GE CF34-3B1

Service difficulty reports · 5,402

Newest first. General aviation reporting is voluntary.

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 CA010501005Windshield · failed(CAN) FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT, NO CABIN PRESSURIZATION LOSS.WINDSHIELD REPLACED.Apr 12, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA972504Anti-Ice System · malfunctionedAFTER TAKEOFF RIGHT STATIC HEAT, RIGHT PITOT HEAT, TAT PROBE HEAT AND RIGHT AOA HEAT WARNINGS ILLUMINATED. RETURNED TO SLC. RESET HEAT SYSTEM FOR RIGHT PITOT STATIC, TAT PROBES, AND AOA SYSTEM. OPS CHECK GOOD.Apr 11, 2001 · N418SW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR ASOA01035Engine · failedFLT 4742 - DURING FLIGHT FROM AUS TO ATL, CREW RECEIVED A NR 2 ENGINE 'LOW OIL PRESSURE' LIGHT. CREW SHUT DOWN RIGHT ENGINE FOLLOWING QRH AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED TO JAN AND LANDED SAFELY. MAINTENANCE PERFORMED MAGNETIC CHIP DETECTOR INSApr 11, 2001 · N843AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA972526Window · crackedON LANDING THE RIGHT SIDE WINDOW CRACKED. REMOVED AND REPLACED RIGHT SIDE SIDE WINDOW IAW 56-12-01; RII 56-401. OPS CHECK GOOD. P/N ON PPG-NP-139322-6, S/N ON 00320H3690, S/N OFF 92016H6381.Apr 10, 2001 · N405SW · Cndair CL6002B19 · Flight Compartment WindowsSDR MASA01036Scavenge Pump · defectiveFLT 6009 - PHX-DSM - DIVERTED TO ABQ AFTER CAPTAIN PERFORMED AN INFLIGHT SHUT DOWN OF THE NR 2 ENGINE. THE OIL PRESSURE WENT DOWN TO 15 PSI AND THE OIL TEMP INCREASED 26 DEG CELSIUS TO 144 DEG CELSIUS. INCREASING POWER AND RETARDING POWER TO IDLE HAD NO AFFEApr 10, 2001 · N37178 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA010430024Handle · jammed(CAN) WHILE AT THE GATE, AFTER BOARDING, THE FLIGHT ATTENDANT REPORTED THAT SHE WAS UNABLE TO CLOSE THE PASSENGER DOOR. THE FLIGHT ATTENDANT REPORTED THAT THE HANDLE WOULD JAM HALF WAY WHEN CLOSING.THE AIRCRAFT WAS BROUGHT TO THE HANGAR AND MAINTENANCE WERE UNApr 7, 2001 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA010430025Windshield · failed(CAN) FIRST OFFICERS WINDSHIELD SHATTERED. CABIN DIFFERENTIAL PRESSURE 7.3. NO PRESSURE LOSS. REPLACED WINDSHIELD.Apr 7, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA972516Anti-Ice System · malfunctionedRIGHT AOA VANE CAUTION MESSAGE CAME ON IN FLIGHT. RETURNED TO SLC. CYCLED POWER. RAN 20 MINUTES. RIGHT AOA HEAT OPS CHECK GOOD.Apr 6, 2001 · N409SW · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR SWIA972517Actuator · malfunctionedAUTOPILOT PITCH TRIM MESSAGE ILLUMINATED WHILE DESCENDING TO FL 270. AFTER FOLLOWING QRH PROCEDURE MESSAGE EXTINGUISHED. RETURNED TO SLC. AUTOPILOT PITCH TRIM SYSTEM OPS CHECKS GOOD. REPLACED THE STABILIZER TRIM ACTUATOR AND MOTOR CONTROL UNIT.Apr 6, 2001 · N413SW · Cndair CL6002B19 · Stabilizer ActuatorSDR CA010430022Lock · out of adj(CAN) FLIGHT ATTENDANT REPORTED THAT SHE WAS UNABLE TO CLOSE AND LOCK THE PASSENGER DOOR. MAINTENANCE FOUND THE SECONDARY LOCK PAWL TO BE FOULING AGAINST THE TORQUE TUBE, TORQUE TUBE AND SECONDARY LOCK PAWL OUT OF ADJUSTMENT. THEY DID A PASSENGER DOOR ADJUSTMEApr 6, 2001 · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA972485Windshield · crackedFIRST OFFICER''S WINDSHIELD SHATTERED INFLIGHT AT FL250. INSIDE LAYER DID NOT DELAMINATE. NO CABIN PRESSURE LOSS. REMOVED AND REPLACED COPILOT''S WINDSHIELD IAW MM 56-11-01, CHECKS GOOD. P/N: NP-139321-10, S/N ON: 0107343239, S/N OFF: 0013047097.Apr 5, 2001 · N418SW · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010410030Windshield · cracked(CAN) THE RT WINDSHIELD INNER PLY CRACKED WHILE THE AIRCRAFT WAS IN DESCENT. THE WINDSHIELD WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Apr 3, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010410025Windshield · cracked(CAN) THE RT WINDSHIELD MIDDLE PLY WAS FOUND CARACKED AIRCRAFT ON PARKING. THE AIRCRAFT DID A FERRY FLIGHT TO MORLAIX. THE WINDSHIELD WAS REPLACED AT THE MAINTENANCE BASE AS PER AMM 56-11-01.Apr 2, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010410027Rod · failed(CAN) IN PITT DURING TURN AROUND, FLT ATTENDANT & CREW WERE UNABLE TO CLOSE MAIN PASSENGER DOOR. AFTER MULTIPLE ATTEMPTS CREW WERE ABLE TO CLOSE DOOR BUT WERE UNABLE TO RE-OPEN FROM INSIDE. NORTHWEST AIRLINK MAINT, ENGINEERING & BOMBARDIER FSR WERE SENT TO PApr 2, 2001 · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA972472Windshield · crackedFIRST OFFICER''''S WINDSHIELD SHATTERED. CABIN DIFFERENTIAL PRESSURE ON 7.3, NO PRESSURE LOSS. REMOVED AND REPLACED WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01. C/W PRESSURIZATION CHECK. LEAK CHECK GOOD. P/N: NP139321-6, S/N ON: 00083H3538, S/N OFMar 31, 2001 · N426SW · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010410023Windshield · cracked(CAN) ON DESCENT INTO WICHITA THE LT WINDSHIELD CRACKED. AIRCRAFT WAS FERRIED TO MEMPHIS AND THE WINDSHIELD WAS REPLACED.Mar 30, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010511002Fuel Control · failed(CAN) CREW REPORTED THAT THEY HAD 3 UNCOMMANDED OVERSPEEDS OF RIGHT ENGINE N1 DURING FLT. 1ST 104.5 PERCENT N1 FOR 5.7 SEC ICAS N1 ICON TURNED RED. PILOT PULLED THROTTLE BACK & ENGINE DID NOT COME BACK FOR 3 TO 4 SEC. PILOT ADVANCED THROTTLE BACK TO CRUISE POWMar 30, 2001 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA010410014Windshield · failed(CAN) ENROUTE ATLANTA TO COLUMBIA SC, FIRST OFFICERS WINDSHIELD SHATTERED. CREW LANDED UNEVENTFULLY IN COLUMBIA.THE DAMAGE TO THE WINDSHIELD IS ON THE INNER SURFACE AND GLASS FRAGMENTS WERE FOUND ON THE GLARESHIELD BY MAINTENANCE. WINDSHIELD WAS REPLACED AND TMar 24, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR AU010264Fuel Control · leaking(AUS) RT ENGINE FUEL CONTROL UNIT LEAKING FROM THE AREA OF THE THROTTLE CONTROL INPUT ARM.Mar 23, 2001 · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR CA010410006Computer · failed(CAN) STALL FAIL MESSAGE AFTER GEAR UP. MAINTENANCE CARRY LRU DIAGNOSTICS AND OPERATIONAL CHECK, NO FAULT FOUND AT THIS TIME AND AIRCRAFT BACK IN SERVICE.Mar 22, 2001 · Cndair CL6002B19 · Stall Warning SystemSDR CA010410008Window · failed(CAN) DURING CRUISE SIDE WINDOW SHATTERED, CREW DIVERTED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED SIDE WINDOW.Mar 22, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010410010Windshield · failed(CAN) AFTER LANDING CREW REPORT LT WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED WINDSHIELD AND AIRCRAFT BACK IN SERVICE.Mar 22, 2001 · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR CA010403007Panel · cracked(CAN) LT WING PLANK CRACKED AT WS 148.019 FOR ABOUT 1.2 INCHES LONG. THE RT HAS NO CRACK. THEY WILL PERFORM THE REO 601R-57-21-130.Mar 14, 2001 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA010403004Windshield · cracked(CAN) PILOT REPORT LT WINDSHIELD INNER PLY BOTTOM LOWER CORNER CRACKED. WINDSHIELD REMOVED AND REPLACED.Mar 13, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR AU010188Windshield · cracked(AUS) CAPTAINS SIDE WINDOW OUTER PANE SHATTERED.Mar 11, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010320010Windshield · cracked(CAN) RT WINDSHIELD INNER PLY FOUND CRACKED, UNIT REPLACED AND AIRCRAFT BACK IN SERVICE.Mar 8, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010320014Adc · failed(CAN) DURING CRUISE STABILIZER TRIM CH2 AND MACH TRIM FAILED. MAINTENANCE REPLACED ADC AND AIRCRAFT BACK IN SERVICE.Mar 8, 2001 · Cndair CL6002B19 · Air Data ComputerSDR CA010706015Line · leaking(CAN) PILOT REPORT: HYDRAULIC SYSTEM NR 2 LOW PRESSURE MESSAGE DURING CRUISE. FOUND HYDRAULIC SYSTEM NR 2 EMPTY OF FLUID. MAINTENANCE FINDING: FOUND FITTING OF FILL LINE LEAKING (REF IPC 29-11-00-5-270). FOUND FITTING ADAPTER WRONG INSTALLED ON FILL LINE. INSTMar 5, 2001 · Cndair CL6002B19 · Hydraulic System, MainSDR CA010307033Sensor · out of adj(CAN) DURING CLIMB CREW RECD PASSENGER ENTRANCE DOOR WARNING MESSAGE PAX DR LATCH (AMBER) & PASSENGER DOOR (WARNING) EICAS MESSAGES. A/C RETURNED TO DEPTR AIRPORT&LANDED W/O INCID.&LATER FERRIED TO MAINT BA SE. MAINT FINDINGS: 1. PSEU FAULT LOG 2 RECORDED S47 Feb 22, 2001 · Cndair CL6002B19 · Door Warning SystemSDR CA010307018Brace · sheared(CAN) AIRCRAFT 604-54F05 WITH TSN OF 611.3 HOURS AND 304 CYCLES HAS BEEN FOUND TO HAVE A BROKEN TRUNNION PIN AT L/H MLG SIDE BRACE ACTUATOR INBOARD END.THIS WAS FOUND AS THE AIRCRAFT WAS ON JACKS AND A TECHNICIAN NOTICED THAT THE GEAR MOVED. THE FORWARD ATTACHFeb 20, 2001 · Cndair CL6002B16 · Landing Gear Door ActuatorSDR CA010307021Windshield · cracked(CAN) DURING THE PRE-FLIGHT INSPECTION, IT WAS NOTICED THAT THE CAPTAINS WINDSHIELD WAS CRACKED. THE AIRCRAFT RETURNED TO SERVICE AFTER REPLACEMENT OF THE WINDSHIELD.Feb 19, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010307024Engine · failed(CAN) PILOT REPORT IN DESCENT: AUDIT ENGINE OIL AND MASTER WARNING. ENGINE NR 2 OIL PRESSURE RAPIDLY DROPPED TO 0 PSI. CREW INITATED AN IN-FLIGHT SHUTDOWN PROCEDURE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PARTICLE ON NR 2 CHIP DETECTOR. AT THE TIMFeb 19, 2001 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA010307028Window · cracked(CAN) WHILE MANOEUVRING ON THE GROUND, THE LT SIDE WINDOW WAS FOUND CRACKED. THE WINDOW WAS REPLACED AND THE AIRCRAFT RETURNED INTO SERVICE.Feb 19, 2001 · Cndair CL6002B19 · Window/Windshield SystemSDR MASA01019Engine · failedFLT 6197 - PHX-SBA - THE PILOT NOTICED ZERO OIL PRESSURE INDICATION ON NR 2 ENGINE. THE ENGINE WAS SECURED IAW THE CFM. THE PILOT DECLARED AN EMERGENCY. THE AIRCRAFT LANDED UNEVENTFUL AT SBA. MAINTENANCE WAS INVESTIGATING IF INDEED THE NR 2 ENGINE WENT WITFeb 16, 2001 · N37178 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA972357Windshield · crackedON PREFLIGHT INSPECTION, NOTICED CAPTAINS SIDE WINDSHIELD CRACKED REPLACED CAPTAINS WINDSCREEN IAW 56-11-04. P/N ON NP-139321-5, S/N ON 9927H9235, S/N OFF 00133H7393.Feb 13, 2001 · N905SW · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010213027Panel · cracked(CAN) WHILE JACKING AIRCRAFT, MAINTENANCE FOUND TWO CRACKS ON AFT SECTION OF LOWER WING PLANK. ONE ON THE LT AND ONE ON THE RT SIDE, AT WS 148, NEAR THE WING JACKING POINTS. REPAIR ACTIVE, AIRCRAFT WILL RETURN INTO SERVICE SOON.Feb 13, 2001 · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA972344Damper · failedUNABLE TO ENGAGE YAW DAMPER NUMBER TWO PRIOR TO FLIGHT. POWERED AIRCRAFT DOWN AND BACK UP. CYCLED YAW DAMPER SEVERAL TIMES. BOTH YAW DAMPER ONE AND TWO OPS CHECK GOOD.Feb 9, 2001 · N905SW · Cndair CL6002B19 · Speed-Attitude Correction SystemSDR CA010226008Windshield · failed(CAN) THE RT WINDSHIELD SHATTERED IN CRUISE DURING THE FLIGHT NR 5.THE MAINTENANCE REPLACED THE WINDSHIELD.Feb 6, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010226009Windshield · failed(CAN) THE LT WINDSHIELD SHATTERED IN CRUISE AT 35,000 DURING THE FLIGHT NR 5.THE MAINTENANCE REPLACED THE WINDSHIELD.Feb 6, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010501021Windshield · failed(CAN) CLIMBING THROUGH 31,000 FEET - 7 MACH, 8.2 P.S.I. LT WINDSHIELD SHATTERED.Feb 5, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA972331Shutoff Valve · failedLEFT 10TH SOV FAILED TO OPEN. RECEIVED STATUS MESSAGE L 10TH ARMED OPEN. RETURNED TO DEN. POWERED DOWN AIRCRAFT AND RE-POWERED. OPS CHECK GOOD.Feb 4, 2001 · N905SW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR CA010226005Apu · leaking(CAN) THE CREW REPORTED THE SMOKE TOILET CAUTION MESSAGE AT 9000 FEET. SMOKE WAS VISIBLE WHEN BLEED WAS TRANSFERRED IN CABIN AND COCKPIT WHEN BLEEDS WERE TRANSFERRED TO APU. AIRCRAFT DID AN EMERGENCY LANDING.THE MAINTENANCE FOUND OIL COMING FROM COMPRESSOR DRAFeb 3, 2001 · Cndair CL6002B19 · APU Oil SystemSDR CA010214004Structure · cracked(CAN) DURING A ROUTINE E3 (1200 HOURS) INSPECTION WHEN REMOVING THE PASSENGER DOOR SIDE PANELS A CRACK WAS FOUND IN THE PASSENGER DOOR LATCH BOX ASSEMBLY 601R31765-3/03. THE AIRCRAFT REMAINED GROUNDED UNTIL A NEW LATCH BOX WAS INSTALLED. FOLLOWING THE REPLACEMFeb 1, 2001 · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA010213028Bolt · sheared(CAN) MAINTENANCE FOUND THE L/H EXHAUST NOZZLE CRACKED DURING A CHECK INSPECTION. DURING REPLACEMENT OF THE EXHAUST NOZZLE, MAINTENANCE FOUND TWO (OUT OF THREE) DELTA BRACKETS ATTACH BOLTS SHEARED, AT 2 AND 10 OCLOCK POSITION.FAULTY PARTS REPLACED PER AMM.Jan 30, 2001 · Cndair CL6002B19 · Engine Exhaust SystemSDR CA010213032Windshield · cracked(CAN) DURING CUSTOMER ACCEPTANCE FLIGHT, IN CRUISE, L/H WINDSHIELD CRACKED. L/H WINDSHIELD REMOVED AND REPLACED.Jan 29, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010213018Actuator · broken(CAN) ON APPROACH, AT LAST FLP SELECTION, A/C ROLLED TO THE RIGHT FOLLOWED BY FLT SPLR DEPLOY CAUTION MESSAGE.CREW DECLARED EMERGENCY AND LANDED WITHOUT ANY FURTHER EVENT. MAINTENANCE FOUND FLIGHT SPOILER PANEL ACTUATOR LUG BROKEN. PANEL REPLACED. AIRCRAFT RETJan 25, 2001 · Cndair CL6002B19 · Drag Control SystemSDR CA010213023Windshield · cracked(CAN) IN CRUISE FLIGHT, F/O WINDSHIELD SHATTERED. NO INFO ON ALTITUDE OR IF EMERGENCY WAS DECLARED. AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT.Jan 25, 2001 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA010213020Actuator · failed(CAN) DURING TAKEOFF ROLL, CONFIG TRIM AND CONFIG STAB WARNINGS APPEARED. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS.HSTA AND MCU REPLACED. AIRCRAFT RETURNED TO SERVICE.Jan 24, 2001 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA010213021Stabilizer · failed(CAN) ON CLIMBOUT, STAB AND MACH TRIM DISENGAGED AT 8.2 UNITS AT NOSE UP TRIM. WOULD NOT RE-ENGAGE. AIRCRAFT PERFORMED A FLAP 20 DEGREES PER QRH WITHOUT ANY FURTHER EVENT. MAINTENANCE REPLACED THE HORIZONTAL STAB TRIM PANEL AND RETURNED AIRCRAFT TO SERVICE.Jan 24, 2001 · Cndair CL6002B19 · Stabilizer Control SystemSDR CA010213024Windshield · cracked(CAN) DURING TAXI, CAPTAIN WINDSHIELD CRACKED.AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT.Jan 17, 2001 · Cndair CL6002B19 · Flight Compartment Windows
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