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 SWIA200312312Ecu · malfunctionedRT SPOILERS FAULT MESSAGE DURING TAXI OUT. REMOVED AND REPLACED RIGHT SECU. OPS CHECKS GOOD IAW 27-62-01.Aug 20, 2003 · N438SW · Cndair CL6002B19 · Drag Control SystemSDR CA030825017Window · delaminated(CAN) LT SIDE WINDOW WAS FOUND DELAMINATED. THERE IS NO POST OR PRE SB CONFIGURE FOR THE WINDOW.Aug 15, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030930016Tru · failed(CAN) AT CRUISE ALT ADG DEPLOYED, AC1 AUTO TRANSFER MSG DISPLAYED. SMOKE IN COCKPIT. NR 1 TRU FAILED. FOLLOWED QRH. DIVERTED.Aug 13, 2003 · Cndair CL6002B19 · AC Generation SystemSDR 03224706Overheat Loop · unreliableDURING DESCENT CREW RECEIVED A 14TH STAGE WARNING MESSAGE AND SHUT DOWN THE LEFT ENGINE AS A PRECAUTION EMERGENCY WAS DECLARED FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LT ENGINE PYLON 14TH STAGE OVERHEAT DETECTION LOOP. AAug 12, 2003 · N706BR · Cndair CL6002B19 · Overheat DetectionSDR SWIA200312321Attach Angle · crackedFS 280 LT FLOORBEAM ATTACH ANGLE LBL 9 IB AND OB CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R-31113-57Aug 8, 2003 · N417SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA03362Snap Ring · missingFLT 9331 - DURNG APPROACH INTO ATL FROM MCN, THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE. THE OIL PRESSURE WAS AT 25 PSI AND CONTINUED TO DECREASE. THE CREW COMPLIED WITH QRH PROCEDURES AND SHUTDOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLAAug 7, 2003 · N851AS · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR SWIA200312317Handle · crackedPAX DOOR HANDLE IS CRACKED. (DISCOVERED DURING C-CHECK) PAX DOOR HANDLE REMOVED, SANDED, PRIMED, PAINTED AND INSTALLED IAW MM 52-11-03-400-801.Aug 2, 2003 · N912SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200312318Flange · crackedFS 484 RT INTERCOSTAL OB FLANGE RBL 36 CRACKED. (DISCOVERED DURING C-CHECK)INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. ''A''.Aug 2, 2003 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312315Attach Angle · crackedFS 280 O/B LEFT FLOORBEAM ATTACH ANGLE LBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401. P/N: 601R31113-57.Aug 1, 2003 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312316Attach Angle · crackedFS 280 I/B AND O/B RIGHT FLOORBEAM ATTACH ANGLES RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. ANGLED REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-58Aug 1, 2003 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312319Support Angle · crackedFS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. (DISCOVERED DURING C-CHECK) ANGLE REPAIRED IAW CRJ REO 601R5361117 REV. ''A''. REF. RII 53-401.Aug 1, 2003 · N912SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312320Floor Support · crackedFS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. (DISCOVERED DURING C-CHECK) REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV. ''A'', RII 53-401.P/N: 601R-53-61-117-2 & P/N: 601R-53-61-117-4Aug 1, 2003 · N912SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA030807003Cowling · damaged(CAN) CREW WAS NOTIFIED BY TOWER THAT THE LT UPPER ENGINE COWLING HAD COME OFF THE AIRCRAFT, AND WAS LAYING ON THE RUNWAY. A/C RETURNED AND LANDED THEY FOUND THE FASTENER STILL LOCKED ON THEIR DZEUS RECEPATCLE .THEY REPLACED THE DAMAGED DZEUS RECEPTACLE AND REJul 30, 2003 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR 03204634Warning System · false indicationDURING CRUISE THE CREW REPORTED A LOW OIL PRESSURE INDICATION ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED AN OPERATIONAL CHECK OF THE RT ENGINE OIL SYSTEM AND A SATISFACTORY MAINTENANCE ACCEPTJul 23, 2003 · N634BR · Cndair CL6002B19 · Engine Oil PressureSDR SWIA200312200Pcu · malfunctionedON TAXI OUT, GOT ''R SPOILERON'' AND ''SPOILERON FAULT'' MSGS. REMOVED AND REPLACED RIGHT SPOILERON INBOARD PCU IAW 27-62-01. LEAK AND OPS CHECK GOOD.Jul 18, 2003 · N435SW · Cndair CL6002B19 · Drag Control SystemSDR CA030729004Light · burned(CAN) GALLEY LIGHTING FIXTURE OVERHEATED: NO SNAGS FOUND IN REVIEW OF SPRING & SUMMER 2003 AMTAK RECORDS WITH REFERENCE TO GALLEY LIGTHING FIXTURE ISSUES. NO LIGHT FIXTURES PURCHASED OR CONSUMED DURING THE PAST 2 YEARS. LIGHT BULB INSTALLED IN GALLEY LIGHTINJul 16, 2003 · Cndair CL6002B19 · Passenger Compartment LightingSDR 03193698Carbon Seal · leakingDURING CRUISE CREW REPORTED SMOKE IN THE FLIGHT DECK AND CABIN. MAINTENANCE PERSONNEL PERFORMED A BORESCOPE INSPECTION AND FOUND NO DISCREPANCIES, DURING AN EXTERNAL VISUAL INSPECTION OF THE TURBINE SECTION THE NR 1 CARBON SEAL WAS FOUND TO BE LEAKING AND WASJul 12, 2003 · N698BR · Cndair CL6002B19 · Turbine SectionSDR SWIA200312175Bpsu · malfunctionedFLAP FAIL CAUTION MESSAGE APPEARED 20 MIN AFTER DEPARTURE. REMOVED AND REPLACED LT BPSU. RIGGED LEFT AND RIGHT BPSU IAW MM 27-51-10. FOUND FECU POTENTIOMETER OUTSIDE LIMIT. ADJUSTED FECU POTENTIOMETERS. REMOVED AND REPLACED FLAP CONTROL LEVER PER CRJ MM 2Jul 12, 2003 · N445SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200312172Actuator · malfunctionedSTAB CHANNEL 1 INOPERATIVE. CHANGED HSTCA & MCU IAW 27-41-00. P/N 7062-3 S/N OFF 926.Jul 8, 2003 · N905SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200312159Control Unit · malfunctionedINFLIGHT (ANTISKID INBD ANTISKID OUTBOARD) YELLOW MESSAGES ILLUMINATED - QRH COMPLIED WITH - MESSAGES WOULD NOT EXTINGUISH. BOTH LEFT SIDE MAIN LANDING GEAR TIRES FAILED ON LANDING. FOUND LEFT AND RIGHT ANTISKID CB'S POPPED. RESET CB'S AS REQUIRED IAW MM 32Jul 1, 2003 · N426SW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR CA030707006Actuator · failed(CAN) FLIGHT CREW REPORTED ' STAB CHANNEL NR 1 FAIL' MESSAGE DURING CRUISE. RESET OK BUT FAIL MESSAGE AGAIN DURING MANUAL TRIM. TROUBLE SHOOTING DISCOVERED MOTOR ON NR 1 HORIZONTAL STAB TRIMACTUATOR HAD FAILED. TRIM UNIT AND MOTOR CONTROL UNIT WERE ALSO REPLACJul 1, 2003 · Cndair CL6002B19 · Elevator Tab Control SystemSDR CA030713001Circuit Breaker · failed(CAN) WHILE TAXIING THE FIRST OFFICER NOTICED AN ODOUR AND THE CAPTAIN VERIFIED PRESENCE OF SMOKE AT CIRCUIT BREAKER PANEL NR 2. THE SMOKE STOPPED WHEN THE CREW REACHED OVER AND PULLED CIRCUIT BREAKER CBP2-G13. THE PROBLEM WAS FINALLY SOLVED WITH THE REPLACEMJun 29, 2003 · Cndair CL6002B19 · Hydraulic Power System WiringSDR CA030713002Windshield · failed(CAN) CAPTAIN'S WINDSHIELD SHATTERED ON CLIMBOUT (RECEIVED A LT WINDSHIELD HEAT CAUTION ABOUT 15 SECONDS PRIOR TO IT SHATTERING). UNEVENTFULL LANDING PERFORMED. REPLACED LT WINDSHIELD AND HEAT CONTROLLER. AIRCRAFT RETURNED TO SERVICE.CONTROLLER PN 16591, SN Jun 29, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030713003Lever · broken(CAN) REPORTED THAT ON THE PAX DOOR BOTH THE FWD AND AFT SWIVEL LEVERS (601R3197411) HAD FAILED ALLOWING THE DOOR TO FREEFALL. MAINTENANCE FOUND THE SUPPORT WHEEL LEVER BENT AND THE DOOR SKIN DISTORTEDAND WITH INTERNAL STRUCTURAL DAMAGE. REPLACED THE SUPPORT WJun 29, 2003 · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200340104Engine · malfunctionedABORTED TAKEOFF, 140 KNOTS NR 2 ENGINE N2 DROPPED OFF TO APPROX 50-60 PERCENT. ON TAKEOFF ROLL, BRAKE MAX TEMPS WERE 11, 9, 7, 8 ABORTED TAKEOFF, TAKEOFF AT 1655Z MARKED FDR AT 1704Z. PERFORMED ACCELERATION/DECELERATION CHECKS AND POWER ASSURANCE CHECKS, NO Jun 24, 2003 · N443AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR 03173662Wire Harness · installedDURING CRUISE FROM EWR AT 16000 FT THE LT 14TH STAGE DUCT WARNING MESSAGE APPEARED. CREW DECLARED EMERGENCY AND SHUT DOWN LT ENGINE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL SWAPPED 14 STAGE FENWAL DUCT WARNING LOOPS AND PERFORMED A SATJun 22, 2003 · N662BR · Cndair CL6002B19 · Pneumatic Indicating SystemSDR A6WA200340098Engine · malfunctionedNR 2 ENGINE ONLY PRODUCED 50 PERCENT POWER. ABORTED TAKEOFF AT 60 KNOTS. ALMOST NO BREAKING USED, MAX 2 PERFORMED POWER ASSURANCE CHECK IAW AMM 71-00-00-710-804. PERFORMED CHECKS WITHIN LIMITS. COULD NOT DUPLICATE PROBLEM. (M)Jun 16, 2003 · N445AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200312123Floorbeam · crackedFS 280 FLOORBEAM O/B ATTACH ANGLE RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601R31113-58.Jun 16, 2003 · N439SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312124Intercostal · crackedFS 484 LT INTERCOSTAL O/B FLANGE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FLANGE IAW CRJ REO 601R-53-41-059 REV A.Jun 16, 2003 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312125Intercostal · crackedFS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-51.Jun 16, 2003 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312126Intercostal · crackedFS 625 RT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-52.Jun 16, 2003 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312127Floor Support · crackedFS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV A. P/N: 601R-53-6117-3.Jun 16, 2003 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312128Floor Support · crackedFS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117 REV A. P/N: 601R-53-61-117-4.Jun 16, 2003 · N439SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312129Intercostal · crackedFS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52.Jun 15, 2003 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312130Floor Support · crackedFS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. DAMAGED AREA REPAIRED IAW CRJ 601R-53-61-117 REV 'A'. P/N: 601R-53-61-117-3Jun 15, 2003 · N438SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312102Bulb · burned outLEFT REAR AFT EMERGENCY LIGHT (EXTERIOR) INOP. REPLACED BAD BULB ON LEFT REAR AFT EMERGENCY LIGHT OVERWING. OPS CHECK GOOD.Jun 12, 2003 · N916SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200312106Lamp · inoperative1ST OVERHEAD EMERGENCY LIGHT IN CABIN INOP. REMOVED AND REPLACED THE LAMP. OPS CHECK GOOD.Jun 11, 2003 · N431SW · Cndair CL6002B19 · Emergency LightingSDR CA030612008Window · cracked(CAN) CO-PILOT'S WINDOW CRACKED ON APPROACH. WINDOW WAS REPLACED AND AIRCRAFT DECLARED SERVICEABLE.Jun 9, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200312080Cam · out of adjustMAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. PAX DOOR LOCK PAWL STOPPING AGAINST LATCH-CAM TORQUE TUBE. ADJUSTED CONTROL ROD END ON LOCK PAWL IAW MM 52-11-15. OPS CHECKS GOOD AT THIS TIME.Jun 8, 2003 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200312103Coalescer Bag · contaminatedAFTER STARTING THE APU AND BRINGING ON BOTH PACKS, GOT SMOKE INTO THE FLIGHT DECK AND THE CABIN. SMOKE WAS COMING FROM THE AIR CONDITIONING SYSTEM. ALSO GOT A SMOKE CAUTION MESSAGE. REMOVED AND REPLACED BOTH RIGHT AND LEFT ACM WATER SEPARATOR SOCKS WITH SERJun 8, 2003 · N411SW · Cndair CL6002B19 · Humidity Control SystemSDR CA030603012Idg · making metal(CAN) IDG 2 CAUTION MSG POSTED WHILE IN CRUISE. LT ENGINE GENERATOR ALREADY DEFERRED. AIRCRAFT DIVERTED, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MTCE REPLACED IDG NR 2 AND OPS CHECKED SERVICEABLE. LEFT ENGINE GENERATOR REMAINED DEFERRED.Jun 2, 2003 · Cndair CL6002B19 · AC Generator-AlternatorSDR SWIA200312056Windshield · crackedOVER MEM AT FL 410 TEMP -60C DEGREES F/O WINDSHIELD CRACKED. F/O SIDE WINDOW CRACKED AT 11,000. FOLLOWED QRH FOR CRACKED WINDSHIELD AND CONTINUED TO KNOXVILLE. REMOVED AND REPLACED RIGHT WINDSHIELD AND RIGHT SIDE WINDOW IAW CRJ MM 56-11-01. P/N OFF: 601RMay 31, 2003 · N441SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200312046Pin · wornLEFT AND RIGHT OVERWING EXIT HINGE SUPPORT PINS SHOWING SIGNS OF WEAR AND SURFACE CORROSION. REPLACED PINS IAW STANDARD MAINTENANCE PRACTICES. DISCOVERED DURING MAINTENANCE INSPECTION.May 29, 2003 · N407SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA200312047Sign · brokenEMERGENCY EXIT SIGN (FLOODLIGHT) AT SERVICE DOOR BROKEN. REPLACED EMERGENCY EXIT SIGN BY SERVICE DOOR AND REPLACED THE ELECTRICAL CONNECTOR. DISCOVERED DURING MAINTENANCE INSPECTION.May 29, 2003 · N407SW · Cndair CL6002B19 · Emergency LightingSDR CA030603013Dowel Pin · sheared(CAN) PILOT REPORTED THAT WHEN AUTOPILOT WAS DISCONNECTED ON APPROACH ELEVATOR CONTROL WAS VERY HEAVY. PILOT ASKED CO-PILOT TO CONFIRM. BOTH WERE IN AGREEMENT THAT AIRCRAFT WAS VERY HEAVY ON THE PITCH CONTROL. AN UNEVENTFUL LANDING WAS COMPLETED WITH BOTH PILOMay 29, 2003 · Cndair CL6002B19 · Autopilot Main ServoSDR SWIA200312085Floorbeam · crackedFS 280 RBL 9.0 FLOORBEAM I/B AND O/B ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. P/N: 601R31113-58.May 28, 2003 · N910SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312086Intercostal · crackedFS 484 LT INTERCOSTAL O/B FLG CRACKED. DISCOVERED DURING C-CHECK. DAMAGED AREA REPAIRED IAW CRJ REO 601R-53-41-059 REV A. NDT-HFEC CARRIED OUT IAW REO 601R-53-41-059. NO CRACKS NOTED.May 28, 2003 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312088Floor Support · crackedFS 521.0 LBL 36 FLOOR SUPPORT ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE AREA IAW CRJ REO 601R-53-61-117 REV A.May 28, 2003 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312089Floor Support · crackedFS 621.0 RBL 36 FLOOR SUPPORT ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV A.May 28, 2003 · N910SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312007Bulb · inoperativeCENTER STEP BOARDING LIGHT IS INOP. REPLACED LIGHT BULBS IN CENTER STEP BOARDING LIGHT PER MM 33-45-01. OPS CHECK GOOD.May 26, 2003 · N412SW · Cndair CL6002B19 · Emergency Lighting
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