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 A6WA200840153Door · stiffSERVICE DOOR HARD TO OPEN. LUBED AND OPS CHECKED IAW 52-40-00, OPS CHECK GOOD. (K)Mar 7, 2008 · N466AW · Cndair CL6002B19 · Service DoorsSDR A6WA200840158Handle · stuckFLIGHT CREW REPORTS PAX DOOR OUTER HANDLE DOES NOT RELEASE WHEN THE TRIGGER IS PRESSED. (K)Mar 7, 2008 · N421ZW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840159Warning Message · illuminatedAIR DIVERSION: RED 14TH STAGE RT DUCT CAS MESSAGE DISPLAYED IN FLIGHT. COMPLIED WITH QRH, WARNING MESSAGE CLEARED. (K)Mar 7, 2008 · N446AW · Cndair CL6002B19 · Central WarningSDR VNAA0803002Apu · malfunctionedCREW REPORTED THE APU FLAMED OUT AFTER ENGINE SHUTDOWN. GROUND CREW STATED SMOKE WAS COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND SMOKE COMING FROM THE APU INTAKE DOOR, FUEL LEAKING FROM DRAIN ON TO THE AFT EQUIPMENT BAY. MAINMar 6, 2008 · N202PS · Cndair CL6002B19 · APU Core EngineSDR CA080314017Flap System · malfunctioned(CAN) FLAP FAIL MESSAGE SHORT FINAL WHEN CREW WERE SELECTING FROM FLAP 8 TO FLAP 20 POSITION, FLAPS REMAINED AT 8 DEGREES AND LANDED NORMAL. MAINT REPORTED THAT THE LIST OF FAULTS IN MDC ARE : 1- JAM 2- FECU 3- L MOTOR BRAKE THE FAULT CODES WERE RETRIEVED FRMar 6, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840154Sill · corrodedSERVICE DOOR LOWER SILL PLATE CORRODED. BLENDED IAW SRM 51-21-06. (K)Mar 5, 2008 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840157Track · crackedCHANNEL TRACK SUPPORT CRACK ON CARGO DOOR TRACK FS 574.0. (K) REPLACED IAW SRM 51-42-06. (M)Mar 5, 2008 · N436AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR AA6WA200840150Strut · underservicedON TAKEOFF RECEIVED NWS INOP AND GEAR DISAGREE, COMPLIED WITH QRH. GEAR DISAGREE ILLUMINATED APPROX 30 SECS. AFTER GEAR UP SELECTION. RETURNED FOR LANDING, LANDING WEIGHT= 41,000 LBS., MAX BTMS=2,2,2,2. SERVICE NOSE GEAR STRUT IAW 12-12-32 OPS CHECK GOOD, Mar 4, 2008 · N453AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA200840151Warning Light · illuminatedRT AOA HEAT CAUTION MESSAGE ILLUMINATED IMMEDIATELY AFTER TAKEOFF. COMPLIED WITH QRH, MESSAGE DID NOT EXTINGUISH. PERFORMED AIR RETURN TO DEPARTURE. LANDED AT 46,900 LBS, BRAKE TEMPS 3-3-5-5. (K)Mar 4, 2008 · N424AW · Cndair CL6002B19 · Central WarningSDR A6WA200840152Pcu · failedSPOILERONS FAULT STATUS MESSAGE ILLUMINATED. NOTE: THIS OCCURRED ON THE GROUND. AFTER MDC INTERROGATION FOUND SECU 2A LABEL 350 CODE: 00402 CODE: LT IB PCU FAIL. SWAPPED SECU UNITS TO PUT 49-164-05 IN THE NR 1 POSITION AND PLACED PCU ON MEL 27-62-03. (K)Mar 4, 2008 · N469AW · Cndair CL6002B19 · Drag Control SystemSDR MASA200800181Scavenge Pump · malfunctionedASH 7423 MDT-ORD. EN ROUTE TO ORD AIRCRAFT DIVERTED TO PIT DUE TO LT ENG SHUTDOWN IN FLIGHT. MX CHANGED LUBE/SCAV PUMP, MASTER CHIP SEALS, OP AND LEAD CHECK GOOD.Mar 2, 2008 · N75995 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200840149Flap System · failedAFTER LANDING, ON TAXI, FLAPS FAILED CAS MESSAGE (45 DEGREES) PERFORMED RESET IAW SUPPLEMENT 98-018B. DURING TEST FLAPS FAILED AT 20 DEGREES. (K)Mar 2, 2008 · N428AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840148Element · malfunctionedRT 14TH DUCT FAIL MESSAGE ILLUMINATED AT 15,000 FT AFTER DEPARTURE. PERFORMED QRH, MESSAGE DID NOT EXTINGUISH FOR APPROX 12 MINUTES. AIR DIVERSION DECLARED EMERGENCY LANDING. (K) REMOVED AND REPLACED FUSELAGE SENSING ELEMENT A46WK (RT SIDE) IAW AMM 36-21-04Mar 1, 2008 · N446AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200840155Step · crackedPAX DOOR STAIR AFT WEB CRACK ON 1ST AND 2ND STEP CORNER AREA. REPAIRED IAW REO 601R-52-11-702 REV A. (K)Feb 29, 2008 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840156Drag Angle · crackedPAX DOOR AFT DRAG ANGLE FOUND CRACK. REPAIRED IAW REO 601R-52-11-513 REV A. (K)Feb 29, 2008 · N410AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200819624Shaft · wornRIGHT ENGINE AFT MOUNT THRUST SHAFT IS WORN, FOUND AT C-CHECK. REPLACED ENGINE THRUST SHAFT IAW CRJ200 AMM 71-00-00-400-801.Feb 27, 2008 · N909SW · Cndair CL6002B19 · Engine Mount SectionSDR VNAA0802021Fairing · damagedCREW REPORTED THE RIGHT WING STRUCK THE GROUND UPON LANDING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND WINGTIP LOWER SKIN PANEL. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND WINGTIP FAIRING IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAFeb 26, 2008 · N250PS · Cndair CL6002B19 · Wing, Plate/SkinSDR VNAA0802019Tire · separatedCREW REPORTED THE LEFT HAND OUTBOARD MAIN TIRE'S TREAD SEPARATED. MAINTENANCE INSPECTED AND CONFIRMED THE TREAD LOSS IN ADDITION TO DAMAGE TO THE LEFT HAND INBOARD FLAP ASSEMBLY AND LEFT GEAR DOOR. MAINTENANCE REMOVED AND REPLACED THE MAIN TIRE, FLAP ASSEMBLFeb 25, 2008 · N207PS · Cndair CL6002B19 · TireSDR CHQA200800039Warning Light · illuminatedSDF TO IAH - AFTER TAKEOFF, THE CREW RECEIVED A REV NR 1 UNLOCK MESSAGE ON EICAS, THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO FIELD AND LANDED UNEVENTFULLY AT SDF. MAINTENANCE LOCKED OUT THE REVERSER AND PLACED IT ON MEL.Feb 23, 2008 · N469SM · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA0802016Tire · separatedCREW REPORTED THE RIGHT INBOARD TIRE SEPARATED. MAINTENANCE INSPECTED AND FOUND THE TREAD SEPARATION AND DAMAGE TO THE RIGHT INBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE NR 3 AND NR 4 MAIN TIRES. MAINTENANCE REPAIRED FLAP DAMAGE PER REO 601R57-52-716 Feb 23, 2008 · N253PS · Cndair CL6002B19 · TireSDR VNAA0802015Door · openCREW REPORTED A NOISE FROM THE FRONT THE AIRCRAFT AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COMM DOOR OPEN. MAINTENANCE SECURED DOOR CLOSED AND FOUND NO DEFECTS OR DAMAGE. AIRCRAFT WAS RELFeb 23, 2008 · N247JS · Cndair CL6002B19 · Accessory Compartment DoorsSDR CA080221003Pump · unserviceable(CAN) CREW RECEIVED A GEAR DISAGREE MESSAGE AFTER TAKEOFF WITH AN APPLICABLE RED NOSE GEAR INDICATION AND 2 MAIN GEAR AMBER MESSAGES. CREW ACTIONED THEIR QRH AND DO AN ALTERNATE EXTENSION, A/C RETURNED. PSEU CODES RETRIEVED AND THE AC WAS ROUTED WHERE MAINT WIFeb 20, 2008 · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CHQA200800034Flap System · out of rigIAH TO SDF - WHILE ON APPROACH TO SDF, THE FLAPS WERE SELECTED TO 8 THE CREW RECEIVED A FLAP FAIL MESSAGE AND THE FLAPS WERE FAILED AT ZERO DEGREES. THE FLIGHT LANDED WITHOUT INCIDENT IN SDF. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND FOUND THE LEFT AND INBFeb 19, 2008 · N469SM · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CHQA200800033Selector Valve · malfunctionedIAH TO CRP - ON TAKEOFF, WHEN THE LANDING GEAR LEVER WAS SELECTED UP THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE AND THE NOSE LANDING GEAR RETRACTED AND LOCKED, BUT THE MAIN LANDING GEAR SHOWED RED AND UNLOCKED. THE LANDING GEAR WAS SELECTED DOWN AND THFeb 18, 2008 · N650BR · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200840097Brake Assy · malfunctionedFLAPS HALF SPEED MESSAGE ON ED2. REMOVED AND REPLACED MOTOR BRAKE UNIT IAW 27-52-05. OPS CHECK GOOD AT THIS TIME. (M)Feb 18, 2008 · N441ZW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200840098Light · inoperativeFLOOR LEVEL EMERGENCY LIGHTING ADJACENT TO ROW 1, ORANGE SEGMENT FWD INOPERATIVE. (K)Feb 18, 2008 · N407AW · Cndair CL6002B19 · Emergency LightingSDR CA080229001Window · crackedFLT NR 6671 - FIRST OFFICER SIDE WINDOW CRACKED ON DESCENT INTO PSP. WINDOW REPLACED (TC NR 20080229001)Feb 18, 2008 · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200840096Detector · malfunctionedON SHORT FINAL FLAPS FAILED AT 45 DEGREES. RAN QRH. NO FURTHER PROBLEMS. REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15. OPS CHECK GOOD IAW AMM 27-54-00. (K)Feb 17, 2008 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840015Warning System · activatedNOSE GEAR DISAGREE WHEN GEAR RETRACTED. NOSE GEAR SHOWED RED, ALSO HEARD CLICKING NOISE BELOW FEET. AIR RETURN TO BTV, UPON GEAR EXTENSION GEAR SHOWED 3 GREEN DOWN AND LOCKED. (K)Feb 16, 2008 · N441ZW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840100Rudder · malfunctionedUNCOMMANDED FULL RT RUDDER AT HIGH ALTITUDE CLIMB 280 KNOTS WITH YAW DAMPER ENGAGED, STEPPED ON RUDDER TO CORRECT AND TRIMMED BACK IN POSITION, PROCEEDED NORMALLY. (K)Feb 15, 2008 · N417AW · Cndair CL6002B19 · Rudder Control SystemSDR MASA200800131Garlock Seal · defectiveASH FLT 7423 MDT-ORD, LEFT ENGINE OIL PRESSURE FLUCTUATING WARNING. CREW REDUCED THROTTLE AND PRESSURE STABILIZED. DECLARED EMERGENCY. REPLACED STARTER GARLOCK SEAL.Feb 14, 2008 · N75991 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200840099Fuel Line · leakingFUEL LEAKING FROM DRAIN UNDER AFT FUSELAGE. REMOVED AND REPLACED FUEL LINE ASSY IAW 28-20-01. (K)Feb 14, 2008 · N425AW · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR VNAA0802011Pdu · failedCREW REPORTED A RIGHT HAND REV UNLOCK MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT HAND THRUST REVERSER PER MEL 78-30-1-1. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT INFeb 14, 2008 · N246PS · Cndair CL6002B19 · Engine Thrust ReverserSDR CA080215011Flap System · failed(CAN) DURING SELECTION OF FLAPS FROM 30 DEG TO 45 DEG ON APPROACH RECEIVED (FLAP FAI) MESSAGE ON EICAS. FLAPS FAILED TO MOVE WITH INDICATION OF 34 DEG. NORMAL LANDING. MAINT INSP FOUND NO ABNORMALITIES. FLAP DRIVE SHAFTS REMOVED AND LUBRICATED IAW COMPANY POLFeb 14, 2008 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840095Coffeemaker · malfunctionedIN FLIGHT WHEN FLIGHT ATTENDANT TURNED ON COFFEE MAKER IT STARTED TO SMOKE. STOPPED SMOKING WHEN IT WAS TURNED OFF. REMOVED AND REPLACED COFFEE MAKER. (K)Feb 13, 2008 · N464AW · Cndair CL6002B19 · Buffet/GalleysSDR A6WA200840091Structure · crackedREPAIR CRACK ON PAX DOOR AFT SIDEWALL LOWER SIDE FWD OF DOOR ASSIST MOTOR PULLEY ASSY. (K) CRACK ON PAX DOOR REPAIRED IAW REO 601-52-11-513 REV A. (M)Feb 13, 2008 · N429AW · Cndair CL6002B19 · Passenger Compartment EquipmentSDR A6WA200840068Flap · malfunctionedFLAPS FAIL CAUTION DISPLAYED ON FINAL APPROACH, COMPLIED WITH QRH BOTH FLAPS DISPLAYED 45 DEGREES. RESET FLAPS, OPS CHECK OK IAW AMM 27-50-AND AWAC SUPLEMENT 98-018B. (K)Feb 12, 2008 · N467AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0802009Blades · damagedCREW REPORTED A BIRD STRIKE TO THE RIGHT HAND ENGINE ON APPROACH. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE ENGINE AND FOUND REMAINS AND DAMAGE TO SEVERAL BLADES. MAINTENANCE REMOVED AND REPLACED DAMAGED BLADES IN ACCORDANCE WITH THE AIRCRAFT MAINTENAFeb 12, 2008 · N256PS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR A6WA200840087Support · crackedCRACK SUSPECTED IN AC GROUND POWER BOX. (K) A/C CONNECTOR SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M)Feb 12, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840094Bulkhead · crackedCRACK FOUND ON REAR PRESSURE BULKHEAD WEB FS 621.00, WL 106.17, LBL 36.00 (LINTEL ATTACHMENT FITTING). (K) REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1230 REV D. (M)Feb 12, 2008 · N429AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840067Ahrs · malfunctionedCOMPLETE NR 1 AHRS FAILURE IN FLIGHT. COMPLIED WITH QRH. NO ALTITUDE OR COMPASS INFORMATION. AFTER REVERSIONARY SLELECTION TO NR 2, ALL DISPLAY INFO WAS NORMAL ON CAPTAINS SIDE. (K)Feb 11, 2008 · N449AW · Cndair CL6002B19 · Integrated Flight SystemSDR VNAA0802005Smoke Detector · failedCREW REPORTED A SMOKE TOILET AMBER MESSAGE ON APPROACH. CREW COULD NOT VISUALLY SEE ANY SMOKE AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND MEL'D THE LAV SMOKE DETECTION SYSTEM PER MEL 26-16-01. MAINTENANCE REMOVED AND REPLACED THE LAVATFeb 11, 2008 · N258PS · Cndair CL6002B19 · Smoke DetectionSDR VNAA0802008Controller · malfunctionedCREW REPORTED A FLAPS FAIL MESSAGE ON APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET FLAP CONTROLLER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.Feb 11, 2008 · N226JS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840079Bulkhead · crackedPILOTS BULKHEAD WEB IS CRACKED AT FS 280.00, WL 85.00 LBL 27.00. (K) REPAIRED WEB IAW SRM 51-71-28 FIGURE 2. (M)Feb 11, 2008 · N431AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840082Door Frame · crackedEXTERNAL AIR COUPLING DOOR FRAME CRACKED AND BENT. (K) REPAIRED IAW BSC EO 601R-53-14474A. (M)Feb 11, 2008 · N469AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200840083Frame · chafedLT FUSELAGE FRAME AT STR 654.00 HAS CHAFED BETWEEN STR 8L AND STR 9L FROM THE 10TH STAGE BLEED DUCT TIE ROD. (K) REPAIRED FRAME IAW BSC EO 601R-53-14477 BY TRIMMING OUT DAMAGE AND INSTALLING REPAIR ANGLE. (M)Feb 11, 2008 · N469AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA200840062Flap · failedFLAP FAIL CAS MESSAGE IN FLIGHT, FLAP FAILED AT ZERO DEGREES. LDNG WT= 44,300. APPROX 150 KNTS. MAT BTMS = 5,4,2,2 AND VERTICAL DESCENT RATE LESS THAN 10 FT PM. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B. STEPS 13 AND 1.4, FLAP SYS OK. (K)Feb 10, 2008 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840063Flap System · failedFLAPS FAILED AT ZERO IN FLIGHT. RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK. (K)Feb 10, 2008 · N438AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840064Connector · damagedWOW INPUT CAUTION MESSAGE DISPLAYED ON T/O ROLL AT 100 KNOTS, MESSAGE CLEARED ON GEAR RETRACTION. MESSAGE REAPPEARED ON GEAR EXTENSION DURING LANDING. PROXY FAULTS STATUS DISPLAYED ON GROUND. REPOSITIONED MLG NR 1 WOW HARNESS AS REQUIRED, CLEANED AND RESEATFeb 10, 2008 · N451AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA200840065Drive Shaft · failedFLAPS FAIL AT ZERO DEGREE, WHEN MOVING TO FLAPS 8 DEGREE ON DESCENT. COMPLIED WITH RESET PROCEDURE IWA AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAP SYS RESET OK. (K) FOUND LT DRIVE SHAFT NR 5 UNSEREVICEABLE. REMOVED AND REPLACED PER AMM 27-53-10, OPS CHECK GFeb 10, 2008 · N421ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
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