GE CF34-3A1

Service difficulty reports · 1,372

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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 = 'CF343A1'
  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 SWIA971503Overheat Message · malfunctionRIGHT 14TH STAGE DUCT OVERHEAT MESSAGE EN ROUTE. QUICK REFERENCE HANDBOOK PERFORMED AND MESSAGE PERSISTS. SINGLE ENGINE PROCEDURE PERFORMED AND DUCT MESSAGE PERSISTS. LEFT BECAME INTERMITTENT JUST PRIOR TO LANDING. FIRE CREWS REPORTED NO SIGN OF FIRE. REMJun 1, 1999 · N410SW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR COMA9960209Oil System · req'd serviceCVG - FLT 9600 - RIGHT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 35 PSI AND 55 PSI. SERVICED OIL TANK TO PROPER LEVEL. (X)May 17, 1999 · N965CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA990514013Fcu · failed(CAN) LIGHTNING STRIKE ON RIGHT WING AREA. LOSS OF N2 ON RIGHT ENGINE FOR 45 SECONDS. HEAVY RAIN. NO FAULTS FOUND BY GROUND CREW. FCU REPLACED, PRECAUTIONARY.May 13, 1999 · Cndair CL6002B19 · Fuel Controlling SystemSDR SWIA971481Rvdt · failedNOSE WHEEL STEERING INOP MESSAGE CAME ON IN FLIGHT. RETURNED TO SLC. REMOVED AND REPLACED RIGHT RVDT AT NOSE GEAR, OPS CHECK GOOD.May 3, 1999 · N409SW · Cndair CL6002B19 · Landing Gear Steering SystemSDR SWIA971465Heat Message · activatedRIGHT AOA HEAT MESSAGE CAME ON AFTER TAKEOFF. RETURNED TO SLC. POWERED SYSTEM DOWN AND BACK UP. OPS CHECK GOOD. COULDN'T DUPLICATE PROBLEM.Apr 9, 1999 · N405SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA971473Window · crackedLEFT SIDE WINDOW CRACKED IN FLIGHT. DIVERTED FROM ABQ TO FMN. NO LOSS OF PRESSURIZATION OR OTHER DIFFICULTIES ENCOUNTERED. REMOVED AND REPLACED LEFT SIDE WINDOW IAW MM 56-12-01. OPS CHECKS GOOD.Apr 8, 1999 · N403SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA971470Computer · trippedSTALL FAIL MESSAGE ILLUMINATED EN ROUTE. RETURNED TO SLC. RESET MEMORY ON STALL COMPUTER. OPS CHECKS GOOD.Apr 6, 1999 · N411SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA971466Bracket · damagedNOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. NOSE GEAR DOORS OPEN AND NOSE GEAR LIGHT REMAINED GREEN. FOUND BRACKET FOR NOSE GEAR TARGET WAS DAMAGED. REPLACED BRACKET AND SET GAP PER MM 32-64-05. OPS CHECK SHOWS ALL INDICATIONS NORMAL.Apr 1, 1999 · N403SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA971446Computer · malfunctionedSTALL FAIL MESSAGE ON RIGHT AFTER TAKEOFF. RETURNED TO SLC. INSTALLED SERVICEABLE STALL WARNING COMPUTER. OPS CHECK GOOD IAW 27-34-00.Mar 30, 1999 · N411SW · Cndair CL6002B19 · Stall Warning SystemSDR JBXA9900077Sensor · failedFLIGHT 853 MYR TO RDU, 15 MINS FROM RDU HAD LEFT 14TH DUCT FAIL MESSAGE ON EICAS. PERFORMED PRECAUTIONARY SHUTDOWN NR 1 ENG ACCORDING TO OPERATIONAL PROCEDURES. REMOVED AND REPLACED LEFT HAND STUB WING DUCT LEAK SENSOR LOOP. OPS CHECK GOOD AT THIS TIME IAW Mar 23, 1999 · N578ML · Cndair CL6002B19 · Pneumatic Indicating SystemSDR CA990330067Windshield · shattered(CAN) IN CLIMB THROUGH 10,000 FEET THE FIRST OFFICER'S WINDSHIELD SHATTERED.Mar 13, 1999 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA990330071Strut · damaged(CAN) ON TAKEOFF DURING GEAR RETRACTION, A GEAR DISAGREE ANNUNCIATION. MAIN GEAR UP, BUT NOSE GEAR DOWN. GEAR SELECTED TO DOWN AND AIRCRAFT RETURNED. THE NOSE GEAR OLEO FLOATING PISTON WAS NOT FULLY BOTTOMED.Mar 12, 1999 · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR CA990330072Psu · deployed(CAN) TWO PASSENGER OXYGEN UNITS OPENED IN-FLIGHT AND DROPPED ON PASSENGER SEAT 8D/F.Mar 12, 1999 · Cndair CL6002B19 · Passenger Oxygen SystemSDR CA990330066Bpsu · failed(CAN) AFTER LANDING FLAPS LOCKED OUT ON RETRACTION, RIGHT HAND BRAKE POSTION SENSING UNIT AND FLAP ELECTRONIC CONTROL UNIT RESET. RIGHT HAND OUTBOARD FLAPS RERIGGED.Mar 9, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA990330076Bpsu · failed(CAN) FLAP FAIL AT 45 DEGREES AND ONCE AT 41 DEGREES. RIGHT BPSU REPLACED AND RE-RIGGED.Mar 9, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971429Skin · dirtyAIRCRAFT NEEDS LEFT AILERON TRIM WHEN FLAPS SET TO 45 DEGREES. DISCOVERED LEADING EDGE OF FLAP HAD RIDGE OF PAINT BUILD-UP FROM RECENT AIRCRAFT RE-PAINTING. RE-SURFACED LEADING EDGE OF FLAP IAW SERVICE LETTER RJ-SL-27-022 DATED 8/28/96.Mar 9, 1999 · N406SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA971445Pseu · malfunctionedPROXIMITY SYSTEM FAULT STATUS MESSAGE. PERFORMED MANUAL EXTENSION OF LANDING GEAR. RETURNED TO SLC. REMOVED AND REPLACED PSEU. PERFORMED SELF TEST. ALL WORK DONE IAW 32-61-01.Mar 9, 1999 · N413SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA990330077Valve · failed(CAN) GEAR SELECTED UP, UNSAFE INDICATION. VIBRATION. RETURNED TO TORONTO. NOSE GEAR SELECTOR VALVE, DOOR SELECTOR VALVE REPLACED.Mar 8, 1999 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR CA990330065Pdu · failed(CAN) FLAP FAIL MESSAGE IN-FLIGHT WITH ZERO FLAP SELECTED. DURING APPROACH, FLAPS DID NOT EXTEND. FLAP POWER DRIVE UNIT CHANGED.Mar 5, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA990330064Sensor · failed(CAN) IN CLIMB, STALL CAUTION MESSAGE AFTER 8 DEGREE FLAP. FIRST OFFICER STALL TAPE CAME UP TO 160 KNOTS. QUICK REF HANDBOOK CARRIED OUT. FIRST OFFICER TAPE 190 KNOTS AT FLAP ZERO DEGREE, 145 KNOTS AT FLAP 45 DEGREE. CHANGED LEFT HAND ANGLE OF ATTACK SENSOMar 2, 1999 · Cndair CL6002B19 · Stall Warning SystemSDR SWIA971422Mechanism · out of adjustPASSENGER DOOR LATCH RED MESSAGE CAME ON INFLIGHT. RETURNED TO OMA, ADJUSTED ROD END TO ROD THAT ROTATES UPPER TWO CAMS IAW MM 52-11-02. OPS CHECKS GOOD.Feb 22, 1999 · N416SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA990308027Sensor · out of adjust(CAN) SHORTLY AFTER TAKEOFF, STEERING INOP AND LANDING GEAR DISAGREE MESSAGES ON WITH NOSE LANDING GEAR STILL DOWN. NOSE LANDING GEAR PROXIMITY SENSORS ADJUSTED. ALSO SENSOR P/N PS13GA.Feb 20, 1999 · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA971420Warning · illuminatedCLIMBING THROUGH 16,000 AN EICAS MESSAGE PAX DOOR LATCH WAS OBSERVED. FOLLOWED QRH AND AT 22,000 AN EICAS RED MESSAGE PAX DOOR CAME ON. FOLLOWED QRH AND DIVERTED TO IDA. CHECKED AIRCRAFT PSEU AND FOUND IN MEMORY S46 FAR IN MEMORY. HAD SLC MAINTENANCE FAX TFeb 20, 1999 · N416SW · Cndair CL6002B19 · Door Warning SystemSDR CA990308029Visor Panel · missing(CAN) ON TRIP CHECK FOUND THE RIGHT HAND VISOR PANEL ON THE STABILIZER MISSING. THIS IS A 2 INCH BY 4 INCH FAIRING. IT IS THE LOWER LEFT ONE.Feb 17, 1999 · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR MASA99025Engine · vibrationPHX/DSM - FLT 6009 - APPROXIMATELY TEN MINUTES AFTER DEPARTURE FROM PHX, THE CREW REPORTED THE NR 2 ENGINE VIBRATION INDICATOR TURNED YELLOW AT 2.7 PERCENT. CREW DECLARED AN EMERGENCY DUE TO THE FACT THE AIRCRAFT WAS OVERWEIGHT. THE AIRCRAFT RETURNED TO THE FIFeb 15, 1999 · N77286 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA990308031Latch · out of adjust(CAN) AFTER TAKEOFF THROUGH 4,000 FEET, PASSENGER DOOR LATCH CAUTION MESSAGE, FOLLOWED BY PASSENGER DOOR WARNING MESSAGE. CABIN PRESSURE AT 2.3. AIRCRAFT RETURNED. DOOR LATCH CAM SPIGOTS ADJUSTED TO LOWER LIMIT, INNER HANDLE FRICTION TENSION ADJUSTED, AND PUFeb 13, 1999 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA990308036Sensor · failed(CAN) PASSENGER DOOR LIGHT AND CAUTION MESSAGE IN FLIGHT THROUGH 10,500 FEET FLOWED 5 SECONDS LATER BY PASSENGER DOOR WARNING MESSAGE. AIRCRAFT DEPRESSURIZED AND LANDED OK. PROXIMITY SWITCH ELECTRONIC UNIT INTERROGATED SHOWING SENSORS OUT OF RIG. SENSOR HFeb 8, 1999 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA990308037Actuator · failed(CAN) FLAPS FAIL MESSAGE ON APPROACH, AS FLAPS TRAVELLING FROM 8 DEGREES TO 20 DEGREES, STUCK AT 15 DEGREES. LANDING OK. RIGHT HAND OUTBOARD FLAP, INBOARD ACTUATOR REPLACED.Feb 8, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA971412Window · failedRIGHT SIDE WINDOW SHATTERED IN FLIGHT. NO APPARENT CONTACT OR LOSS OF PRESSURE. NORMAL LANDING IN FAT. REMOVED AND REPLACED RIGHT SIDE COCKPIT WINDOW IAW MM 56-12-01.Feb 6, 1999 · N412SW · Cndair CL6002B19 · Flight Compartment WindowsSDR CA990129023Seal · ruptured(CAN) ON FINAL,THE NR 2 ENGINE OIL PRESSURE SHOWED ON THE ECAIS. FOLLOWING THE CHECK LIST, THE NR 2 ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION FOUND A RUPTURED RING MATING SEAL ON THE AXIS BETWEEN THE IDG AND THE ACCESSORY GEARBOX, WHICH CAUSED THE LOSS OF Jan 27, 1999 · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR CA990203022Panel · missing(CAN) DURING WALK-AROUND , FOUND THE LEFT HAND ENGINE EXHAUST PIPE A PANEL MISSING.Jan 20, 1999 · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA9960034Fuel Control · malfunctionNR 1 ENGINE LAGS NR 2 DURING TAKEOFF. REPLACED THE LEFT ENGINE FUEL CONTROL.Jan 15, 1999 · N943CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA990119033Controller · failed(CAN) ON DEPARTURE, AIR TEMP PROBE, RIGHT ANGLE OF ATTACK, RIGHT STATIC HEAT MESSAGES ON EICAS. REPLACED AIR DATA SENSOR CONTROLLER.Jan 11, 1999 · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR CA990119038Valve · malfunctioned(CAN) UNABLE TO PRESSURIZE AFTER TAKEOFF. SUSPECT OVERBOARD COOLING VALVE DID NOT CLOSE. TOTAL CYCLES: 6.668.Jan 11, 1999 · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR SWIA971365Sensor · out of adjustGEAR DISAGREE AND NOSE DOOR DISAGREE RED LIGHTS CAME ON AFTER GEAR HANDLE IS SELECTED UP. GEAR WILL NOT GO UP TO LOCKED POSITION. RETURNED TO SLC. ADJUSTED S23 SENSOR ON NOSE GEAR. GEAR EXTENDS AND RETRACTS NORMALLY, OPS CHECKS GOOD.Jan 9, 1999 · N407SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR CA990119036Flaps · failed(CAN) FLAP FAIL MESSAGE ON APPROACH. SYSTEM RESET. FLAP CHECK CARRIED OUT NORMAL. TOTAL CYCLES: 6,860.Jan 8, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971377Pump · failedNUMBER ONE HYDRAULIC QUANTITY DROPPED TO 35 PERCENT EN ROUTE. RETURNED TO SLC. INSTALLED SERVICEABLE HYDRAULIC PUMP ON LEFT ENGINE IAW MM 29-13-00. OPS AND LEAKS CHECK GOOD.Jan 5, 1999 · N409SW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR CA990115017Panel · missing(CAN) LEFT HAND ENGINE EXHAUST NOZZLE ACCESS PANEL MISSING AT 12 O'CLOCK POSITION. TOTAL CYCLES: 5,926.Dec 31, 1998 · Cndair CL6002B19 · Accessory Compartment DoorsSDR CA990115021Flaps · failed(CAN) AFTER TAKEOFF, FLAP RETRACTION LOCKED AT 8 DEGREES AND FLAP FAIL MESSAGE ON. AIRCRAFT DIVERTED. FLAP RIGGING AND OPERATIONAL CHECK NORMAL. TOTAL CYCLES: 5,487.Dec 31, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971358Wire · chafedLEFT ENGINE JET PIPE OVERHEAT FAILED IN FLIGHT. SHUT ENGINE DOWN. FOUND LEFT ENGINE JET PIPE WIRES CHAFED TO GROUND. REPAIRED AND REPOSITIONED WIRES. TESTED JET PIPE SYSTEM, LEFT SIDE CHECKS GOOD.Dec 31, 1998 · N408SW · Cndair CL6002B19 · Fire DetectionSDR CA990115023Plate · failed(CAN) IN CLIMB THROUGH 17,000 FEET, CAUTION MESSAGE PASSENGER DOOR LATCH FOLLOWED BY AURAL WARNING. QUICK REF CARRIED OUT. EMERGENCY DEPRESSURIZATION INITIATED. AIRCRAFT RETURNED. MAIN CABIN DOOR STRIKER PLATE RE-WORKED. DOOR RIGGING CHECKED. TOTAL CYCLEDec 29, 1998 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA990219017Solenoid · failed(CAN) DURING DOOR WARNING PROBLEM WITH AIRCRAFT ON DESCENT, THE OXYGEN MASKS WERE DEPLOYED. MASKS, ROWS 5 TO 13, FAILED TO DEPLOY. CIRCUIT BREAKER HAD TRIPPED ON THE LEFT SIDE CONTROL WHEN MASKS DID NOT DEPLOY . INVESTIGATION SHOWED THAT ROW 13AB SOLENOID LDec 29, 1998 · Cndair CL6002B19 · Passenger Oxygen SystemSDR CA990111039Windshield · leaking(CAN) DURING TAXI AN ELECTRICAL BURNING SMELL IN COCKPIT. GLYCOL HAD LEAKED THROUGH THE COPILOT'S WINDSHIELD ONTO A FLOOD LIGHT. TOTAL CYCLES: 7,289.Dec 23, 1998 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA971353Yaw Damper · inopYAW DAMPER 1 IS INOP. RETURNED TO FIELD. REMOVED AND REPLACED R1 YAW DAMPENER LINEAR ACTUATOR. REPLACED FLIGHT CONTROL PANEL, OPS CHECK OK FOR CAT II OPERATION.Dec 23, 1998 · N408SW · Cndair CL6002B19 · Autopilot SystemSDR VTZA98369Valve · failedFLT 6665 - SGE-ORD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITHONE DISCREPANCY WHICH WAS RT ENGINE ANTI-ICE FAILED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ANTI-ICE VALVE, OPS CHECK OK. AIDec 20, 1998 · N621BR · Cndair CL6002B16 · Engine Anti-Icing SystemSDR SWIA971339Bpsu · failedFLAPS FAIL MESSAGE AT FL330. RETURNED TO SLC, MADE A NO FLAP LANDING. COMPLIED WITH AD 98-20-01. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10.Dec 15, 1998 · N407SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA981230052Door · out of rig(CAN) DURING CLIMB AT ABOUT 290 KNOTS AND 8,000 FEET, THE CREW RECEIVED A MASTER CAUTION DOOR HANDLE WARNING AND SUBSEQUENTLY A MASTER WARNING FOR PASSENGER DOOR, AND AN AURAL WARNING. DOOR FOUND OUT OF RIG. PART TC: 5,388.Dec 12, 1998 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA981230054Sensor · contaminated(CAN) AT 19,000 FEET, PASSENGER DOOR LATCH CAUTION MESSAGE CAME ON. CABIN PRESSURE NORMAL, 20 SECONDS LATER, THE PASSENGER DOOR RED WARNING CAME ON. IN DESCENT, MESSAGE CYCLED UNTIL PRESSURE WAS ZERO. SWITCHES AND BOTH SENSORS ON DOOR HANDLE WERE CLEANED ANDec 8, 1998 · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA971325Engine · failedDURING TAKEOFF, LEFT ENGINE ITT WAS IN YELLOW RANGE. DURING CLIMB ITT HAD A 877 FT RED EXCURSION FOR ABOUT 2 SEC. ICING CONDITIONS WERE ENCOUNTERED AND ITT WENT RED 888 FT WITH N21 PERCENT HIGHER THAN RIGHT, FUEL FLOWS 90 LBS HIGHER. ABOUT 3 TO 4 SECONDS, LNov 29, 1998 · N406SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA981216023Rod · out of adjust(CAN) PASSENGER DOOR ANNUNCIATION IN-FLIGHT. EMERGENCY DEPRESSURIZATION CARRIED OUT, AIRCRAFT RETURNED. FLAPPER DOOR ROD ADJUSTED. TOTAL CYCLES: 5,318.Nov 28, 1998 · Cndair CL6002B19 · Passenger/Crew Doors
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