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 VNAA0408001Door · failedTHE CREW REPORTED RECEIVING A RIGHT HAND EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL MEL'D THE EMERGENCY DOOR IN ACCORDANCE WITH MEL 52-70-3 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.Aug 2, 2004 · N220PS · Cndair CL6002B19 · Emergency ExitsSDR VNAA0407010Warning Light · illuminatedDURING DESCENT, THE CREW RECEIVED A LEFT HAND EMERGENCY EXIT DOOR AMBER CAS MESSAGE WHICH EXTINGUISHED AT 8,000 FEET. MAINTENANCE THEN MEL'D THE EXIT DOOR IN ACCORDANCE WITH 52-70-03 CODE-C.Jul 31, 2004 · N256PS · Cndair CL6002B19 · Emergency ExitsSDR CA040802001Skin · lightning strike(CAN) THE FLIGHT CERW REPORTED A POSSIBLE LIGHTINING STRIKE , UPON INSPECTION BY MAINTENANCE IT WAS FOUND THAT THERE WAS DAMAGE TO NR 2 DME ANTENNA , NR 2 COMM ANTENNA AND NR 1 AND 2 ATC ANTENNES WHICH WERE REPLACED AND TESTED . ALSO FOUND STRUCTURAL DAMAGE ONJul 30, 2004 · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR VNAA0408005Structure · vibrationAT 28,000, THE CREW FELT A MODERATE VIBRATION AND SLOWED TO 290 AND THE VIBRATION LESSENED. AFTER SELECTING THE FLAPS TO 20, THE VIBRATION INCREASED THEN LESSENED AGAIN. THE MODERATE VIBRATION CONTINUED UNTIL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT IN AJul 29, 2004 · N253PS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA04531Clip · crackedDURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAWJul 27, 2004 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA040728002Control Unit · failed(CAN) DISPLAY BLANK. REPAIRED UNIT, INSTALLED F/T, OK (RADIO TUNING UNIT).Jul 27, 2004 · Cndair CL604 · Communications SystemSDR CA040811001Windshield · cracked(CAN) CAPTAINS WINDSHIELD SHATTERED, OCCURRED AT FL330, CREW DESCENDED TO FL100, W/S HEAT ON LOW, MFG P: 7.2 WHEN WINDOW SHATTERED. WINDSHIELD REPLACED. (SEE ALSO: US NR 2004081200104)Jul 27, 2004 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA040811003Nose Cowl · damaged(CAN) PILOT REPORTED LOUD NOISE AND SOME LOSS OF ENGINE POWER ON THE RT ENGINE AT CRUISE. UPON LANDING, THE TOWER INFORMED THE AIRCRAFT THAT A COWLING FELL OFF AT LANDING. ENGINE LOWER NOSE COWLING PANEL WAS RECOVERED.MTC LOOKED AT THE AIRCRAFT AND FOUND THE Jul 25, 2004 · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR ASOA04524Step · crackedFLT 4310 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AND BOWING. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Jul 23, 2004 · N840AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA040803010Frame · crackedDURING INSPECTION AS PER AD CF-2003-12, MAINTENANCE FOUND CRACKS IN THE LT AND RT FRAME AND REINFORCING ANGLE AT STATION FS 640 BETWEEN STRINGER 9 AND STRINGER 12. REPAIR WORK IS CURRENTLY IN PROGRESS, AND SDR WILL BE UPDATED UPON COMPLETION OF REPAIR. AIRCRJul 23, 2004 · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA0408004Trim System · out of adjustDURING TAKEOFF, THE CREW RECEIVED AN AILERON TRIM AND A CONFIG TRIM WARNING INDICATION AND ABORTED TAKEOFF. ALL TRIM INDICATIONS WERE NORMAL AFTER THE ABORTED TAKEOFF. HOWEVER, THE CREW ADJUSTED THE AILERON TRIM DUE TO BEING CLOSE TO THE ALLOWABLE TOLERANCE.Jul 22, 2004 · N229PS · Cndair CL6002B19 · Elevator Tab Control SystemSDR CA040818002Computer · inoperative(CAN) DURING APPROACH AT 2500 FEET, THE STICK SHAKER AND STICK PUSHER WERE ENGAGED SIMULTANEOUSLY, FOLLOWING BY THE DE-CONNECTION OF THE AUTOPILOT. THIS INDUCED A LITTLE VARIATION OF THE AIRCRAFT NOSE DOWN. THE FIRST OFFICER IMMEDIATELY COMPENSATED THIS VARIAJul 21, 2004 · Cndair CL6002B19 · Stall Warning SystemSDR VNAA0407005Fire Loop · failedTHE CREW REPORTED THAT THE LEFT HAND ENGINE FIRE LOOP-A WAS INOP. MAINTENANCE CONTROL DEFERRED THE LEFT HAND FIRE LOOP-A WITH THE CREW PER MEL 26-11-01 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.Jul 20, 2004 · N202PS · Cndair CL6002B19 · Fire DetectionSDR CA040728001Charger · failed(CAN) MAIN BATTERY CHARGER FAILED, NO FAULT CODES, REPAIRED UNIT, INSTALLED F/T OK.Jul 19, 2004 · Cndair CL604 · Battery/Charger SystemSDR ASOA04518Clip · crackedDURNG A C-CHECK IN MCN, THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625, NEAR STRINGERS 14 L/R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625, NEAR STRINGERS 14 Jul 18, 2004 · N915EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0407003Fire Loop · failedTHE CREW REPORTED RECEIVING A LEFT HAND JET OVERHEAT FAIL INTERMITTENTLY. MAINTENANCE INSPECTED AND FOUND THAT WITH THE LOOP-B SELECTED, THE INDICATION EXTINGUISHES AND WITH LOOP-A, SELECTED, THE INDICATION STAYS ON. MAINTENANCE CONTROL THEN DEFERRED LOOP-A Jul 16, 2004 · N245PS · Cndair CL6002B19 · Fire DetectionSDR ASOA04496Handle · bindingDURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. THE DOOR LATCH AND HANDLE WERE VERY STIFF. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE AND THE LOWER BEARING ASSEMBLY P/N MS21151-8. OPERATIONAL CHECKS GOOD. AIRJul 10, 2004 · N835AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA04505Computer · malfunctionedFLT 4124 - DURING CLIMB-OUT FROM TRI-ATL, THE CREW NOTICED A LARGE FUEL DISPARITY BETWEEN THE PEFORMANCE INITIALIZATION PAGE AND THE TOTAL FUEL ON THE EICAS AND OVER THE FOLLOWING TEN MINUTES THE FUEL QUANTITY DROPPED 2,000 LBS. AN EMERGENCY WAS DECLARED AND Jul 5, 2004 · N820AS · Cndair CL6002B19 · Fuel Controlling SystemSDR ASOA04482Step · crackedDURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Jul 4, 2004 · N862AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA04481Control Unit · intermittentDURING DESCENT, THE CREW RECEIVED A 14 TH STAGE DUCT MESSAGE. THE QRH WAS COMPLIED WITH AND THE THRUST LEVER WAS REDUCED TO IDLE AT WHICH TIME THE MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACJul 2, 2004 · N903EV · Cndair CL6002B19 · Pneumatic Distribution SystemSDR ASOA04479Light · odorDURING CRUISE, THE CREW NOTICED A HOT PLASTIC TYPE SMELL FROM THE LAVATORY AREA. UPON INVESTIGATION THE CREW DETERMINED THE LAVATORY OCCUPIED LIGHT WOULD NOT EXTINGUISH WHICH WAS CAUSING THE SMELL. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE LAVATJul 1, 2004 · N925EV · Cndair CL6002B19 · Passenger Compartment LightingSDR ASOA04480Intercostal · crackedDURING (C) CHECK, THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL 27 IAW EO 600-53-0098.Jul 1, 2004 · N885AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04478Trim Panel · stuckDURING TAKEOFF, AT APPROXIMATELY 800 FEET THE STAB TRIM AND MACH TRIM DISENGAGED AND THE CREW RE-ENGAGED THEM. WHILE CLIMBING THROUGH 14,00 FEET WITH THE AUTOPILOT ON, STAB TRIM AND MACH TRIM MESSAGES APPEARED AND THEY DISENGAGED AGAIN. THE QRH WAS COMPLIED Jul 1, 2004 · N901EV · Cndair CL6002B19 · Stabilizer Position IndicatingSDR ASOA04473Step · brokenDURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN ON THE FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.Jun 30, 2004 · N848AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA04471Handle · crackedDURING (C) CHECK, THE AVIONICS BAY DOOR HANDLE CUP AROUND THE SUPPORT SHAFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS BAY DOOR HANDLE ASSEMBLY.Jun 29, 2004 · N844AS · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR ASOA04469Handle · crackedDURING (C) CHECK, THE AVIONICS DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS DOOR HANDLE ASSEMBLY.Jun 29, 2004 · N885AS · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR ASOA04465Seat Track · corrodedDURING A (C) CHECK, THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS559 + 32 TO FS 559 + 80 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS 559 +80.Jun 29, 2004 · N844AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA04468Coalescer Bag · dirtyFOLLOWING CLIMB OUT, UPON LEVELING OFF AT APPROX 31,000 FEET, CREW BEGAN NOTICING A SMELL, JET A FUMES COMING THROUGH THE VENTS IN THE COCKPIT ONLY. AFTER DESCENDING TO 24,000 FEET, CREW ATTEMPTED TO ISOLATE THE SMELL BY SHUTTING DOWN THE LT PACK BUT THE SMELJun 29, 2004 · N884AS · Cndair CL6002B19 · Humidity Control SystemSDR ASOA04466Clip · crackedDURING A (C) CHECK, THE RT IB CLIP AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT IB CLIP AT FS 280.Jun 29, 2004 · N885AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04464Clip · crackedDURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 IAW ASA EO 600-53-0098. (M)Jun 29, 2004 · N844AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0460475Support Beam · crackedLT LOWER ENGINE SUPPORT BEAM IS CRACKED. C/W REO 601R-53-61-366.Jun 29, 2004 · N479CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR ASOA04463Step · crackedDURING A C-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW SRM 51-73-00.Jun 28, 2004 · N844AS · Cndair CL6002B19 · Entrance StairsSDR SWIA200413511Floorbeam · crackedFUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED O/B LOCATION FS 280.00 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11.Jun 22, 2004 · N906SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200413512Intercostal · crackedFS 484 RIGHT INTERCOSTAL RBL 27 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11.Jun 22, 2004 · N906SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA04445Clip · crackedDURING A C-CHECK IN MCN, THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625. (M)Jun 20, 2004 · N883AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413453Actuator · malfunctionedSTAB TRIM CH 1 DISENGAGED IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR AND MOTOR CONTROL UNIT, IAW CRJ MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD.Jun 19, 2004 · N915SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413471Indicator · contaminatedRECEIVED IAS EI MACH TRIM CAUTION MESSAGE ON DESCENT. DRAINED WATER FROM MACH SYSTEM NR 1. RESET CIRCUIT BREAKERS. OPERATIONAL CHECK OK.Jun 18, 2004 · N432SW · Cndair CL6002B19 · Speed-Attitude Correction SystemSDR SWIA200413475Handle · dirtyGALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED DOOR HANDLE SHAFT OF DEBRIS AND LUBRICATED AS NEEDED. OPERATIONAL CHECK GOOD.Jun 18, 2004 · N956SW · Cndair CL6002B19 · Service DoorsSDR SWIA200413473Lens · missingMISSING RED LENS ON AFT EMERGENCY EXIT SIGN OF ROW 8. INSTALLED NEW RED LENS ON AFT EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD.Jun 17, 2004 · N964SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200413477Control Unit · malfunctionedSTAB TRIM CHANNEL 1 INOP STATUS MESSAGE DISPLAYED. REPLACED HSTA AND MOTOR CONTROL UNIT (MCU). OPERATIONAL CHECK GOOD. P/N: 8396-3, S/N OFF: 1087.Jun 17, 2004 · N955SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413479Control Lever · malfunctionedFLIGHT SPOILER FAULT (AMBER MESS) CAME ON AT SHORT FINAL. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW 27-61-01. OPERATIONAL CHECK GOOD.Jun 16, 2004 · N407SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413462Floorbeam · crackedFS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-41-21, 51-42-06, AND 51-23-00.Jun 15, 2004 · N452SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200413463Intercostal · crackedCRACKED INTERCOSTAL AT STA 484.00 LBL 36. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. A.Jun 15, 2004 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR WVE2004F00021Element · mislocatedAPPROXIMATELY 30 MINUTES AFTER DEPARTURE, THE LT ENGINE TAILCONE OVERHEAT LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN, LIGHT WENT OUT AND AIRCRAFT RETURNED WITHOUT INCIDENT. THE FIRE DETECTION ELEMENT WAS FOUND TO BE CHAFING ON THE ELEMENT COVER. REPOSITIONED ELJun 15, 2004 · N330FX · Cndair CL6002B16 · Overheat DetectionSDR SWIA200413438Wire · brokenWIRES PULLED OUT OF CONNECTOR OF FIRST OFFICER'S STICK SHAKER. REPAIRED CONNECTOR PER AWM 20-17-10. OPERATIONAL CHECK GOOD PER AMM 27-35-01.Jun 13, 2004 · N915SW · Cndair CL6002B19 · Navigation System WiringSDR SWIA200413436Wire · brokenDURING FFOD STALL TEST, STICK SHAKER DID NOT ACTUATE. REPAIRED WIRING TO FIRST OFFICER'S STICK SHAKER IAW MM 27-35-00. OPERATIONAL CHECK GOOD.Jun 12, 2004 · N923SW · Cndair CL6002B19 · Navigation System WiringSDR SWIA200413743Floor Support · corrodedPAX DOOR LOWER THRESHOLD FLOOR SUPPORT ANGLE CORRODED. ( ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED FLOOR SUPPORT ANGLE IAW CRJ 200 SRM CHAP. 51-42-01, 51-42-13, AND 51-42-21.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413798Frame · crackedRT FS 718 BETWEEN STRINGERS 10R AND 12R IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECTION.) SB 601R-53-055, REV-A STRUCTURAL REPAIR AT F.S. 718.00 RT BETWEEN STRINGERS 10 AND 12, PART-E INCORPORATED.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200413799Frame · crackedLT FS 718 BETWEEN STRINGERS 10L AND 12L IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECTION.) SB 601R-53-055 REVISION A, STRUCTURAL REPAIR AT FUSELAGE STATION (FS) 718.00 BETWEEN STRINGERS 10 AND 12, PART B INCORPORATED.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200413433Windshield · crackedCAPTAINS WINDSHIELD CRACKED ON TAXI IN. REMOVED AND REPLACED THE PILOT'S WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. P/N OFF NP-139321-1, S/N OFF 97007H5138.Jun 11, 2004 · N418SW · Cndair CL6002B19 · Flight Compartment Windows
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