GE CF34-3B1

Service difficulty reports · 5,402

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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 = 'CF343B1'
  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 CA141217008Plug · cracked(CAN) DURING ROUTINE INSPECTION OF THE NR 1 ENGINE IDG THE DRAIN PLUG WAS FOUND TO HAVE A CRACK AROUND WHERE THE HEAD MEETS THE SHANK. THE SHANK IS SEPARATING FORM THE HEAD. PICTURES ATTACHED PLUG REPLACED AND AIRCRAFT RETURNED TO SERVICE.Dec 13, 2014 · Cndair CL6002B19 · AC Generator-AlternatorSDR SWIA201440391Diode · failedRT THRUST REVERSER UNLOCK MESSAGE. RETURNED TO FIELD. REMOVED AND REPLACED TB207-7 ASSY FOR DIODE 2CR7KE IAW ESPM.Dec 10, 2014 · N8982A · Cndair CL6002B19 · Engine Thrust ReverserSDR CA141203002Bpsu · failed(CAN) ON FLIGHT, ON DESCENT PRIOR TO APPROX FLAP WAS SELECTED TO 8 DEGREES. HAD A FLAP FAIL ICAS CAUTION MESSAGE, FLAP WAS SELECTED BACK TO 0 DEGREE IAW THERE PILOT PROCEDURE CHECK, AND ACFT RETURED BACK TO HOME BASE FOR MAINTENANCE. THE ACFT WAS PLACED INTODec 2, 2014 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA141211002Shaft · contaminated(CAN) FLAP FAIL MESSAGE WAS DISPLAYED WHEN FLAP LEVER WAS SET TO DOWN AFTER 25 MINUTE. THE AIRCRAFT RETURNED TO ORIGIN & LANDED WITH NO FLAP. AFTER POWER RESET ON GROUND FLAP OPERATION BECAME NORMAL, THEN THE AIRCRAFT WAS FERRIED. FLAP OPERATION WAS NORMAL IDec 2, 2014 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA141120017Skin · cracked(CAN) DURING A ROUTINE WALK AROUND THE PILOT NOTICED A 2 INCH LONG CRACK IN THE LEADING EDGE SKIN ON THE LWS 194. THE CRACK IS VERTICAL IN RELATION TO THE LEADING EDGE AND IS LOCATED AT RIB 6 OF THE LEADING EDGE SECTION. THE LEADING EDGE SECTION WAS REPLACED. Nov 18, 2014 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA141121002Actuator · failed(CAN) ON APPROACH, AT 4000 FT, WHEN THE FLAPS WERE SELECTED FROM 0 TO 8 DEGREES, THEY FAILED AT ZERO DEGREES WITH THE FLAP FAIL CAUTION POSTED. OAT AT THE TIME WAS -15C. AFTER CIRCLING TO COMPLETE CHECKLISTS THE ACFT LANDED UNEVENTFULLY WITH FLAPS AT ZERO. CNov 17, 2014 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA201442169Engine · failedCLIMBING THRU 19,000 FEET, HEARD A LOUD THUD & LT ENGINE N2 WENT TO ZERO. COMPLIED WITH QRH, ENGINE SHUTDOWN, DIVERTED. OIL PRESSURE AT ZERO.Nov 15, 2014 · N423AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA141114003Cable · frozen(CAN) NR 2 ENGINE THRUST LEVER FROZEN AT MIN CRUISE SETTING. CREW CHECKED FRICTION LOCKS, ALL FREE AND NR 1 LEVER HAS FREE TRAVEL. (RESOLVED ON W/O: 456461 TASKCARD: NR-00001) TIB CRJ-76-01 CARRIED OUT WITH NO FAULTS FOUND. NR 2 ENGINE THROTTLE CABLE REMOVENov 13, 2014 · Cndair CL6002B19 · Power LeverSDR CA141120018Window · cracked(CAN) RT SIDE WINDOW CRACKED.Nov 12, 2014 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA141114008Compressor · failed(CAN) CREW STATED THEY HEARD POPPING ON TAKEOFF AND ITT STARTED CLIMBING. THE RT ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WITH AN UNEVENTFUL LANDING. THE FDR SHOWS 965C MAX FOR 2 SECONDS. THE HPC HAS MAJOR IMPACT DANov 11, 2014 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA201440045Vane · chafedLEFT INBD FLAP VANE CHAFED AT INBD L/E. BLENDED THE CHAFE IAW REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440046Vane · chafedLEFT INBD FLAP VANE CHAFED AT OTBD L/E. BLENDED THE CHAFE IAW REO.Nov 8, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201440043Vane · chafedRIGHT WING INBD FLAP VANE L/E CHAFED 91.5 INCHES FROM OTBD END. BLENDED CHAFE IAW REO.Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge FlapsSDR CA141110006Ballast · failed(CAN) AIRCRAFT WAS IN DESCENT TROUGH 11000FT WHEN THE ON-BOARD AME REPORTED A STRONG ELECTRICAL OVERHEAT SMELL IN THE CABIN BUT NO SMOKE AS THE SOURCE COULD NOT BE CONFIRMED, AN IMMEDIATES DECISION TO TERMINATE FLIGHT AND LAND THE AIRCRAFT IMMEDIATELY WAS MADENov 7, 2014 · Cndair CL6002B19 · Passenger Compartment LightingSDR SWIA201440049Structure · erodedFOUND EROSION ON THE LT ENGINE NOSE COWL, 6 O'CLOCK POSITION, TO BE WITHIN LIMITS. REPAIRED IAW CMM AND REO.Nov 6, 2014 · N821AS · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR CA141107004O-Ring · torn(CAN) ON APPROACH THE HYD 3 LOW PRESS CAUTION LIGHT CAME ON, THE NR 3 HYD SYS QTY WAS OBSERVED AT 5 PERCENT. AN ALTERNATE GEAR EXTENSION WAS CARRIED OUT AND EMERGENCY DECLARED. THE ACFT LANDED UNEVENTFULLY. MAINTENANCE INVESTIGATION FOUND A HYDRAULIC LEAK ANov 6, 2014 · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA201439813Thrust Reverser · out of adjustRIGHT THRUST REVERSER UNLOCK CAUTION FAILED. ADJUSTED THE TWO THRUST REVERSER ALIGNMENT HOLES IAW AMM AND THEN LUBRICATED THE BALLSCREW ACTUATORS IAW AMM. OPS CHECKED GOOD AT THIS TIMENov 5, 2014 · N935SW · Cndair CL6002B19 · Engine Thrust ReverserSDR ASOA2014112511787Drag Angle · crackedSMALL CRACK AT PAX DOOR AFT DRAG ANGLE BY DOOR ASSIST ACTUATOR PULLEY BRACKET. COMPLIED WITH REO 601R-52-11-513. REMOVED PULLEY FITTING ASSY 601R-31706-1, REF IAW SRM 51-42-06-00. COMPLIED WITH REO 601R-52-11-513, REV A. THIS REPAIR IS CLASSIFIED AS A MAJOOct 26, 2014 · N868AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA141023012Duct · broken(CAN) PILOTS REPORTED LITTLE TO NO AIRFLOW IN FLT DECK. AIR CONDITIONING PACKS, LT, MAINTENANCE DISCOVERED THAT THE LT PACK, COCKPIT AIR SUPPLY DUCT FROM THE WATER SEPARATOR TO MAIN DUCT HAD DE-BONDED AND SEPARATED CAUSING A LEAK. DUCT REPLACED WITH NEW. POct 18, 2014 · Cndair CL6002B19 · Air Distribution SystemSDR SWIA201439804Channel · crackedLT ENGINE, FIXED CORE COWL AFT CHANNEL CRACKED AT UPPER FWD SIDE STA FS682, STA XN208.39. C-CHECK, R & R DUCT ON LT FIXED CORE COWL AFT SIDE IAW SRM AND STS EA.Oct 16, 2014 · N906SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR REXA2014100901031Grommet · missingRIGHT ENG VGV MISSING GROMMET & SEVERAL LOOSE. SEAL AT AFT BOTTOM CORNER OF RT ENG ATR BOX IS TORN 432-24. R & R RT ENG IAW CF 34 3 ENG CHANGE CHECKLIST & IAW AMM 71-00-00. COMPLIED WITH ALL REQUIRED OPERATIONS & LEAKS CHECK IAW CF 34 3 ENG CHANGE CHECKLIST Oct 9, 2014 · N833AY · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR CA141017003Swivel · misinstalled(CAN) WHILE TROUBLESHOOTING FLAT SPOT ON 2 MAIN WHEEL TIRES, IT WAS FOUND THAT BOTH LT AND RT MLG UPPER SWIVEL FITTINGS HYDRAULIC SUPPLY LINES WERE INSTALLED REVERSE ALTHOUGH SB 601R-32-110 WAS INCORPORATED ON 09/23/2014 COMPLYING WITH AD, CF-2014-10. OBJECTIVOct 9, 2014 · Cndair CL6002B19 · Main Landing GearSDR CA141002004Cable · binding(CAN) GROUND CREW WERE UNABLE TO OPEN THE PASSENGER DOOR FROM THE OUTSIDE. FOUND THE PRESSURE RELIEF DOOR TO BE OUT OF ADJUSTMENT IN THE FULL OPEN POSITION, CAUSING THE MAIN CABIN DOOR TO JAM. DOOR TRAVEL ADJUSTED & THE OPERATION OF THE MAIN CABIN DOOR HANDLOct 1, 2014 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA140919011Wire Harness · loose(CAN) CREW REPORTS OF SHUTTERING FELT IN THE NOSE GEAR AT PWR APLICATION AND THE INTERNITTANT REPORTS OF THE A/C PULLING TO THE RIGHT ON TAKE OFF ROLL. STEERING ECU REMOVED AND REPLACED IAW CRJ200 MM ATA 32-51-10. TAXI TEST CARRIED OUT. AIRCRAFT STILL WANDERS Sep 18, 2014 · Cndair CL6002B19 · Landing Gear System WiringSDR CA140917008Pulley · seized(CAN) DURING HEAVY MAINTENANCE INSPECTION, AILERON CONTROL PULLEYS FOUND SEIZED AT WING STATION 242 LT AND RT. PULLEYS REPLACED WITH NEW.Sep 17, 2014 · Cndair CL6002B19 · Aileron Control SystemSDR CA140915004Screen · crushed(CAN) THE LEFT SCAVENGE EJECTOR MESSAGE CAME ON AT THE TOP OF DESCENT AT FL200. ALL ENGINE PARAMETERS WERE NORMAL. MAINTENANCE REPLACED THE LT SCAVENGE EJECTOR ASSY WHICH CLEARED THE DEFECT. THE REMOVED SCAVENGE EJECTOR WAS DISASSEMBLED AND THE INTERNAL SCRSep 12, 2014 · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR A6WA201441943Bracket · crackedLEFT EXHAUST FAIRING STANDOFF BRACKET IS CRACKED.Sep 9, 2014 · N414ZW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR SWIA201439271Inlet · erodedLEFT ENGINE INLET HAS EROSION FROM 6 O`CLOCK POSTITION TO 8 O`CLOCK POSTION. COMPLIED WITH TEMPORARY REPAIR OF EROSION ON OUTER SKIN L/E OF LT ENGINE INLET COWL FROM 6 O`CLOCK POSITION TO 8 O`CLOCK POSITION IN REFERENCE TO REO.Sep 9, 2014 · N445SW · Cndair CL6002B19 · Turbine Engine Air Inlet SectionSDR CA140918011Bellcrank · cracked(CAN) FLIGHT CREW RECORDED A RIGHT ENGINE N2 OVERSPEED (RED INDICATING ABOVE 99.3 N2) WHILE ON AN APPROACH TO LAND. MAINTENANCE TROUBLESHOT THE IDENTIFIED DEFECT AND FOUND THE VARIABLE GUIDE VANE BELLCRANK (GE IPC FIG 10 ITEM 390, P/N 5026T46G01) FRACTURED AT Sep 8, 2014 · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA201439212Fcu · unknownLEFT ENGINE SHUTDOWN ON DESCENT. COMPLIED WITH QRH AND LANDED NORMALLY. R & R LEFT ENGINE FUEL PUMP AND FUEL CONTROL. LEAK AND OPS CHECKED GOOD.Aug 24, 2014 · N685BR · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR SWIA201439218Power Supply · failedRETURNED TO FIELD FLAP FAIL AT 0 AFTER FLAP RETRACTION. REMOVED AND REPLACED RT BPSU, OPS CHECKED GOOD IAW AMM.Aug 24, 2014 · N916SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2014082300017Wire Harness · failedCREW REPORTED LT THRUST REVERSER UNLOCK AMBER MESSAGE DURING FLIGHT. DECLARED AN EMERGENCY AND SAFELY LANDED AT DESTINATION AIRPORT. MAINTENANCE TROUBLESHOT, R & R LT ENGINE ORANGE HARNESS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Aug 23, 2014 · N245PS · Cndair CL6002B19 · Engine Exhaust System WiringSDR CA140825002Drive Unit · failed(CAN) FLAPS HALF SPEED STATUS AFTER LANDING, 1 FLAP PDU INOPERATIVE WITH NO SKEW DETECT DEFERRAL M. SKEW DETECTION DUMMY BOX REMOVED AND ORIGINAL SKEW DETECTOR REINSTALLED. PDU FOUND U/S AND REPLACED WITH NEW UNIT, INSTALLED IAW AMM 27-52-01. FLAP SYS FUNCTIAug 23, 2014 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA140825004Sensor · failed(CAN) FLAPS FAIL MESSAGE. FLAPS STOPPED AT 38 DEGREES, FERRY FLIGHT DEFERRAL, LT BPSU FOUND BINDINING, CAUSING DRAG ON FLAP SYS, LT BPSU REPLACED WITH NEW UNIT, BPSU INSTALLED AND FUNCTION CHECKED SERVICEABLE IAW AMM 27-52-01. ALL FLAP DRIVE CABLE CONNECTINGAug 23, 2014 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA140811007Adg · failed(CAN) DURING CLIMB OUT THE AIR DRIVEN GENERATOR (ADG) DEPLOYED ITSELF FOR NO APPARENT REASON, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED/LANDED WITHOUT FURTHER INCIDENT. DURING TROUBLESHOOTING, THE ADG AUTO DEPLOYMENT CONTROLLER FAILED UNIT SELF-TEST.Aug 7, 2014 · Cndair CL6002B19 · Phase AdapterSDR CA140807012Engine · malfunctioned(CAN) DURING TAXI THE CREW HAS REPORTED UNUSUAL NOISE FROM LT ENGINE ACCOMPANIED BY RAPID INCREASE IN ITT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO GATE. VISUAL INSPECTION OF ENGINE EXTERNALS HAS NOT REVEALED ANY DAMAGES HOWEVER SOME AMOUNT OF MAug 4, 2014 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA2014080711027Engine · flamed outDURING CRUISE AT FL300, NR 1 ENGINE FLAMED OUT. ATTEMPTED TWO RELIGHT ATTEMPTS WITHOUT SUCCESS. LANDED WITHOUT FURTHER INCIDENT. FLAME OUT EMERGENCY DECLARED. ENGINE CHANGED. ACFT OK FOR SERVICE.Aug 3, 2014 · N907EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA140804021Bearing · failed(CAN) AIRCRAFT WAS ENROUTE TO DESTINATION WHEN THE CREW REPORTED,VIA ACARS, THAT THEY HAD LOST THE LT ENGINE IN FLIGHT. THE CREW DID ATTEMPT TO RESTART THE ENGINE BUT IT WAS REPORTED THERE WAS NO N2 INDICATION PRESENT. AN EMERGENCY WAS DECLARED AND CREW ELECAug 3, 2014 · Cndair CL6002B19 · Accessory GearboxesSDR REXA2014072800745Engine · malfunctionedACFT EXPERIENCED INFLIGHT SHUTDOWN OF THE RT ENG. RT ENG OIL PRESS WARNING MSG & RT ENG OIL PRESS INDICATIONS WERE <30 PSI & DECREASING, FLUCTUATING. REDUCED RT ENG THRUST TO IDLE ALMOST IMMEDIATELY THEN COMPLETED QRH WITH INFLIGHT SHUTDOWN. R & R RT ENG IAJul 28, 2014 · N8972E · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201441747Wire · out of positionIDG WIRE TB208-1 ROUTED AGAINST THE PYLON SEPARATOR PN 601R37138-20 ON PANEL 422DB CAUSING AN EVENTUAL ARC & HOLE THROUGH THE SEPARATOR & DAMAGE TO THE WIRE. WIRE & SEPARATOR WERE REPLACED. THIS WAS DISCOVERED WHILE PERFORMING A ROUTINE RT ENG CHANGE.Jul 9, 2014 · N437AW · Cndair CL6002B19 · Electrical Power System WiringSDR SWIA201438617Bolt · galledLEFT ENGINE, YOKE MOUNT BOLTS HAVE GALLING MARKS. FOUND DURING LT ENGINE CHANGE. R & R LT ENGINE YOKE MOUNT BOLTS IAW AMM.Jul 4, 2014 · N885AS · Cndair CL6002B19 · Engine Mount SectionSDR SWIA201438618Bushing · galledLEFT ENGINE, YOKE MOUNT LINK BUSHINGS HAVE GALLING MARKS, FOUND DURING LT ENGINE CHANGE. R & R LT ENGINE MOUNT LINK BUSHINGS IAW AMM.Jul 4, 2014 · N885AS · Cndair CL6002B19 · Engine Mount SectionSDR A6WA201441728Cover · crackedLEFT THRUST REVERSER LOWER PYLON COVER IS CRACKED.Jul 3, 2014 · N402AW · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2014070300003Blades · damagedCREW REPORTED BIRD STRIKE AFTER TAKEOFF AND DAMAGED FAN BLADES ON RT ENGINE. CREW DECLARED EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED DEBRIS FROM RT ENGINE INLET, R & R 4 FAN BLADES AND PERFORMED CHECKS IAJul 3, 2014 · N249PS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR SWIA201438521Engine · malfunctionedNR 2 ENGINE INDICATION FLUCTUATION AND UNCOMMANDED ACCELERATION ON CLIMBOUT.Jul 2, 2014 · N693BR · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA201441723Seal · crackedLT THRUST REVERSER LOWER TORQUE BOX METAL SEAL IS CRACKED.Jul 1, 2014 · N402AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA140627007Apu · failed(CAN) DURING APU START A LOUD BANG WAS NOTED. SHORTLY AFTER THE APU SHUTDOWN SMOKE WAS NOTED COMING FROM THE INTAKE OF THE, AUXILIARY POWER UNIT. THE APU HAD CATASTROPHIC FAILURE TO THE HOT SECTION. TURBINE ASSY HAD DISINTEGRATED. SUBSTANTIAL TWISTING DAMAGJun 22, 2014 · Cndair CL6002B19 · APU Core EngineSDR VNAA2014062000019Feeder Cable · damagedCREW REPORTED LT ENGINE SURGING AT MAXIMUM CLIMB THRUST (MCT) 86.0 TO 91.0 PERCENT N1 AND LT ENGINE FUEL FLOW SURGE 2,300-2,500 AT MCT. NO SURGE BELOW 76 PERCENT N1. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LT ENGINE SPEED CJun 20, 2014 · N202PS · Cndair CL6002B19 · Engine Indicating System WiringSDR A6WA201441664Cowling · crackedLT LOWER CORE COWL FWD BAYONET HOLE HAS CRACK. REPAIRED LT LOWER CORE COWL IAW EA 25-20144-177.Jun 17, 2014 · N437AW · Cndair CL6002B19 · Engine Cowling SystemSDR CA140619010Distributor · leaking(CAN) WHILE UNDERGOING ROUTINE MAINTENANCE FUEL WAS DISCOVERED LEAKING FROM THE WING ROOT AREA. FOUND TO BE THE FUEL DISTRIBUTION BOX IN THE BELLY OF THE AIRCRAFT. FUEL BOX WAS REPLACED.Jun 17, 2014 · Cndair CL6002B19 · Aircraft Fuel Distribution System
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