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 A6WA200840066Adc · failedAIR DATA COMPUTER NR 1 FAILED IN FLIGHT. COMPLIED WITH QRH , SWITCHED TO AIR DATA COMPUTER NR 2, ALL INDICATING NORMAL AIR DIVERSION AND LANDING UNEVENTFUL. (K)Feb 10, 2008 · N435AW · Cndair CL6002B19 · Air Data ComputerSDR VNAA0802007Tire · damagedCREW REPORTED THE RIGHT INBOARD MAIN TIRE SHREDDED UPON LANDING IN PHL. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT HAND MAIN GEAR TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS FERRIED TO DAY FOR FURTHER EVALUATION AND TO REPAIR DAMAFeb 10, 2008 · N242JS · Cndair CL6002B19 · Landing Gear SystemSDR CA080211013Pcu · malfunctioned(CAN) TASK NR RJ2-27-900-714 FOR THE BACKLASH AND FUNCTIONAL CHECK OF RUDDER CONTROL SYS WAS CARRIED OUT ON THIS AC DURING A HEAVY MAINT CHECK. TEST RESULT PARAMETERS WERE FOUND BEYOND LIMITS. FURTHER INVESTIGATION DURING RECTIFICATION LEAD TO THE DISCOVERY OFFeb 10, 2008 · Cndair CL6002B19 · Rudder Control SystemSDR CHQA200800027Contactor · looseIAH TO HRL - DURING CRUISE, THE CREW NOTICED SPARKS AND SMOKE FROM AROUND THE LOWER RIGHT CORNER OF THE FO'S WINDSHIELD. THE CREW RAN THE MEMORY ITEMS FOR COCKPIT SMOKE, TURNED OFF THE WINDSHIELD HEAT, AND PULLED THE CIRCUIT BREAKER FOR THE RIGHT WINDSHIELD HFeb 9, 2008 · N653BR · Cndair CL6002B19 · Ice/Rain Protection System WiringSDR A6WA200840078Plate · corrodedSERVICE DOOR PLATE ASSY CORRODED. (K) SERVICE DOOR PLATE ASSY REPLACED.Feb 9, 2008 · N431AW · Cndair CL6002B19 · Service DoorsSDR CHQA200800026Bulb · malfunctionedCLT TO IAH - APPROXIMATELY 40 MINUTES INTO THE FLIGHT THE CREW RECEIVED AN APU OIL TEMP MESSAGE ON EICAS. THE AIRCRAFT DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE APU WITH OIL AND IT OPERATED NORMALLY, AND THE AIRCRAFT WAS RETUFeb 7, 2008 · N473CA · Cndair CL6002B19 · APU Oil SystemSDR A6WA200840080Cargo Track · corrodedAT FS 574.00, WL 73.50 CARGO TRACKS LT AND RT SIDE INNER OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-12-00. (M)Feb 7, 2008 · N431AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA200840081Cargo Track · corrodedAT FS 559.96 WL 73.50 CARGO TRACK LT AND RT SIDE INNER, OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-12-00. (M)Feb 7, 2008 · N431AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR CHQA200800024Handle · malfunctionedAFTER TAKEOFF THE CREW SELECTED THE MLG LEVER TO THE UP AND THE MLG DID NOT RETRACT. WHILE THE LEVER WAS IN THE UP POSITION, CREW RECEIVED MESSAGES FOR PARKING BRAKE SHUT-OFF VALVE AND ANTI-SKID INBOARD. EICAS INDICATING 3 GREEN AND DOWN WITH NO MLG DISAGREEFeb 6, 2008 · N478CA · Cndair CL6002B19 · Landing Gear SelectorSDR VNAA0802003Control Panel · faultyCREW REPORTED THE CAPTAINS AND FIRST OFFICERS WIPER BLADES CAME ON DURING FLIGHT MULTIPLE TIMES. THE FIRST OFFICERS SIDE CAME ON AND WOULD NOT SHUT OFF. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFeb 5, 2008 · N221PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR A6WA200840085Intercostal · crackedCRACK EXIST ON INTERCOSTAL FS 481, LBL 36 AND LBL 27 CRACK LENGTH .200. (K) REPAIRED IAW REO 601R-53-41-059. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840086Intercostal · crackedCRACK EXIST ON INTERCOSTAL FS 484, RBL 36 CRACK LENGTH .200. (K) REPAIRED INTERCOSTAL IAW REO 601R-53-41-059. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840092Structure · crackedCRACK EXIST ON FLOOR STRUCTURE FS 280, RBL 9 CRACK LENGTH .150. (K) CUT OUT DAMAGE IAW REO 601R-53-11-171. REPAIR PERFORMED IAW REO 601R-53-11-171. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840093Bracket · crackedCRACK EXIST ON BRACKET FS 280, LBL 9, ABD RBL 9 CRACK LENGTH .200. (K) REPAIR PERFORMED IAW REO 601R-53-11-171, FABRICATED NEW ANGLE. (M)Feb 5, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CHQA200800023Oil System · lowIAH TO MCI - DUE TO THE NR 2 IDG BEING ON MEL THE APU WAS REQUIRED TO BE RUN DURING THE FLIGHT. WHILE EN ROUTE TO MCI, THE CREW RECEIVED AN APU OIL TEMP CAUTION MESSAGE. THE CREW FOLLOWED THE QRH AND DIVERTED TO TUL. MAINTENANCE INSPECTED THE APU AND FOUND Feb 4, 2008 · N473CA · Cndair CL6002B19 · APU Oil SystemSDR A6WA200840101Sill · crackedCRACK FOUND ON LOWER SILL FS 572, LBL 40, UNDER BRACKET SCUFF PLATE RETAINER. LOWER SILL PLATE REPLACED IAW REO 601R53-61-690 REV D. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840088Scuff Plate · corrodedSCUFF PLATE OF SERVICE DOOR FOUND CORRODED. (K) SCUFF PLATE REPLACED IAW SRM 51-42-06 AND 51-41-02. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Service DoorsSDR A6WA200840089Radome · crackedLIGHT GLAZING ON RADOME FOUND CRACK. (K) REPLACED IAW SRM 51-42-20. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA200840090Angle · crackedANGLE CRACK AT FS 621.0 AND MEMBER BEAM OF CARGO DOOR. (K) ANGLE REPLACED IAW SRM 51-2-16 AND 51-42-20. (M)Feb 4, 2008 · N429AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CHQA200800020Seal · leakingIAH TO SRQ - DURING CLIMB, THE CREW RECEIVED A WARNING FOR E1 OIL PRESSURE. E1 OIL PRESSURE WAS NOTED TO FLUCTUATE FROM BELOW 25PSI TO 40PSI. CREW FOLLOWED THE QRH AND REDUCED THRUST ON E1, AFTER WHICH IT WAS NOTED THAT THE OIL PRESSURE HAD STABILIZED AT THEFeb 3, 2008 · N467CA · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR A6WA200840061Warning System · activatedON NORMAL TAKEOFF, SELECTED GEAR UP AND RECEIVED NLG DOOR OPEN AND GEAR DISAGREE WARNINGS AND WOW INPUT AND NWS INOP CAS MESSAGES. COMPLIED WITH QRH FOR ALL MESSAGES, ALL CLEARED, ALL 3 GEARDOWN AND LOCKED. RETURNED TO DEPARTURE FOR NORMAL LANDING. (K)Feb 3, 2008 · N460AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA0802001Selector Valve · failedCREW REPORTED A GEAR DISAGREE MESSAGE ON APPROACH. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MLG SELECTOR VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.Feb 3, 2008 · N206PS · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA200840048Pitot System · contaminatedON TAKEOFF ROLL STANDBY IAS READS -0- KNOTS, REJECTED TAKEOFF AT ABOUT 85 KNOTS, MAX BTMS = 8,7,6,6. NOTE: NO HES/RTO INSPECTION REQUIRED. FOUND WATER IN THE STANDBY PITOT/STATIC SYSTEM. PERFORMED CONTAMINATION REMOVAL OF THE STANDBY PITOT/ STATIC SYSTEM. Feb 2, 2008 · N462AW · Cndair CL6002B19 · Pitot/Static SystemSDR A6WA200840084Bulkhead · crackedLT LWR NOSE COMPARTMENT CRACK FOUND ON PRESSURE BULKHEAD AROUND BRAKE FS 202. (K) JOB PERFORMED IAW REO 601R-53-11-563. (M)Feb 2, 2008 · N429AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840058Flap · failedFLAPS FAIL CAUTION IN FLIGHT. FLAPS FAILED AT 40 DEGREES. EMERGENCY LANDING DECLARED. LANDING UNEVENTFUL. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-108B STEPS 1.3 AND 1.4, FLAPS SYSTEM RESET OK. (K)Feb 1, 2008 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840060Flap · stuckINFLIGHT, FLAPS STUCK AT 42 DEGREES WHEN SELECTED 45 DEGREES. AFTER 10 MINUTES, FLAPS WENT TO 45 DEGREES, NO FAULT MESSAGES ILLUMINATED. (K)Feb 1, 2008 · N441ZW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840074Plate · corrodedFLOOR LANDING PLATE CORRODED BETWEEN FS 559 + 112 TO FS 621, AROUND NUT PLATE HOLES. (K) CORROSION ON FLOOR LANDING PLATE BETWEEN FS 559 PLUS 112 TO FS 621 AROUND NUT PLATE HOLES, BENDED IAW SRM 51-21-06. (M)Feb 1, 2008 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840075Plate · corrodedTWO CRACKS ON FLOOR LANDING PLATE AT FS 589 AND FS 605. (K) REPAIRED IAW REO 601R-53-61-433. (M)Feb 1, 2008 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840077Support · crackedAC GROUND POWER RECEPTACLE SUPPORT MEMBER IS CRACKED. (K) SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M)Feb 1, 2008 · N431AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA080204001Oil System · overserviced(CAN) DUE TO HIGH OIL TEMP INDICATION, NR 1 ENGINE WAS SHUTDOWN BY THE CA, ACFT LANDED IN IAD WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINT INSPECTED ACFT. INVESTIGATION OF ENGINE WAS BELIEVED TO BE OVER SERVICED. WHEN MAINT OPENED THE OIFeb 1, 2008 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200840059Bpsu · faultyFLAPS FAIL CAS MESSAGE, BOTH FLAPS INDICATE 42 DEGREES. PERFORMED FLAPS RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS RESET OK. (FERRIED TO ORF DUE TO HISTORY) LT BPSU WON`T STAY IN RIG. REMOVED AND REPLACED LT PBSU IAW AMM 27-51-10-. Jan 31, 2008 · N441ZW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA0801009Idg · failedCREW ABORTED THE TAKEOFF DUE TO A GEN 2 OFF CAS MESSAGE. CREW RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED A REJECTED TAKEOFF INSPECTION AND DEFERRED THE NR 2 IDG PER MEL 24-11-01-3. MAINTENANCE REMOVED AND REPLACED THE NR 2 IDG. MEL WAS Jan 31, 2008 · N218PS · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA200840056Warning System · activatedIDG NR 1 CAUTION MESSAGE ON TAKEOFF, TAKEOFF ABORTED AT LESS THAN 80 KNOTS. (K)Jan 30, 2008 · N448AW · Cndair CL6002B19 · AC Indicating SystemSDR A6WA200840073Structure · damagedDAMAGE ON LT FUSALAGE AT STA 220. REPAIRED CUTOUT ON LT FUSELAGE IAW REO 601R-53-11-1332. (K)Jan 29, 2008 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CHQA200800015Pseu · faultedCMH TO IAH - DURING TAKEOFF, CREW RECEIVED A WOW INPUT AND WOW OUTPUT EICAS MESSAGE. AFTER RUNNING THE APPROPRIATE QRH CHECKLISTS, IT WAS DECIDED TO DIVERT TO SDF WHERE THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE PSEU FOR FAULT CODES WHIJan 28, 2008 · N638BR · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840072Skin · tornPAX DOOR STAIR HAVE APPROX 1.5 IN X 1.5 IN TEAR IN FWD FACE SKIN AT FWD HANDRAIL DOWN STOP BRACKET POINT. REPAIRED IAW REO 601R-52-11-702, REV A. (K)Jan 28, 2008 · N423AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840054Handle · looseSERVICE DOOR HOLD OPEN LATCH HANDLE LOOSE. (K) REMOVED AND REPLACED HOLD OPEN LATCH HANDLE ROLL PINS (2). OPS CHECK GOOD IAW AMM 52-41-00. (S)Jan 27, 2008 · N460AW · Cndair CL6002B19 · Service DoorsSDR A6WA200840055Handle · unsecureON CLIMBOUT AFTER TAKEOFF, APROX 600 MSL, CARGO DOOR MESSAGE ED1 AND CAUTION LIGHT ILLUMINATED. CABIN CLIMBING APPROX 1400 FT PER MIN. C/W QRH. AFTER LANDING NOTED CARGO DOOR HANDLE POPPED. FOUND CARGO DOOR HANDLE EXTENDED UPON ARRIVAL AT GATE. STOWED CARJan 27, 2008 · N452AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200840053Smoke Warning · malfunctionedINFLIGHT DURING BLEED TRANSFER (SMOKE TOILET) CAS MESSAGE APPEARED. COMPLIED WITH QRH. MESSAGE WENT AWAY. FLIGHT ATTENDANT REPORTED ACRID SMELL IN CABIN. (K)Jan 26, 2008 · N468AW · Cndair CL6002B19 · Smoke DetectionSDR A6WA200840071Support · crackedAC EXTERNAL POWER CONNECTOR BOX SUPPORT MEMBER BTW FS 193.00 - 202.00 RT SIDE IS CRACKED AT TOP FWD AND LWR AFT ATTACHMENT POINTS. TOP FWD AND LWR AFT CRACKS IN SUPPORT MEMBER TEMPORARILY REPAIRED IAW REO 601R-24-41-002 PERMANENT REPAIR TO BE CARRIED OUT AT NJan 26, 2008 · N403AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840070Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED AT FS 621.00 AT LINTEL FITTING AREA. AFT PRESSURE BULKHEAD AT FS 621.00 AT LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230 REV D. (K)Jan 25, 2008 · N403AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200840052Hydraulic System · leakingIB CREW REPORTED HYD NR 2 LEAK ON SHORT FINAL. HYD NR 2 CAUTION MESSAGE RECEIVED. HYD QUANTITY NO READS 25 PERCENT. (K)Jan 24, 2008 · N426AW · Cndair CL6002B19 · Hydraulic System, MainSDR CHQA200800012Proximity Switch · malfunctionedCMH TO IAH - AFTER A NORMAL TAKEOFF ON THE APU'S 10TH STAGE BLEED, THE BLEED SOURCE WAS TRANSFERRED OVER TO THE ENGINE'S 10TH STAGE BLEED. THE CABIN PRESSURE HELD FOR APPROXIMATELY 1 MINUTE THAN BEGAN TO RISE. AFTER LEVELING AT 11,000 FT, THE CABIN ALTITUDE Jan 23, 2008 · N639BR · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR A6WA200840050Door · faultyREQUEST INSPECTION FOR OPERATION OF SERVICE DOOR. (DOOR OPENS ABNORMALLY). (K)Jan 23, 2008 · N440AW · Cndair CL6002B19 · Service DoorsSDR A6WA200840051A/C Pack · malfunctionedRT PACK PRESSURE UNCONTROLLABLE, FOLLOWS ENGINE POWER SETTINGS, FALLS OFF LINE AT HIGH POWER SETTINGS. (K)Jan 23, 2008 · N413AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA20080046Unknown · malfunctionedHIGHER THAN NORMAL BACK PRESSURE NEEDED DURING LANDING WITH YOKE. (K)Jan 23, 2008 · N460AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA200840069Frame · dentedFRAME DENTED OVER LIMITS AT FS 700.00 BTW STR 22L TO STR 23L. FRAME SELECTOR REPLACED AT FS 700.00 BTW STR 22L TO 23L SRM 51-42-06. (K)Jan 23, 2008 · N428AW · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA0801008Oil System · lowCREW REPORTED ON TAXI-OUT AN APU AUTO SHUTDOWN. CREW ELECTED TO RETURN TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE APU PER MEL 49-10-01-1. MAINTENANCE PROPERLY SERVICED THE APU OIL LEVEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE Jan 22, 2008 · N202PS · Cndair CL6002B19 · APU Oil SystemSDR CA080125002Actuator · failed(CAN) THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE ON FINAL AFTER SELECTING FLAP TO 8 DEGREES. AN EMERGENCY WAS DECLARED AND THE AC CONDUCTED A FLAPLESS LANDING WITHOUT FURTHER INCIDENT. THE AC WAS FERRIED. ALL FLAP ACTUATORS WERE REPLACED AND THE AC WAS RELEJan 22, 2008 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR A6WA200840047Flap · failedFLAPS FAILED AT ZERO DEGREES, COMPLIED WITH QRH. FAILED ON APPROACH, OAT -1C. (K)Jan 22, 2008 · N438AW · Cndair CL6002B19 · Trailing Edge Flap Control System
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