GE CF34-8C5B1

Service difficulty reports · 418

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 = 'CF348C5B1'
  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 SWIA201439144Blade · stuckEXCESSIVE N1 FAN VIBRATION ON RT ENGINE. INSPECTED RT FAN. FOUND TWO STUCK BLADES. FREED BLADES. PERFORMED VIBRATION CHECK IAW AMM. VIBRATION CHECK PASSED.Aug 16, 2014 · N797SK · Cndair CL6002C10 · Turbine Engine Air Inlet SectionSDR SIMA20140813004Engine · vibrationRIGHT ENGINE HIGH VIBRATION 2.2 PLUS AT FL250, 63 PERCENT N1. ALSO AT 8000 FT 47 PERCENT N1 1.8 VIBRATION. R & R OTBD MULTI-FUNCTIONAL SPOILER PCU. OPS & LEAK CHECKED IAW AMM 27-62-01.Aug 13, 2014 · N536EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA140820016Compressor · damaged(CAN) REJECTED TAKE-OFF, NR 1 ENGINE COMPRESSOR STALLED AT TAKEOFF POWER. OPERATOR CONFIRMED THAT THE EVENT COULD BE REPRODUCED DURING MAINTENANCE TROUBLESHOOTING. A BOROSCOPE INSPECTION WAS CONDUCTED AND DAMAGE WAS FOUND TO THE COMPRESSOR SECTION.Aug 13, 2014 · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR N6WA20140719002Sensor · faultyNUMBER 1 ENG HIGH OIL TEMP IN FLIGHT, ENG SHUTDOWN. R & R NR 1 ENG OIL LEVEL & TEMP SENSOR IAW AMM 79-31-01.Jul 19, 2014 · N168GJ · Cndair CL6002C10 · Engine Oil Indicating SystemSDR SIMA20140717001Unknown · malfunctionedLOUD BANG ON LT SIDE ENG INFLIGHT N1 & N2 FLUCTUATING 2%, ITT FLUCTUATING 15* ON LT ENG. LOUD BOOM SOUND FROM LT SIDE OF ACFT EVERY 15 SEC OR SO AUDIBLE IN THE COCKPIT. PERFORMED MANUAL TASK 72-00-00-700-801, NO DEFECTS NOTED.Jul 17, 2014 · N546FF · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA20140713001Engine · vibrationNUMBER 1 ENG N1 VIBE 1.9. INSPECTED NR 1 ENG BLADES FOR STIFFNESS CHECK & PERFORMED ENG RUN. FOUND TO HAVE 0.2 N1 VIBE AT THIS TIME IAW AMM 72-21-02. PLACED ON CARRYOVER 4239.Jul 13, 2014 · N165GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA20140617002Warning System · false activationABORTED TAKEOFF DUE TO LT ENG IIT FLAGGING RED & OVER TEMPED. PERFORMED FIM TASK IAW CRJ700 72-00-00, NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE.Jun 17, 2014 · N157GJ · Cndair CL6002C10 · Engine EGT/TIT Indicating SystemSDR VNAA2014060200001Window · separatedCREW REPORTED WINDOW OUTSIDE PANEL MISSING AT ROW 15 D/F ON RT SIDE OF ACFT AND DAMAGE TO RT ENGINE FAN BLADES. MAINTENANCE INSPECTED, INSTALLED NEW OUTER PANEL AND R & R INNER PANEL FOR SIDE WINDOW AT ROW 15 D/F AND R & R RT ENGINE. MAINTENANCE PERFORMED CHJun 2, 2014 · N719PS · Cndair CL6002C10 · Passenger Compartment WindowsSDR SWIA201437686Structure · gougedFOUND A GOUGED AREA ABOUT A .2500" LONG AT THE VERY INBD T/E, TOP SIDE OF THE LT WING. COMPLIED WITH REPAIR OF THE GOUGE AT THE VERY INBD T/E, TOP SIDE OF THE LT WING IAW EA.May 15, 2014 · N793SK · Cndair CL6002C10 · Wing Main, Frame StructureSDR N6WA2014051202Engine · vibrationLEFT ENG VIB AT 2.9 AT ONE POINT. INSPECTED ENG FAN BLADES FOR STIFFNESS & FOR ICE, SHOOK FAN BLADES & PERFORMED ENG RUN IAW AMM 72-21-02 ANS 71-00-00.May 12, 2014 · N168GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2014051203Indication Sys · faultyN1 VIBRATION REACHED 2.6 IN FLIGHT AIR RETURN TO DEN VIBRATION 2.6. SWAPPED N1 FAN PICKUP FROM LT TO RT IAW AMM 77-11-01. PERFORMED PWR RUN WITH CREW. VIBRATION INDICATION APPEARS TO BE ERRONEOUS. ACFT SAFE FOR ONE TIME FERRY FLIGHT FROM DEN TO STL.May 12, 2014 · N168GJ · Cndair CL6002C10 · Engine Vibration AnalyzerSDR SWIA201437688Floorbeam · crackedFS 280 FLOORBEAM HAS A CRACK AT RT BL 14.0 & LT BL 14.0 ON THE UPPER FLANGE. R & R RT AND LT FS 280.00 CROSSBEAMS AND RESTORED FINISH IAW SRM.May 6, 2014 · N793SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA201438010Blowout Door · looseRT LOWER COWL BLOW OUT DOOR HAS PLAY AT HINGES. C-CHECK, REPLACED OTBD SIDE IAW SRM.Apr 1, 2014 · N227AG · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA201438011Blowout Door · looseRT LOWER COWL BLOW OUT DOOR HAS PLAY AT HINGES. C-CHECK, REPLACED INBD SIDE IAW SRM.Apr 1, 2014 · N227AG · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWIA201438121Latch · wornRT ENGINE LOWER COWL BLOW OUT DOOR LATCH CATCH WORN. C-CHECK, R & R DOOR LATCH CATCH IAW SRM.Mar 31, 2014 · N227AG · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR N6WA20140320001Engine · bird ingestionBIRD STRIKE ON LT ENG MULTIPLE FAN BLADES DAMAGED. PERFORMED BIRD STRIKE INSP IA WCRJ700 AMM 05-51-25 & 72-00-00. NO BIRD REMAINS PRESENT IN THE CORE PATH, NO VISIBLE DAMAGE.Mar 20, 2014 · N166GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA201436674Battery Pack · dischargedEMERGENCY LIGHTS AT EXIT ROWS FAILED. ALLOWED EMERGENCY LIGHT BATTERIES TO CHARGE.Mar 9, 2014 · N779SK · Cndair CL6002C10 · Emergency LightingSDR VNAA2014030600006Shutoff Valve · failedCREW REPORTED LT ENGINE BLEED AMBER CAUTION MESSAGE IN FLIGHT. CREW COMPLIED WITH QRH AND RETURNED TO FIELD. MAINTENANCE TROUBLESHOT, R & R LT ENGINE PRESSURE-REGULATING SHUT-OFF VALVE AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.Mar 6, 2014 · N705PS · Cndair CL6002C10 · Pneumatic Distribution SystemSDR N6WA20140302003Pump · faultyLEFT ENG HIGH OIL TEMP. R & R NR 1 ENG LUBE & SCAVENGE OIL PUMP IAW CRJ700 AMM 71-00-00, OPERATIONS & LEAK CHECK GOOD. PERFORMED ENG RUN UP IAW CRJ700 AMM 71-00-00, NO DEFECTS NOTED.Mar 2, 2014 · N161GJ · Cndair CL6002C10 · Turbine Engine Oil SystemSDR VNAA2014010900006Pump · failedCREW REPORTED A LEFT SCAVENGER EJECTOR AMBER MESSAGE ON CLIMBOUT. NR 1 ENGINE SURGED BETWEEN 55 -78 PERCENT N1 AT CLIMB POWER. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED GROUND RUN AND FOUND LT ENGINE WOULD NOT ADVANCE TO CLIMBJan 9, 2014 · N703PS · Cndair CL6002C10 · Engine Fuel PumpSDR N6WA20131226002Warning System · activatedLEFT THRUST REVERSER CAUTION MESSAGE. DEFERRED LT T/R IAW MEL 78-30-01.Dec 26, 2013 · N159GJ · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20131218002Relay · faultyRIGHT ENG WILL NOT START, STRONG FUEL SMELL. R & R START RELAY CHANNEL A K24 & START RELAY CHANNEL B K 26, IAW CRJ 700 AMM CHAPT 20-42-00 & CHAPT 24-05-09. OPERATIONS CHECKED GOOD.Dec 18, 2013 · N543EA · Cndair CL6002C10 · Engine CrankingSDR SIMA20131209008Compressor Blade · damagedSTAGE 7 COMPRESSOR BLADE HAS DAMAGE, OUT OF LIMITS, AS VIEWED THROUGH PORT S9, LT ESN GEE194949. INSTALLED ESN GEE965344.Dec 9, 2013 · N525AE · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SIMA20131209010Compressor Blade · damagedLEFT ENG STAGE 7 COMPRESSOR BLADE HAS DAMAGE AS VIEWED THROUGH PORT S9. BLADE FOUND OUT OF LIMITS IAW PAGE 34 FIGURE 7 OF WC 000-72-430-102. DEPTH OF DAMAGE MEASURED AT 052 INCHES. ALLOWABLE DAMAGE 040 INCHES. R & R LT ENG IAW AE WC'S 71-001 & 71-002 OPERADec 9, 2013 · N525AE · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR N6WA20131119001Thrust Reverser · malfunctionedABORTED TAKEOFF DUE TO LT THRUST REVERSER UNSAFE ON ROLLOUT. LOCKED OUT & DEFERRED LT THRUST REVERSER ON DMI IAW MEL 78-30-01 CAT C.Nov 19, 2013 · N159GJ · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20131118001O-Ring · failedTHE CREW REPORTED THAT RT OIL LEVEL LOW STATUS MESSAGE POSTED ON CLIMBOUT. THE MENU PAGE SHOWED 18 PERCENT, EVENTUALLY FALLING TO 15 PERCENT. THE CREW COMPLETED THE APPROPRIATE CHECKLIST. THE OIL PRRESSURE FELL INTO AMBER AN AMBER RANGE ON EICAS, FOLLOWED SHNov 16, 2013 · N537EA · Cndair CL6002C10 · Turbine Engine Oil SystemSDR SIMA20131112014Engine · vibrationCREW REPORTED AT FL 290, NOTICED LT ENGINE VIBRATION IN AMBER RANGE. COMPLIED WITH AOM, VOL 1 PROCEDURES AND INITALLY WAS ABLE TO REDUCE VIBRATION. DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DEPARTURE. DURING DESCENT, WAS ABLE TO REGAIN NORMAL ENGINE VNov 12, 2013 · N525AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA131002001Stud · fractured(CAN) THE HPT ROTOR MODULE, S/N RDUC1253, FROM CF34-8C5B1, WAS SHIPPED FOR REFURBISHMENT (NEW STAGE 1 & 2 BLADES AND STAGE 1 & 2 SHROUDS). THE HPT DISKS WERE NOT SEPARATED DURING THE REPAIR. (FOR REFERENCE, QTY-26 HPT STUDS ASSEMBLE THE STAGE 1 AND STAGE 2 HPSep 30, 2013 · Turbine SectionSDR SIMA20130926005Engine · power lossCREW REPORTED DURING DEPARTURE, BETWEEN 80KTS AND V1., ACFT FELT SLIGHT YAW MOVEMENT TO THE SIDES. AT THE SAME TIME THE F/O CALLED FOR AN ABORT DUE TO LT ENGINE POWER LOSS. CREW INITIATED ABORT PROCEDURES. COMPLETED ENGINE SHUTDOWN PROCEDURES. INFORMED OFSep 26, 2013 · N541EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20130917001Engine · vibrationLEFT ENGINE, HIGH VIBATION ON CLIMBOUT WENT UP TO 1.8 BEFORE WE LEVELED OFF AND BROUGHT BACK THE POWER. PREFORMED FIM TASK 72-00-00-810-011. ALL VIBRATIONS WITHIN LIMITS.Sep 17, 2013 · N542EA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2013071701Placard · damagedPAX DOOR EXIT SIGN IS WORN. INSPECTED & FOUND PLACARD TO BE SCUFFED AND NOT WORN, CLEANED MARKS AND SCUFFS OFF OF PLACARD IAW AMM 12-21-00.Jul 17, 2013 · N167GJ · Cndair CL6002C10 · Placards and MarkingsSDR WVER201306205181Drag Angle · crackedLEFT SIDE FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE IS CRACKED APPROXIMATELY 2 INCHES LONG.Jun 20, 2013 · N518LR · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR MASA2013061652486Light · inoperativeRIGHT OVERWING EXIT SIGN HAS 3 LAMPS INOP. REPLACED BULBS.Jun 16, 2013 · N521LR · Cndair CL6002C10 · Emergency LightingSDR SWIA201333694Skin · chafedSKIN CHAFED BS 969 BELLY AREA UNDER PANEL 196DR. BLENDED OUT CHAFE IAW REO.Jun 11, 2013 · N631SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR CA130521014Engine · malfunctioned(CAN) DURING TAKEOFF, THE COCKPIT CREW NOTICED A LOUD NOISE FOLLOWED BY RAPID THRUST CHANGES ON THE ENGINE NR 2. THERE WAS NO ENGINE VIB INDICATION ON THE EICAS DISPLAYED.May 21, 2013 · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA130528004Computer · failed(CAN) CREW REPORTED THE FUELER OBSERVED SMOKE COMING FROM REFUEL PANEL. MAINTENANCE REMOVED AND REPLACED REFUEL/DEFUEL CONTROL PANEL PER AMM 28-25-18. DURING OPS CHECK MAINTENANCE OBSERVED SMOKE VISUALLY ALONG WITH STRONG BURNING ODOR. OPS CHECK FAILED. MAIMay 20, 2013 · Cndair CL6002C10 · Aircraft Fuel Distribution SystemSDR VNAA2013042800021Fadec · failedCREW REPORTED THE RIGHT ENGINE FLAMED OUT. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT ENGINE FADEC PER AIRCRAFT MANUALS. OPERATION CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAApr 28, 2013 · N712PS · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR CA130327005Engine · bird ingestion(CAN) ACFT RETURNED TO ORIGIN AFTER SEVERAL BIRDS WERE INGESTED INTO THE RT ENGINE. VIB OF 9.9 INDICATED, CREW SHUTDOWN RT ENGINE AND RETURNED. DECLARED EMERGENCY ON SHORT FINAL.Mar 24, 2013 · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA121206005Fan · iced(CAN) CREW REPORTED HIGH RT ENGINE FAN VIBRATES. REPORTED VIBES AT 1.7 TO 1.9 AND THEN JUMPING TO ABOVE 3.5 BRIEFLY. THEY WERE NOT IN ICING CONDITIONS BUT PERFORMED ICE SHEDDING PROCEDURE IN QRH WITHOUT ACCEPTABLE RESULT. CREW ELECTED TO DIVERT AND DECLAREDDec 4, 2012 · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR N6WA2012092301Seal · leakingESCAPE HATCH LEAKING. CLEANED ESCAPE HATCH SEALING SURFACE, INSPECTED SEAL AND SEALING AREA IAW AMM 52-22-00 NO DEFECTS NOTED AT THIS TIME.Sep 23, 2012 · N156GJ · Cndair CL6002C10 · Emergency ExitsSDR N6WA2012092101Light · inoperativeEMERGENCY LIGHT OVER ROW 4 INOPERATIVE.Sep 21, 2012 · N153GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA2012091901Bulb · inoperativeEMERGENCY LIGHT IN ROW 15 ON CEILING OUT. R & R EMERGENCY LIGHT BULB AT ROW 15 IAW AMM 33-51-09. OP'S CHECK GOOD AT THIS TIME.Sep 19, 2012 · N158GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA2012091701Light · unsecureFLOOR LIGHTING STRIP AT 12C & 12D IS LOOSE. OP'S CHECKED GOOD, SECURED IAW AMM 33-51-01.Sep 17, 2012 · N159GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA2012091702Cover · missingEMERGENCY LIGHTS COVER IN GALLEY MISSING.Sep 17, 2012 · N168GJ · Cndair CL6002C10 · Emergency LightingSDR N6WA2012091401Connector · dirtyPAX DOOR LATCH CAUTION MESSAGE ALONG WITH PROXIMITY SYS FAULT 2 STATUS MSG IN FLIGHT. CLEANED BOTH SENSOR CONNECTORS ON CAM LATCH ASSY IAW AMM 52-11-02. OP'S TEST IAW AMM 25-11-00. OP'S CHECK GOOD AT THIS TIME.Sep 14, 2012 · N175GJ · Cndair CL6002C10 · Door System WiringSDR N6WA2012091001Warning Message · illuminatedPAX DOOR OUTER HANDLE CAUTION MESSAGE.Sep 10, 2012 · N175GJ · Cndair CL6002C10 · Door Warning SystemSDR N6WA2012090801Unknown · vibrationRT ENGINE FAN VIBRATION IN YELLOW 5.0, OBSERVED DURING FLIGHT. INSPECTED FAN BLADES, NO DEFECTS FOUND IAW AMM 72-21-02. PERFORMED FAN TRIM BALANCE , OP'S CHECKED GOOD IAW AMM 71-00-00.Sep 8, 2012 · N167GJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2012090703Shutoff Valve · malfunctionedRIGHT ENGINE BLEED CAUTION MESSAGE IN FLIGHT. SWAPPED LT ENGINE HIGH PRESSURE SHUTOFF VALVE WITH THE RIGHT FOR TROUBLESHOOTING. OP'S CHECKED GOOD AT THIS TIME IAW AMM 36-12-05.Sep 7, 2012 · N175GJ · Cndair CL6002C10 · Pneumatic Distribution SystemSDR N6WA2012090601Door · inoperativePAX DOOR WILL NOT RETRACT.Sep 6, 2012 · N175GJ · Cndair CL6002C10 · Passenger/Crew DoorsSDR N6WA20120903011Proximity Sensor · inoperativePAX DOOR MASTER WARNING ON GROUND WITH DOOR CLOSED AND LOCKED. R & R PASSENGER DOOR PROXIMITY SENSOR PX101 IAW AMM 52-70-04, OP'S CHECK GOOD AT THIS TIME. NO MESSAGE AT THIS TIME.Sep 3, 2012 · N165GJ · Cndair CL6002C10 · Door Warning System
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