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 ASOA05497Cover · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LENS COVER ON THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR. (K)Jun 7, 2005 · N830AS · Cndair CL6002B19 · Emergency LightingSDR CA050617010Windshield · broken(CAN) RT WINDSHIELD INNER PLY BROKE DURING THE APPROACH. WINDSHIELD REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Jun 7, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0506002Tire · failedAFTER LANDING INSPECTION REVEALED NR 3 TIRE THREAD HAD SEPARATED DURING LANDING CAUSING DAMAGE TO RT INBD FLAP AND TO NR 2 ENGINE FAN BLADES. NR 3 WHEEL & TIRE ASSEMBLY WAS REMOVED & REPLACED IAW CRJ200 AMM 32-41-01-000-801 & 32-41-01-400-801. SIX FAN BLADE Jun 6, 2005 · N248PS · Cndair CL6002B19 · TireSDR A6WA200540191Bushing · migratedLT MLG AFT TRUNNION BUSHING MIGRATED .025 INCH. REMOVED BUSHING AND INSTALLED 2ND OVERSIZE BUSHING IAW REO. (K)Jun 5, 2005 · N418AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540192Skin · dentedRUDDER RT SKIN DENTED 2.0 INCHES ABOVE RIB STATION 72.75 AND 14.3750 FORWARD OF TRAILING EDGE. DENT IS 2 INCHES LONG X 1.5 INCHES WIDE AND .020 INCH DEEP. REPAIRED RUDDER RT SKIN IAW EO. (K)Jun 5, 2005 · N418AW · Cndair CL6002B19 · Rudder, Plate/SkinSDR ASOA05489Fitting · bindingDURING A GROUND INSPECTION, UPON CLOSING THE PASSENGER DOOR AN OVERBOARD COOL MESSAGE WAS RECEIVED AND THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FOR THE PURPOSE OF MAINTENAJun 5, 2005 · N829AS · Cndair CL6002B19 · Door Warning SystemSDR ASOA05491Pressure Panel · corrodedDURING A C-CHECK, THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT AND RT OVERWING EXITS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT AJun 5, 2005 · N850AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA05492Frame · corrodedDURING A C-CHECK, THE MAINFRAME AT FS 473.15 AT THE FLOOR LEVEL UNDER THE LT AND RT OVERWING EXITS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE MAINFRAME AT FS 473.15 AT THE FLOOR LEVEL UNDER THE LT AND RT OVERWING EXITS IAW EO. (K)Jun 5, 2005 · N850AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA05493Pressure Panel · corrodedDURING A C-CHECK, THE PRESSURE FLOOR AT FS 424-449.85 LT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR AT FS 424-449.85 LT IAW EO. (K)Jun 5, 2005 · N850AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200540213Intercostal · crackedTHE UNDER FLOOR INTERCOSTAL AT FS 484, RBL 36 IS CRACKED 1 INCH LONG. REPAIRED INTERCOSTAL IAW REO. (K)Jun 5, 2005 · N418AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05487Circuit Card · malfunctionedDURING DESCENT, THE CREW RECEIVED AN AUXILIARY POWER UNIT (APU) OVERTEMP MESSAGE. DURING COMPLIANCE WITH THE QRH, AN APU FIRE WARNING WAS RECEIVED AT WHICH TIME THE CREW DISCHARGED THE APU FIRE BOTTLE FOLLOWED BY ALL INDICATIONS GOING AWAY. AN EMERGENCY WASJun 4, 2005 · N833AS · Cndair CL6002B19 · Overheat DetectionSDR ASOA05487SFire Warning · false activationDURING DESCENT, THE CREW RECEIVED AN AUXILIARY POWER UNIT (APU) OVERTEMP MESSAGE. DURING COMPLIANCE WITH THE QRH, AND APU FIRE WARNING WAS RECEIVED AT WHICH TIME THE CREW DISCHARGED THE APU FIRE BOTTLE FOLLOWED BY ALL INDICATIONS GOING AWAY. AN EMERGENCY WASJun 4, 2005 · N833AS · Cndair CL6002B19 · Fire DetectionSDR ASOA05490Placard · wornDURING A C-CHECK, THE EXTERIOR EXIT PLACARD ON THE PILOTS ESCAPE HATCH WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EXIT PLACARD ON THE PILOTS ESCAPE HATCH. (K)Jun 3, 2005 · N850AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA05495Bulkhead · corrodedDURING C-CHECK, THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)Jun 3, 2005 · N850AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA05496Floorbeam · corrodedDURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)Jun 3, 2005 · N850AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR MASA200500436Engine · overtempASH 6322 PHX - PHX TO GJT ABORTED TAKEOFF DUE TO THE RT ENGINE ITT OVERTEMP. MAINTENANCE REPLACED NR 2 ENGINE.Jun 3, 2005 · N17358 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA05484Clip · crackedDURING A C-CHECK, THE CLIP AT FS 484, LBL 27 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL 27 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL 27 IAW EO. (K)Jun 2, 2005 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05485Intercostal · crackedDURING A C-CHECK, THE FS 484 INTERCOSTAL AT LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 INTERCOSTAL AT LBL 36 IAW EO. (K)Jun 2, 2005 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05486Rib · crackedDURING A C-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K)Jun 2, 2005 · N850AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA05494Angle · crackedDURING C-CHECK, THE ANGLE IB OF LBL 9 AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ANGLE IB OF LBL 9 AT FS 280 IAW EO. (K)Jun 2, 2005 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05478Support Beam · crackedDURING A C-CHECK, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K)Jun 1, 2005 · N850AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR ASOA05479Clip · crackedDURING A C-CHECK, THE CLIP AT FS 625 LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 625 LT. (K)Jun 1, 2005 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05480Doubler · crackedDURING C-CHECK, THE DOUBLERS AT FS 718, STRINGER 10-12 LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE DOUBLERS AT FS 718, STRINGER 10-12 LT AND RT SIDES. (K)Jun 1, 2005 · N850AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05481Housing · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT HOUSING BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. (K)Jun 1, 2005 · N850AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05482Threshold · crackedDURING A C-CHECK, THE CARGO COMPARTMENT THRESHOLD PLATE WAS FOUND TO BE CRACKED AT THE THRESHOLD COVER FORWARD LATCH BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT THRESHOLD PLATE AT FS 562.72 TO FS589.00 IAW EO. (K)Jun 1, 2005 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05483Push-Pull Rod · bindingDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE WHICH WAS ACCOMPANIED BY AN OUTER HANDLE CAUTION MESSAGE. THE AC WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FOR MAINTENANCE REPAIRS TO THE PASSENGER DOOR. THE AC WAS FERRIED AND LANDJun 1, 2005 · N820AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0505017Unknown · unknownTHE CREW ABORTED THE TAKEOFF AFTER RECEIVING A CONFIG TRIM VOICE WARNING AT 80 KTS. AFTER CONFERRING WITH MAINTENANCE CONTROL, THE CREW PUT THE AIRCRAFT INTO PROPER TAKEOFF CONFIGURATION. THE CONFIGURATION WARNING SYSTEM OPS CHECKED GOOD. THE AIRCRAFT THEN May 31, 2005 · N251PS · Cndair CL6002B19 · Flight Control SystemSDR MASA200500421None · noneASH 6087 PHX - ABORTED TAKEOFF DUE TO THE ENGINE 2 OVERTEMP ON TAKEOFF ROLL. WITHIN LIMITS PER MANUALMay 31, 2005 · N17358 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200540188Attach Fitting · crackedUNDERFLOOR INTERCOSTALS HAVE CRACKED ATTACH FLANGES AT FS 484, LBL 36, AND RBL 36. REPAIRED INTERCOSTAL IAW REO. (K)May 30, 2005 · N418AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540189Floorbeam · crackedTHE LT AND RT SIDE UNDERFLOOR SUPPORT ANGLE IS CRACKED 1.0 INCH AT FS 621, LBL 40 AND RBL 40, WL 73. REPAIRED INTERCOSTALS IAW REO. (K)May 30, 2005 · N418AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200540190Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT POWER ASSIST PULLEY BRACKET. REPAIRED AFT DRAG ANGLE IAW REO. (K)May 30, 2005 · N418AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR REX2005F00031Carbon Seal · damaged(REF NR: 05-072) ON DECENT, THE RT ENGINE OIL PRESSURE WARNING ILLUMINATED. THE FLIGHT CREW NOTED THAT THE INDICATED PRESSURE WAS LOW, BUT STILL IN THE GREEN ARC. FLIGHT CREW REVIEWED QRH PROCEDURES FOR A POSSIBLE ENGINE FAILURE. MINUTES LATER THE OIL PRESMay 30, 2005 · N8940E · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0505015Control Unit · failedTHE AIRCRAFT VEERED HARD LEFT AND THE CREW ABORTED THE TAKEOFF. MAINTENANCE REMOVED & REPLACED THE RT & LT NLG STEERING FEEDBACK RVDTS IAW CRJ 200 AMM 32-51-20-400-801. OPERATIONAL CHECKS AND HIGH SPEED TAXI CHECK CONFIRMED THE SYSTEM SERVICEABLE. THE AIRCRMay 29, 2005 · N245PS · Cndair CL6002B19 · Landing Gear Steering SystemSDR A6WA200540187Intercostal · crackedRT SIDE FS 621- 625.3 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROXIMATELY 1.2 INCH LONG. REMOVED AND REPLACED RT SIDE FS 621- FS625.3 INTERCOSTAL AT STR 14R IAW SRM. (K)May 28, 2005 · N418AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05468Wire · brokenDURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE AND THE GREEN ALIGNMENT MARKS WERE NOT ALIGNED. MAINTENANCE INSPECTED THE AC AND FOUND IT SAFE FOR A FERRY FLIGHT FOR PERFORMANCE OF THE APPROPRIATE C/A. MAINT FOUND THE INNER HANDMay 28, 2005 · N820AS · Cndair CL6002B19 · Door System WiringSDR ASOA05469Step · brokenDURNG A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP RETRACTING HINGE LINKAGE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)May 28, 2005 · N824AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540186Intercostal · crackedLT SIDE FS 621-625.3 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROXIMATELY 0.9 INCH LONG. REMOVED AND REPLACED LT SIDE FS621-625.3 INTERCOSTAL AT STR 14L IAW SRM. (K)May 28, 2005 · N418AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA050603001Filter · contaminated(CAN) DURING TAKEOFF ROLL, RT FUEL FILTER CAUTION MESSAGE. AFTER RUN UP, IT OCCURRED AGAIN. EARLIER SAME DAY, LT FUEL FILTER CAUTION MESSAGE POSTED. MAINT REPLACED LT ENG FUEL FILTER PRESSURE SWITCH AND FUEL FILTER. RT ENG FILTER WAS ALSO REPLACED AND SENT FMay 28, 2005 · Cndair CL6002B19 · Aircraft Fuel Filter/StrainerSDR REX2005F00032Control System · failed(REF NR: 05071) FLAPS FAIL AT 11 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)May 28, 2005 · N8409N · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00034Control System · failed(REF NR: 05-069) FLAPS FAILED AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K)May 28, 2005 · N8942A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA05466Frame · crackedDURING HANGAR MAINTENANCE, THE LT FRAME STA 640 WAS FOUND TO BE CRACKED AFT OF LBL 10 BEYOND LIMITS. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR A FERRY FLIGHT FOR PERFORMANCE OF THE APPROPRIATE CORRECTIVE ACTION. THE AIRCRAFT LANDED SAFELY. MAINTENMay 27, 2005 · N851AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA05467Handle · bindingDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN AND THE SLOW HANDLE PUSHING OUT. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE AND INTERNAL MECHANISM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)May 27, 2005 · N820AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0505014Access Door · openDURING CLIMB THE STALL FAIL WARNING MESSAGE ILLUMINATED. THE CREW RETURNED TO CLT. MAINTENANCE INTERROGATED THE MDC AND FOUND NO FAULT CODES. THE STALL WARNING SYSTEM OPERATIONALLY CHECKED GOOD. THE OXYGEN SERVICING DOOR WAS FOUND OPEN ON THE RIGHT SIDE OFMay 27, 2005 · N245PS · Cndair CL6002B19 · DoorsSDR REX2005F00033Windshield · cracked(REF NR: 05-070) CAPTAINS WINDSHIELD CRACKED. REMOVED AND REPLACED CAPTAINS LT FRONT WINDSHIELD IAW AMM. (K)May 27, 2005 · N8891A · Cndair CL6002B19 · Flight Compartment WindowsSDR CA050601003Housing · broken(CAN) ON ARRIVAL, GROUND CREW WAS UNABLE TO OPEN CARGO DOOR. INVESTIGATION BY MAINTENANCE FOUND CENTER PART OF THE DOOR HANDLE ASSY HOUSING WHERE THE SHAFT PASSES THROUGH WAS COMPLETELY BROKEN AWAY. CRJ 200 IPC REF 52-31-00 FIG.2 ITEM 20A. CARGO DOOR HANDLE AMay 26, 2005 · Cndair CL6002B19 · Cargo/Baggage DoorsSDR CA050528001Windshield · cracked(CAN) RT WINDSHIELD CRACKED WHILE IN CRUISE. THE WINDSHIELD IS POST SB.May 26, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR REX2005F00035Control System · failed(REF NR: 05-068) FLAP FAIL. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD98-20-01. (K)May 26, 2005 · N8524A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VTZA200500090Engine · shutdownRT ENG SHUTDOWN ON TAKEOFF ROLL AT ROTATION.May 25, 2005 · N625BR · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0505012Trim System · unknownSTABILIZER TRIM FAILED IN FLIGHT AND THE MACH TRIM DISENGAGED. MAINTENANCE OPERATIONALLY CHECKED THE STAB TRIM SYSTEM IAW BOMBARDIER RJ-SL-00-001. THE SYSTEM CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.May 25, 2005 · N242JS · Cndair CL6002B19 · Stabilizer Position IndicatingSDR A6WA200540184Bushing · migratedLT MLG AFT TRUNNION FITTING BUSHING IS MIGRATED .055 INCH OUT OF BORE. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZE BUSHING, IAW MFG REO. (K)May 25, 2005 · N456ZW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
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