VIBRATION ON NR 2 ENG, N1 DROPPED TO 50 % & RETURNED TO NORMAL ABOUT 5 SECONDS LATER. PERFORMED GVI OF NR 2 ENG INLET, EXHAUST & FAN BLADES. INSPECTED FOR PRESENCE OF CHIP DETECTOR CONTINUITY, NO DIC FOUND. PERFORMED GND POWER RUN WITH CREW. NO DEFFeb 3, 2015 · N160GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA150108011Fadec · malfunctioned(CAN) RIGHT AFTER LANDING, RT ENGINE FLAMED OUT. RT ENG FLAMEOUT CAUTION MSG AND RT FADEC FAULT 1 STATUS MSG. RH FADEC TO BE REPLACED.Jan 7, 2015 · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2015010204Cover · missingLEFT EMER ROPE COVER MISSING. DEFERRED LT ROPE COVER IAW NEF 25-100-1 CAT 5.Jan 2, 2015 · N174GJ · Cndair CL6002C10 · Emergency EquipmentSDR N6WA2014122801Thrust Reverser · malfunctionedLEFT THRUST REVERSER UNSAFE CAUTION MSG. DEFERRED LT THRUST REVERSER IAW MEL 78-30-01 CAT C.Dec 28, 2014 · N162GJ · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2014121640392Baffle · brokenRIGHT ENGINE THRUST REVERSER TRANS COWL UPPER OTBD BAFFLE BROKEN. REMOVED AND REPLACED RIGHT ENGINE UPPER OUTBOARD THRUST REVERSER BAFFLE IAW REO AND SRM.Dec 14, 2014 · N227AG · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20141122008Turbine Blades · damagedRIGHT ENG FIRST STAGE TURBINE HAS MULTIPLE DAMAGED BLADES & A FUEL NOZZLE BAFFLE MISSING. MATERIAL OUT OF LIMITS IAW MM. R & R RT ENG IAW WC 71-001. OPERATIONS CHECK & LEAK CHECKED GOOD.Nov 22, 2014 · N540EG · Cndair CL6002C10 · Turbine SectionSDR SWIA201439425Sensor · inaccurateDURING CLIMBOUT THROUGH 10,000 FT, THE LT ENGINE OIL TEMP STARTED TO CLIMB RAPIDLY TO 165A C. PERFORMED QRH PROCEDURE AND RETURNED TO FIELD. OIL TEMP CAME BACK INTO NORMAL LIMITS ON DESCENT BUT REMAINED ON THE HIGH SIDE OF THE MARGIN. R & R LT ENGINE OIL LEOct 3, 2014 · N606SK · Cndair CL6002C10 · Engine Oil TemperatureSDR SIMA20140830001Fadec · failedLEFT FADEC CAUTION MSG CAME ON INFLIGHT. CLIMBING THROUGH 15,000 IT DID NOT GO OFF. R & R LT FADEC IAW AMM 73-21-01, ALL SUBSEQUENT CHECKS GOOD.Aug 30, 2014 · N537EA · Cndair CL6002C10 · Fuel Control/Turbine Engines
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