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 CA020515006Engine · failed(CAN) A/C 7325 EXPERIENCED UNCOMMANDED IFSD. A/C DIVERTED & LANDED IN FRESNO, CA. 2ND EENT WITH A/C & ENGINE. REFER TO LINK FOR PREVIOUS SER. AFTER 1ST EVENT FUEL CONTROL & FILTERS WERE REPLACED. FUEL CONTROL WENT TO REPAIR CAME BACK AS NFF. ENGINE HAS BEEN OPMay 10, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020515007O-Ring · misinstalled(CAN) AIRCRAFT 7318 REPOSITION FROM WVAC TO PHOENIX LOST OIL PRESSURE. A/C LANDED AT WITCHITA, ON PRELIMINARY INVESTIGATION FOUND OIL LOW. SERVICED WITH 5.5 QUARTS. ON CALL MECHANIC AT THIS POINT CANNOT FIND SOURCE OF LEAK. ALSO WVAC IS SENDING A TEAM ETA FORMay 10, 2002 · Cndair CL6002B19 · Engine Oil PressureSDR SWIA200210829Wire Harness · faultyLEVEL AT 27,000 FEET, AFTER COWL ANTI-ICE WAS TURNED ON AND ASSOCIATED THRUST REDUCTION WAS MADE, THE RIGHT ENGINE N1 FLUCTUATED UNCOMMANDED 89.0 TO 95 PERCENT. ALSO ON DESCENT, WITH THRUST LEVER REDUCTION, RIGHT N1 FROM 81 TO 83 PERCENT. NOTICED SOME N2 FLUMay 8, 2002 · N906SW · Cndair CL6002B19 · Turbine Engine System WiringSDR CA020510015Window · cracked(CAN) NAT 07/2002: ON APPROACH FROM THE PILOT REPORTED THE LEFT SIDE WINDOW CRACKED. MAINTENANCE REPLACED THE LEFT SIDE WINDOW (S/N INSTALLED 01306H2383).May 8, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020524004Engine · overtemp(CAN) ON LANDING LT ENGINE OVERTEMP TO 998 FLASHING (HOT), AT GATE SHUTDOWN. MDC SHOWS ENGINE WENT TO 1165 DEGREES FOR 22 SECONDS. THIS AIRCRAFT JUST HAD LT ENGINE REPLACED ON 5/5/02, THE ORIGINAL ENGINE WAS REMOVED DUE TO COKING PROBLEMS. THE AIRCRAFT AFTEMay 5, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA020502026Window · cracked(CAN) PILOT'S SIDE WINDOW CRACKED IN FLIGHT.Apr 28, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020502022Switch · failed(CAN) DURING FLIGHT AT FL290, THE RT REVERSER UNLOCK MESSAGE APPEARED. AIRCRAFT DIVERTED TO ATLANTA AND LANDED WITHOUT FURTHER INCIDENT. RT THRUST REVERSER DEFERRED PER MEL. LATER R&R RT ENGINE TR STOW SWITCH IAW AMM 78-37-01-400-801. RT THRUST REERSER OPS CHEApr 22, 2002 · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA200210809Switch · out of adjustUPON CLIMBOUT OF SLC, RECEIVED 'PAX DOOR LATCH' CAUTION MESSAGE. FOUND PS2M3 SWITCH HITTING EXTERNAL HANDLE. ADJUSTED PER MM 52-70-04. DOOR CHECKS GOOD.Apr 20, 2002 · N587SW · Cndair CL6002B19 · Door Warning SystemSDR CA020502021Connector · burned(CAN) DEPARTED NORMALLY. CLIMB TO CRUISE ALTITUDE WAS UNEVENTFUL (FL270). AUTOPILOT ENGAGED & CLEARED DIRECT APPROX 20 NM NORTH, STAB CH 1 INOP WHILE STATUS MESSAGE ILLUMINATED. QRH PROCS REQUIRED ATTEMPTED RESET - UNSUCCESSFUL - QRH REQD NO FUTHER ACTION (SApr 18, 2002 · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200210799Switch · out of adjustDURING CLIMBOUT RECEIVED LEFT THRUST REVERSER UNLOCKED MESSAGE. FOLLOWED QRH AND RETURNED TO GSO. ADJUSTED THROTTLE LOCKOUT MICROSWITCH IAW CRJ MM 78-30-00. OPS CHECK GOOD.Apr 17, 2002 · N432SW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA020412001Actuator · failed(CAN) "FLAP FAIL" WHEN FLAPS WERE SELECTED TO 8 DEG DURING APPROACH. EMERGENCY DECLARED AND LANDED. SYSTEM WOULD NOT RESET. FERRIED A/C , R&R'D LT INBD FLAP NR 1 AND 2 ACTUATORS FOR FAILING THEIR TORQUE CHECK. "FLAP FAIL" AT ZERO DEG AT 205 KNOTS ON DESCENApr 9, 2002 · Cndair CL6002B19 · Leading Edge Slat ActuatorSDR CA020412002Control Panel · failed(CAN) CREW REPORTED THAT RUDDER TRIM INPUT (NOSE RIGHT) WAS APPLIED BUT, WHEN TRIM SWITCH WAS RELEASED, THE AIRCRAFT CONTINUED TO YAW PROGRESSIVELY MORE. THE RUDDER TRIM INDICATOR CONFIRMED THAT TRIM WAS STILL BEING APPLIED. THE TRIM SWITCH WAS THEN MOVED TO TApr 9, 2002 · Cndair CL6002B19 · Rudder Tab Control SystemSDR CA020412003Window · cracked(CAN) DURING DESCENT FOR APPROACH, THE LT SIDE WINDOW CRACKED. WINDOW REPLACED AND AIRCRAFT RETURNED IN SERVICE.Apr 9, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020412004Switch · loose(CAN) CAPTAIN'S SIDE POST MAP LIGHT WAS SPARKING WITH AN ASSOCIATED ELECTRICAL FIRE SMELL WHEN LIGHT WAS MANIPULATED. IF LIGHT CASING WAS NOT MOVED, NO NOTED ABNORMALTIES. FOUND SWITCH TO BE LOOSE AND TIGHTENED THE JAM NUT ON THE SWITCH TO RESTORE IT TO NORMApr 9, 2002 · Cndair CL6002B19 · Flight Compartment LightingSDR CA020412005Apu · leaking(CAN) ON CLIMB OUT, SMOKE NOTED IN CABIN. APU FAULT AND APU OIL PRESS CAUTION MESSAGES POSTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO WHERE AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND AN APU EXTERNAL OIL LEAK - EXACT LOCATION NOT KApr 9, 2002 · Cndair CL6002B19 · APU Oil SystemSDR CA020412006Windshield · cracked(CAN) DURING CRUISE CAPTAIN'S FRONT WINDSCREEN PLY CRACKED. EMERGENCY DESCENT AND LANDING MADE AT NEAREST AIRPORT AFTER CAPTAIN'S WINDSCREEN PLY SHATTERED DURING CRUISE. AIRCRAFT MADE SAFE LANDING. WINDSCREEN REPLACED.Apr 9, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020412007Windshield · cracked(CAN) CREW REPORTED THE LT WINDSHIELD SHATTERED AT THE GATE. THE LT WINDSHIELD WAS REMOVED AND REPLACED.Apr 9, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020412008Control Unit · failed(CAN) "AFTER T/O MACH TRIM & STAB TRIM CAUTION MESSAGES ILLUMINATED. DECLARED EMERGENCY AND LANDED. "PERFORMED OPS CHECK. NO DEFECTS FOUND. RESET PER FIM AND OPS CHECKED GOOD. RETURNED TO SERVICE. 2ND FLT "AFTER T/O MACH TRIM & STAB TRIM CAUTION MSGS ILLUMApr 9, 2002 · Cndair CL6002B19 · Stabilizer Position IndicatingSDR CA020412009Connector · damaged(CAN) APU BATTERY CHARGER CONNECTOR P12PA BURNED. REPLACED CONNECTOR PINS, CHARGER AND BATTERY. ALL TESTS SATISFACTORY.Apr 9, 2002 · Cndair CL6002B19 · Battery/Charger SystemSDR CA020408015Windshield · failed(CAN) ENROUTE AT 33,000 FEET, THE LEFT WINDSHIELD SHATTERED. FLIGHT DIVERTED TO JFK.WINDSHIELD REPLACED AND AIRCRAFT RETURNED IN SERVICE.Apr 8, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020412010Skin · cracked(CAN) CRACKS FOUND ON THE WIND LOWER CENTRE WING PLANK ACCESS HOLE 540FB, BETWEEN WS 127.25 AND 148.19 ACCESS PANEL.Apr 4, 2002 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA020412011Floor Support · cracked(CAN) CRACK FOUND AT LONGITUDINAL FLOOR SUPPORT LT AND RT BL9.Apr 4, 2002 · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA020531003Brace · unsecure(CAN) A/C LEVELED OFF AT FL290. CREW ATTEMPTED TO THROTTLE BACK & NOTICED LT POWER LEVER JAMMED AT 95.1 PERCENT N1. QRH / INFLT SHUT-DOWN PERFORMED ON LT ENGINE & A/C DIVERTED. ALL ENGINE PARAMETERS INDICATED NORMAL AT ITS PRESENT POWER SETTING PRIOR TO SHUT-Apr 1, 2002 · Cndair CL6002B19 · Power LeverSDR 02088658Engine · malfunctionedDURING CLIMB OF THE FLIGHT FROM IAD TO ALB, THE CREW NOTED THAT THE LT ENGINE VIBRATION INDICATOR WAS READING IN THE YELLOW ARC. THE CREW COMPLIED WITH THE QRH, SHUT DOWN THE LT ENGINE, AND RETURNED TO IAD. MAINTENANCE PERSONNEL INSPECTED THE SPINNER, FAN BLMar 29, 2002 · N658BR · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR WVE2002F00006Engine · lack of lubePILOT REPORTED INFLIGHT NR1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE DURING FLIGHT AFTER C1/C2 INSPECTION. DECLARED IFE AND DIVERTED. UPON INSPECTION BY MAINTENANCE, THE NR1 ENGINE REQUIRED FIVE QUARTS OF OIL. CAUSE AND CORRECTIVE ACTION REMAINS UNDER INMar 26, 2002 · N27318 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200210748Pcu · malfunctionedRECEIVED SPOILERON FAULT STATUS MESSAGE. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU WITH SERVICEABLE UNIT IAW MM 27-62-01. OPS CHECK GOOD.Mar 21, 2002 · N426SW · Cndair CL6002B19 · Drag Control SystemSDR CA020322015Strut · cracked(CAN) DURING INSPECTION, MAINTENANCE FOUND LT MAIN LANDING GEAR CRACKED. MAIN LANDING GEAR REMOVED AND REPLACED.Mar 20, 2002 · Cndair CL6002B19 · Main Landing Gear Strut/Axle/TruckSDR CA020322016Line · ruptured(CAN) OXYGEN LINE AT OBSERVER MASK RUPTURED. MAINTENANCE REPLACED LINE AND SERVICED THE O2 SYSTEM. LEAK CHECK CARRIED OUT.Mar 20, 2002 · Cndair CL6002B19 · Crew Oxygen SystemSDR CA020322012Control Unit · failed(CAN) WHILE AT THE GATE, STAB TRIM PERFORMED UNCOMMANDED FULL NOSE UP TO FULL NOSE DOWN MOVEMENT. 'STAB CH 2 INOP' STATUS MESSAGE APPEARED. DISCONNECTED STAB TRIM. STAB TRIM RE-ENGAGED SEVERAL TIMES ON ITS OWN. INSTALLED SERVICEABLE HSTCU. OPS CHECKS OF STAB/YMar 18, 2002 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA020322014Window · cracked(CAN) CLIMBING THROUGH FL240 THE RIGHT COCKPIT SIDE WINDOW CRACKED. SIDE WINDOW REPLACED AND AIRCRAFT RETURNED TO SERVICE.Mar 18, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020322013Apu · failed(CAN) FLIGHT CAREW REPORTED SMOKE AND OIL SMELL IN COCKPIT AND CABIN. EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE STARTED APU ON GROUND AND UPON TRANSFER OF BLEEDS TO APU, SMOKE FILLED THE CABIN AND COCKPIT. ALSO, APU OIL PREMar 18, 2002 · Cndair CL6002B19 · APU Oil SystemSDR CA020315002Windshield · cracked(CAN) RT WINDSHIELD CENTRE PLY CRACKED DURING CLIMB. THE WINDSHIELD INSTALLED WAS A POST SERVICE BULLETIN WINDSHIELD. RT WINDSHIELD HAS BEEN REPLACED AND AIRCRFT RETURNED TO SERVICE.Mar 12, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020311004Duct · damaged(CAN) IN FLT A/C DEPRESSURIZED AT FL 300. CABIN ALTITUDE CLIMBED TO 14,000 FEET. EICAS MESSAGE AUTO PRESS 2 FAIL(S) POSTED. A/C LANDED UNEVENTFULLY. A/C THEN FERRY LYS FOR TROUBLESHOOTING. MDC INDICATON SHOWED CABIN PRESS CONTOLLER NR 2 AT FAULT. CPC 2 REPLACEMar 11, 2002 · Cndair CL6002B19 · Air Distribution SystemSDR CA020306002Handle · failed(CAN) IN CRUISE, LOUD NOISE COMING FROM NOSE AREA AND MESSAGES (GEAR DISAGREE(W) AND NOSE DOOR (W) POSTED. MESSAGE CLEARED BY THEMSELVES AFTER SEVERAL SECONDS. AIRCRAFT DID AN AIR TURN BACK WHERE IT LANDED SAFELY. AIRCRAFT WAS FERRIED FOR TROUBLESHOOTING. GEARMar 4, 2002 · Cndair CL6002B19 · Landing Gear SelectorSDR CA020301003Window · cracked(CAN) DURING CRUISE, COPILOT WINDOW INNER PLY SHATTERED. AIRCRAFT LANDED SAFELY. NEW WINDOW INSTALLED P/N NP-139322-6 AND S/N 01138H8148.Mar 1, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020304002Engine · leaking(CAN) DEPARTURE FROM SAN ANTONIO, TEXAS DURING CRUISE PHASE OF FLT NR 2 ENGINE EXHIBITED OIL TEMP OF 185C & PRESSURE OF 27 PSI. CREW C/W WITH AFM PROCEEDURES & SHUTDOWN ENGINE. CREW DECLARED EMERGENCY & LANDED IN EL PASO, TEXAS. MESA SENT 2 MECHANICS TO INVESTMar 1, 2002 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200210683Potentiometer · malfunctionedAPU AUTO SHUTDOWN ON THE INITIATION OF TAKEOFF ROLL. ABORTED TAKEOFF AND TAXIED AIRCRAFT BACK TO THE GATE. FOUND APU DOOR POTENTIOMETER BAD. INSTALLED NEW POTENTIOMETER IAW 49-14-01. RIGGED DOOR AND RAN APU. ALL CHECKS OK AT THIS TIME.Feb 28, 2002 · N913SW · Cndair CL6002B19 · APU Start/Ignition SystemSDR CA020228015Windshield · cracked(CAN) THE WINDSHIELD INSTALLED WAS A POST SERVICE BULLETIN WINDSHIELD. RT WINDSHIELD CORE PLY CRACKED IN CRUISE AT FL 350. FLIGHT DIVERTEDREMOVED AND REPLACED WINSHIELD. AIRCRAFT RETURNED TO SERVICE.Feb 28, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200210695Door · unlatchedAFTER TAKEOFF THE CREW HEARD A "POP" AND THE AVIONICS BAY DOOR WARNING LIGHT ILLUMINATED. RETURNED TO BOI. FOUND AVIONICS DOOR LATCH NOT SECURED. INSPECTED AND LATCHED AVIONICS BAY DOOR. NO DEFECTS FOUND.Feb 25, 2002 · N907SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR CA020228014Circuit Card · failed(CAN) AFTER EXCEEDING 250 KTS IAS, RUDDER FLUTTERED UNTIL AIRCRAFT WAS IN LANDING CONFIGURATION. REMOVED AND REPLACED LEFT (UPPER) LHP-4000 CARD IAW AIRCRAFT MM 22-12-01. OPS CHECKED GOOD ON GROUND.Feb 22, 2002 · Cndair CL6002B19 · Rudder Control SystemSDR CA020221016Windshield · cracked(CAN) CLIMBING THROUGH 28,000 FEET AT ABOUT 290 KNOTS LEFT FRONT WINDSHIELD SHATTERED. DECLARED AN EMERGENCY AND DIVERTED TO KNOXVILLE.Feb 20, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020221011Windshield · cracked(CAN) CREW REPORTED THE RIGHT WINDSHIELD CRACKED WHILE ON DESCENT. RIGHT WINDSHIELD REMOVED AND REPLACED IAW CRJ AMM 56-11-01. THE WIDNSHIELD WAS PRE-SERVICE BULLETIN.AIRCRAFT RETURNED TO SERVICE.Feb 19, 2002 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA020221014Nut · loose(CAN) ON APPROACH NOSE DOOR OPEN AT 250 KTS WITH NO INPUT TO GEAR HANDLE. NOSE GEAR SOUNDED LIKE IT CYCLED AND GEAR DISAGREE MESSAGE. ABORTED APPROACH. MANUAL EXTENSION PERFORMED. EMERGENCY DECLARED AND LANDED.DUPLICATED PROBLEM IN HANGAR ON JACKS.NLG DOOR WOUFeb 19, 2002 · Cndair CL6002B19 · Landing Gear SelectorSDR CA020221008Bolt · worn(CAN) DURING DESCENT, THE FLIGHT CREW WERE UNABLE TO RETARD THE NR 1 THROTTLE LEVER. THE ENGINE WAS SHUTDOWN THROUGH THE GLARE SHIELD'S FIRE PUSH BUTTON. EMERGENCY LANDING WAS DECLARED. MAINTENANCE STAFF VERIFIED THE BOLT SECURING THE "THROTTLE CONTROL LEVER Feb 15, 2002 · Cndair CL6002B19 · Power LeverSDR SWIA200210649Circuit Board · faultyAFTER EXCEEDING 250 KTS IAS, RUDDER FLUTTERED UNTIL AIRCRAFT WAS IN LANDING CONFIGURATION. REMOVED AND REPLACED LEFT (UPPER) LHP-4000 CARD IAW A/C MM 22-12-01. OPS CHECKED GOOD ON GROUND.Feb 14, 2002 · N439SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA200210663Blade · bentWHILE INFLIGHT AT 35,000 FT FELT A THUMP, FOLLOWED BY A SLIGHT VIBRATION. ALL INDICATIONS NORMAL AND WITHIN PARAMETERS. ON DESCENT INTO SLC RIGHT NR 2 ENGINE VIBRATION INDICATION GRADUALLY INCREASED UP TO 2.5 BUT STILL WITHIN GREEN BAND ON GAUGE. ALL OTHER Feb 14, 2002 · N590SW · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR CA020221006Circuit Board · failed(CAN) "ON FINAL TO TXK A/C WAS ALMOST UNCONTROLLABLE. YAW DAMPER THREW A/C IN A LT BANK & THEN A RT BANK WITH AUTOPILOT OFF. IT SETTLED DOWN ENOUGH TO GET A/C ON GROUND."MAINT SIGN OFF AS FOLLOWS: PERFORMED FCC DIAGNOSTICS T/S IAW CRJ MM. NO DEFECTS NOTED. PFeb 14, 2002 · Cndair CL6002B19 · Autopilot SystemSDR CA020221005Engine · failed(CAN) AIRCRAFT WAS CLIMBING THROUGH 21K, ENGINE VIBE WENT TO 2.6, THEN ENGINE SHUT DOWN UNCOMMANDED. FLIGHT ATTENDANT REPORTED HEARING A "BANG" IN THE CABIN. ON THE GROUND, OIL WAS NOTED ON THE COWLINGS AND IN THE TAIL PIPE.PREPARATIONS BEING MADE FOR A CREW TFeb 13, 2002 · Cndair CL6002B19 · Engine Emergency Shutdown SystemSDR CA020226009Windshield · failed(CAN) ENROUTE TO KINGSTON, JAMAICA, FROM TORONTO, A CRACK OCCURRED IN THE FACEPLY OF THE CO-PILOT'S WINDSCREEN. ON DESCENT INTO KINGSTON, THE PLY BEGAN TO DELAMINATE. APPROXIMATELY 2/3'S OF THE FACE PLY DEPARTED THE AIRCRAFT PRIOR TO TOUCHDOWN IN JAMAICA.Feb 13, 2002 · Cndair CL604 · Flight Compartment WindowsSDR CA020215003Windshield · cracked(CAN) RIGHT WINDSHIELD FOUND CRACKED ON THE GROUND. WINDSHIELD REMOVED AND REPLACED.THE WINDSHIELD INSTALLED WAS A PRE SERVICE BULLETIN WINDSHIELD.Feb 12, 2002 · Cndair CL6002B19 · Flight Compartment Windows
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