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 A6WA200540268Fitting · looseHORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 6 LOOSE MOUNT BOLTS. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K)Jul 24, 2005 · N405AW · Cndair CL6002B19 · Horizontal Stabilizer, Attach FittingsSDR ASOA05628Clip · crackedDURING A C-CHECK, THE LT IB AND RT OB FS 280 CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT OB AND RT IB FS 280 CLIPS IAW SRM. (K)Jul 24, 2005 · N833AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA05629Pressure Panel · corrodedDURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATIOJul 24, 2005 · N833AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA05630Pressure Panel · corrodedDURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMIT ON THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING AN REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATJul 24, 2005 · N833AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA05631Switch · inoperativeON APPROACH, THE CREW RECEIVED A STEERING INOP CAUTION MESSAGE WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION. THE CREW TRIED TO RESET THE NOSE WHEEL STEERING SWITCH, BUT THE SWITCH WOULD NO RESET. THE QRH WAS FOLLOWED. AN EMERGENCY WAS NOT DECLARED, BUT EJul 24, 2005 · N915EV · Cndair CL6002B19 · Landing Gear Steering SystemSDR ASOA05632Anchor Fitting · crackedDURING HANGAR MAINTENANCE, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE COMPLIED WITH REO, A TEMPORARY REPAIR VALID FOR 100 FLIGHT HOURS FROM DATA OF INCORPORATION. THIS MRR WILL REMAIN OPEN PENDING COMPLETION OF PERMANENT REPAJul 24, 2005 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05629SFloor Panel · corrodedDURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TOO 559 RBL AND 36 AND 45. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45 IAW EO. (K)Jul 24, 2005 · N833AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA05630SFloor Panel · corrodedDURING C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45 IAW EO. (K)Jul 24, 2005 · N833AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA05632SAnchor Fitting · crackedDURING HANGAR MAINTENANCE, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 24, 2005 · N886AS · Cndair CL6002B19 · Entrance StairsSDR ASOA05625Floorbeam · corrodedDURING A C-CHECK, THE FORWARD FLOOR SUPPORT ANGLE FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND CORRODED BEYOND LIMITS. (K)Jul 23, 2005 · N833AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA05626Floorbeam · corrodedDURING A C-CHECK, THE AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CORRODED FLOOR SUPPORT ANGLE IAW EO. (K)Jul 23, 2005 · N833AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA05645Intercostal · crackedDURING C-CHECK, THE INTERCOSTAL AT FS 280, RBL 9 OB OF THE CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTAL AT FS 280, RBL 9 IAW EO. (K)Jul 23, 2005 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05652Skin · crackedDURING A C-CHECK, THE PASSENGER DOOR INNER SKIN AND INTERCOSTAL AT TATUM 1, FS 338 FRAME BETWEEN DATUM 1 AND THE UPPER CLOSE OUT WEB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR INNER SKIN AND INTERCOSTAL AT DATUM 1, FS 338 FJul 23, 2005 · N854AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05614Inverter · malfunctionedDURING A GROUND INSPECTION, THE EMERGENCY LIGHTS FROM ROWS 2 TO 4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER FOR THE EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 22, 2005 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05615Handle · bindingDURING A GROUND INSPECTION, THE FLIGHT ATTENDANT REPAORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE REMOVED, REBUILT, AND REINSTALLED THE PASSENGER DOOR HANDLE ASSY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 22, 2005 · N842AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05619Panel · crackedDURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LT SIDE IAW EO. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA05621Clip · crackedDURING A C-CHECK, THE LT OB AND RT IB FS 280 CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT OB AND RT IB FS 280 CLIPS IAW SRM. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA05622Lens · crackedDURING C-CHECK, THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05623Light · inoperativeDURING A C-CHECK, THE LT AND RT OVERWING EMERGENCY EXIT BETA LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT AND RT OVERWING EMERGENCY EXIT BETA LIGHTS. OPS CHECK GOOD. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05624Door · stiffDURING A C-CHECK, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE INSIDE AND OUTSIDE. MAINTENANCE RE-RIGGED THE PASSENGER DOOR OUTER HANDLE IAW MM. OPS CHECK GOOD. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05620Frame · crackedDURING C-CHECK, THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE IAW EO. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASO2005F00008Doubler · crackedDURING A C-CHECK, THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE IAW EO. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05636Doubler · crackedDURING C-CHECK, THE RT FS 718 DOUBLER AT STRINGER 10-12 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT FS 718 DOUBLER AT STRINGER 10-12 RT IAW EO. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05655Handle · damagedDURING A C-CHECK, THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0507017Cap · missingDURING PREFLIGHT, BEFORE FIRST FLIGHT OF THE DAY, THE CREW DISCOVERED THE SINGLE POINT FUEL CAP MISSING. UPON FURTHER INSPECTION THE RIGHT ENGINE INLET COWL WAS FOUND DAMAGED. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSTALLED A NEWJul 21, 2005 · N261PS · Cndair CL6002B19 · Fuel StorageSDR A6WA200540258Beam · dentedNESTED ANGLE ON FWD WEB OF ENGINE BEAM HAS A DEEP GOUGE IN RADIUS APPROX .300 INCH LONG X .075 INCH WIDE AND .050 DEEP. REMOVED DAMAGED SECTION OF NESTING ANGLE. FABRICATED AND INSTALLED REPAIR PARTS IAW EO. (K)Jul 21, 2005 · N420AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR A6WA200540256Support Beam · crackedENGINE SUPPORT BEAM LOWER WEB IS CRACKED AT FWD IB CORNER OF THE RT ACCESS PANEL CUT OUT. ENGINE SUPPORT BEAM LOWER WEB WAS REMOVED AND REPLACED BY MODIFICATION OF BEAM UNDER WO 81584 JOB CARD 4EOMFG08364, SEG NR 14, EO2/081/453. (K)Jul 20, 2005 · N418AW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR VNAA0507014Flap · unknownON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. MAINTENANCE CLEARED THE CAUTION MESSAGE IAW BOMBARDIER SERVICE LETTER RJ-SL-00-001. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.Jul 20, 2005 · N209PS · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR ASOA05612Door · lack of lubeAFTER PARKING THE AIRCRAFT, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE CLEANED AND LUBRICATED THE TRACK AND ROLLER ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (K)Jul 20, 2005 · N846AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR REX2005F00013Sensor · failed(REF NR 05-090) FLAPS FAIL AT 4 DEGREES ON FINAL. PERFORMED RIGGING OF LT AND RT BRAKE POSITION SENSING UNIT ( BPSL) IAW AMM. (K)Jul 20, 2005 · N8560F · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR MASA200500578Tube · unknownASH 6414 DRO, IN FLIGHT ENGINE SHUTDOWN OF NR 1 ENGINE DUE TO LOW OIL PRESSURE. MAINTENANCE REPLACED THE TURBINE REAR FRAME C-SUMP SCAVENGE TUBE AND SEALS.Jul 20, 2005 · N27318 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200540259Sensor · inoperativeRT FUEL HIGH LEVEL SENSOR INOPERATIVE PLACARD AND PLACED ON MEL. CODE ON COMPUTER SHOWS 140 (LT TANK HIGH LEVEL SENSOR). REMOVED AND REPLACED RT FUEL LEVEL SENSOR IAW AMM. OPS AND LEAK CHECK GOOD. (K)Jul 19, 2005 · N459AW · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR A6WA200540260Bpsu · inoperativeFLAPS FAIL CAS APPROACH, MYR FLAPS SELECTED NOT MOVE QAR C/W FLAPS ZERO LANDING. ACCOMPLISHED -30 DEGREES. REMOVED AND REPLACED LT BPSU IAW AMM. OPS CHECK GOOD. (K)Jul 19, 2005 · N426AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA050817007Block · worn(CAN) DURING AN INSPECTION AME FOUND DAMAGE ON NR 2 HYDRAULIC SUCTION LINE UPSTREAM OF RESERVOIR DAMAGE CAUSED BY WORN FAIRLEAD BLOCK ALLOWING HYD SUCTION LINE TO CHAFE ON CASE DRAIN LINE.Jul 19, 2005 · Cndair CL6002B19 · Hoses and TubesSDR CA050817008Block · worn(CAN) DURING AN INSPECTION AME FOUND DAMAGE ON NR 2 HYDRAULIC CASE DRAINLINE UPSTREAM OF RESERVOIR. DAMAGE CAUSED BY WORN FAIRLEAD BLOCK ALLOWING HYDCASE DRAIN LINE AND SUCTION LINE TO CHAFE.Jul 19, 2005 · Cndair CL6002B19 · Hoses and TubesSDR ASOA05610Light · brokenDURING C-CHECK, EMERGENCY EXIT FLOODLIGHT ASSEMBLY BY THE FLIGHT ATTENDANTS STATION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT FLOODLIGHT ASSEMBLY BY FLIGHT ATTENDANTS STATION. OPERATIONAL CHECKS GOOD. (K)Jul 18, 2005 · N832AS · Cndair CL6002B19 · Emergency LightingSDR A6WA200540248Door · damagedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 640BB HAS FRETTING DAMAGE. 2 INCH LONG X .125 INCH WIDE. REPAIRED BY BLENDING AND TREATING DAMAGED AREA IAW REO. (K)Jul 17, 2005 · N420AW · Cndair CL6002B19 · Fluid Service DoorsSDR ASOA05607Step · separatedDURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP ATTACH BRACKET TO THE STAY ROD WAS FOUND SEPARATING FROM THE STEP. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (K)Jul 17, 2005 · N923EV · Cndair CL6002B19 · Entrance StairsSDR ASOA05608Strip · missingDURING A GROUND INSPECTION, AN EMERGENCY FLOOR LIGHT ORANGE STRIP WAS FOUND MISSING. MAINTENANCE REPLACED AN EMERGENCY FLOOR LIGHT, ORANGE STRIP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 17, 2005 · N878AS · Cndair CL6002B19 · Emergency LightingSDR A6WA200540251Clip · crackedFS 280, RBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ SRM 51-42-06 AND BRAS EO 601R-53-6888. (M)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540249Access Panel · damagedRT LOWER WING PLANK AT WS 45, FUEL ACCESS PANEL 640BB CUT OUT, RAS FRETTING DAMAGE 2 INCH LONG X .175 INCH WIDE. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540252Clip · crackedFS 280, RBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540253Clip · crackedFS 280, LBL 9, OB ATTACH CLIP CRACKED. (K) REPLACED ANGLE P/N 601R31113-58 IAW CRJ CRM 51-42-06 AND BRAS EO 601R-53-6888. (M)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540255Clip · crackedFS700, LBL 9 IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW CRM AND EO. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA0507013Access Door · openDURING CLIMB A LOUD NOISE WAS HEARD COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. SUSPECTING AN OPEN DOOR THE CREW DIVERTED TO PIT. MAINTENANCE FOUND THE OXYGEN SERVICING ACCESS PANEL (212BR) OPEN. THE PANEL AND FUSELAGE WERE INSPECTED IAW CRJ200 AMM 05-51-03Jul 16, 2005 · N237PS · Cndair CL6002B19 · Service DoorsSDR A6WA200540274Angle · crackedFS 280, LBL 9, IB ATTACH CLIP CRACKED. REPLACED ANGLE IAW SRM AND EO. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REX2005F00014Warning Light · illuminated(REF NR: 05-088) GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF, DURING GEAR RETRACTION, FOLLOWED QRH WITH UNEVENTFUL LANDING. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/ RETRACTION. OPS CHECK GOOD, OK FOR SERVICE. (K)Jul 16, 2005 · N8525B · Cndair CL6002B19 · Landing Gear Position and WarningSDR REX2005F00015Landing Gear · malfunctioned(REF NR: 05-088) NOSE GEAR WAS NOT DOWN AND LOCKED WITH THE LANDING GEAR SELECTOR IN THE DOWN POSITION, ON APPROACH. THE CREW RECYCLED THE GEAR UP AND DOWN. LANDING GEAR CAME DOWN NORMALLY ON SECOND ATTEMPT. QRH FOLLOWED, LANDING UNEVENTFUL. PERFORMED GEAJul 16, 2005 · N8458A · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA200540250Skin · dentedPROTRUDING DENT AT FS 679, BETWEEN STR 23 AND STR 24, RT MEASURES .5 INCH X .020 INCH DEEP. PERFORMED REPAIR TO FUSELAGE SKIN FROM FS 672 TO 682 BETWEEN STRING STR 23 AND 24 BY CUTTING OUT DAMAGED AREA, PERFORMED NDT OF CUT LINE FAB AND DOUBLER AND INSTALLED Jul 15, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540254Support · crackedWO 84084, MWC 131, RT SIDE UNDERFLOOR SUPPORT STRUCTURE IS CRACKED 1.0 INCH AT FS 621, RBL 40, WL 73. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW REO. (K)Jul 15, 2005 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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