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 ASOA06190Floorbeam · crackedDURING C-CHECK, THE FS280 BEAM, AT RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 BEAM, AT RBL 9, IAW REO. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA06191Angle · corrodedDURING A C-CHECK, THE FLOOR PANEL AFT ATTACH ANGLE, FS 280, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA06192Panel · corrodedDURING A C-CHECK, THE FLOOR PANEL 221ALF, RT ATTACH ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA06193Attach Angle · corrodedDURING A C-CHECK, THE FLOOR PANEL 221ALF, LT ATTACH ANGLE, WAS FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06194Lamp · burned outDURING A GROUND INSPECTION, THE LT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LT AFT EXTERIOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 16, 2006 · N836AS · Cndair CL6002B19 · Emergency LightingSDR ASOA06197Wire · separatedDURING C-CHECK, THE FLIGHT ATTENDANTS CLOSET EMERGENCY LIGHTING TERMINAL END WAS FOUND TO BE SEPARATED FROM THE WIRING. MAINTENANCE REPLACED THE TERMINAL END ON THE FLIGHTS ATTENDANTS CLOSET EMERGENCY LIGHT ASSY. (K)Feb 16, 2006 · N916EV · Cndair CL6002B19 · Emergency LightingSDR ASOA06198Handle · corrodedDURING A C-CHECK, THE CREW ESCAPE HATCH DOOR HANDLE WAS FOUND TO HAVE CORROSION INSIDE THE HANDLE. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH DOOR HANLE IAW CMM. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA06199Doubler · corrodedDURING AC-CHECK, THE RT PRESSURE FLOOR OB SILL DOUBLER, FROM FS 409+128 TO FS 559, WAS FOUND TO BE CORRODED IN SEVERAL PLACES. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06200Clip · crackedDURING AC-CHECK, THE CLIP ON THE FORWARD FACE 654 WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMNATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06201Clip · crackedDURING C-CHECK, THE CLIP ON RT FS 461, RBL9 OB PRESSURE FLOOR AREA, WAS FOUND TO BE CRACKED.Feb 16, 2006 · N842AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06202Skin · corrodedDURING C-CHECK, THE MIDDLE FUSELAGE AREA FROM FS 409.00+112 TO FS559.00, ON THE LT SIDE, WAS FOUND TO BE CORRODED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Feb 16, 2006 · N843AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA06187Floorbeam · corrodedDURING A C-CHECK, THE FS 280 FLOORBEAM, BETWEEN LBL 9 AND RBL 9, FRONT STRINGER, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 FLOORBEAM, BETWEEN LBL 9 AND RBL 9, FRONT STRINGER IAW REO. (K)Feb 15, 2006 · N843AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA06196Plate · crackedDURING A C-CHECK, THE FORWARD HYDRAULIC ACCESS BAY, AROUND THE BRAKE CABLE HOLE, AT APPROXIAMATELY THE 7 OCLOCK POSITION, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD HYDRAULIC ACCESS BAY, AROUND THE BRAKE CABLE, AT APPROXIMATELY THFeb 15, 2006 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA060228001Windshield · crackedWHILE CRUISING THE LT WINDSHIELD OUTER PLY CRACKED. THE AIRCRAFT CONTINUE INTO WHERE A NEW WINDSHIELD WAS INSTALLED.Feb 15, 2006 · Cndair CL604 · Flight Compartment WindowsSDR ASOA06180Doubler · crackedDURING C-CHECK, THE LT FS 640 DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FS 640 DOUBLER IAW SRM. (K)Feb 14, 2006 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06181Doubler · crackedDURING A C-CHECK, THE RT FS 640 DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT FS 640 DOUBLER IAW SRM. (K)Feb 14, 2006 · N843AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06182Coalescer Bag · dirtyDURING DESCENT, THE CREW REPORTED A SLIGHT BURNING OIL SMELL, WITH NO VISIBLE SMOKE. THE APU WAS STARTED AND THE BLEEDS SWAPPED, AND THE SMELL WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE COALESCER SOCKS. OPFeb 14, 2006 · N932EV · Cndair CL6002B19 · Cabin Cooling SystemSDR ASOA06185Lamp · burned outDURING A HANGAR INSPECTION, THE RT SIDE EXTERIOR AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT SIDE EXTERIOR AFT EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 14, 2006 · N908EV · Cndair CL6002B19 · Emergency LightingSDR ASOA06186Lens · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER, NEAR THE GALLEY, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT COVER, NEAR THE GALLEY. (K)Feb 14, 2006 · N843AS · Cndair CL6002B19 · Emergency LightingSDR VNAA0602007Flap · bird strikeDURING THE SERVICE CHECK, MAINTENANCE FOUND EVIDENCE OF BIRD STRIKE DAMAGE TO THE LEFT INBOARD FLAP. MAINTENANCE COMPLIED WITH A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-57-52-517. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 13, 2006 · N202PS · Cndair CL6002B19 · Leading Edge DevicesSDR VNAA0602006Sensor · damagedTHE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED WHEN THE LEVER WAS MOVED FROM 20 DEGREES TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE SKEW DETECTION SYSTEM TO BE FAULTY. THE SKEW DETECTION SYSTEM WAS DEFERRED PER Feb 13, 2006 · N215PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA06179Manifold · malfunctionedDURING APPROACH, AT APPROXIMATELY 1,500 FT, THE CREW RECEIVED A STEERING INOPERATIVE MESSAGE. THE CREW COMPLIED WITH THE QRH AND REQUESTED THAT THE EMERGENCY VEHICLES BE DISPATCHED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC Feb 13, 2006 · N843AS · Cndair CL6002B19 · Landing Gear Steering SystemSDR ASOA06179AServo Valve · malfunctionedDURING APPROACH, AT APPROXIMATELY 1,500 FT, THE CREW RECEIVED A STEERING INOPERATIVE MESSAGE. THE CREW COMPLIED WITH THE QRH AND REQUESTED THAT THE EMERGENCY VEHICLES BE DISPATCHED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC Feb 13, 2006 · N843AS · Cndair CL6002B19 · Landing Gear Steering SystemSDR ASOA06179BStrut · malfunctionedDURING APPROACH, AT APPROXIMATELY 1,500 FT, THE CREW RECEIVED A STEERING INOP MESSAGE. THE CREW COMPLIED WITH THE QRH AND REQUESTED THAT THE EMERGENCY VEHICLES BE DISPATCHED. THE AIRCRAFT LANDED SAFELY. (K)Feb 13, 2006 · N843AS · Cndair CL6002B19 · Landing Gear Steering SystemSDR ASOA06174Sill · corrodedDURING A C-CHECK, SURFACE CORROSION WAS FOUND AROUND THE NUT PLATE, AT THE CARGO DOOR SILL. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL. (K)Feb 12, 2006 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06176Clip · crackedDURING C-CHECK, THE LT FS 484 CLIP, ON THE OB SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT FS 484 CLIP, ON THE OB SIDE IAW EO. (K)Feb 12, 2006 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06177Door · crackedDURING C-CHECK, THE PASSENGER DOOR, UNDER THE TOP STEP AT THE FORWARD END, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, UNDER THE TOP STEP AT THE FORWARD END, IAW EO. (K)Feb 12, 2006 · N916EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA06167Step · brokenDURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 11, 2006 · N850AS · Cndair CL6002B19 · Entrance StairsSDR ASOA06168Track · crackedDURING C-CHECK, THE CABIN FLOOR EMERGENCY LIGHT TRACK WAS FOUND TO BE CRACKED IN SEVERAL PLACES. MAINTENANCE WILL REMOVE AND REPLACE THE CABIN FLOOR EMERGENCY LIGHT TRACK. (K)Feb 11, 2006 · N916EV · Cndair CL6002B19 · Emergency LightingSDR ASOA06169Web · crackedDURING A C-CHECK, THE LT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, IAW EO. (K)Feb 11, 2006 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA06170Web · crackedDURING A C-CHECK, THE RT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, IAW EO. (K)Feb 11, 2006 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA06171Clip · crackedDURING C-CHECK, THE LT AND RT 625 CLIPS, NEAR STR 14, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LT AND RT 625 CLIPS, NEAR STR 14, IAW REO. (K)Feb 11, 2006 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA06172Doubler · crackedDURING C-CHECK, THE LT 640 DOUBLER, AT STR 10, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE LT 640 DOUBLER, AT STR 10, IAW SRM. (K)Feb 11, 2006 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06173Frame · crackedDURING C-CHECK, FS280, AT RBL9, FROM THE CLIP BOTTOM FASTENER HOLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FS 280, AT RBL 9, FROM THE CLIP BOTTOM FASTENER HOLE, IAW EO. (K)Feb 11, 2006 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA06165Wire · brokenDURING A C-CHECK, THE CABIN OVERHEAD EMERGENCY LIGHT, BETWEEN THE EMERGENCY EXITS ON THE AFT SIDE, WAS FOUND TO BE INOPERATIVE. (K)Feb 10, 2006 · N889AS · Cndair CL6002B19 · Light System WiringSDR ASOA06166Nut Plate · brokenDURING C-CHECK, THE NUT PLATE, ON THE MOST OB FLOOR PANEL, AT FS 409.0+128, WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE NUT PLATE, ON THE MOST OB FLOOR PANEL, AT FS 409.0+128, IAW SRM. (K)Feb 10, 2006 · N916EV · Cndair CL6002B19 · Fuselage Floor PanelSDR VNAA0602004Flap System · malfunctionedTHE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED ON FINAL APPROACH WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND RESET THE FLAP SYSTEM IAW BOMBARDIER SL-27-084. NO FAULTS WEREFeb 9, 2006 · N209PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA06164Step · brokenDURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 9, 2006 · N837AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA06162Mechanism · malfunctionedDURING CLIMB OUT, THE CREW RECEIVED A GEAR DISAGREE MESSAGE AND THE NOSE LANDING GEAR WOULD NOT RETRACT. THE QRH WAS COMPLIED WITH, THE CREW DECLARED AN EMERGENCY AND RETURNED, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UNLOCK ASSFeb 8, 2006 · N828AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR VNAA0602001Warning Light · false activationDURING CLIMBOUT THE -CARGO DOOR- CAUTION MESSAGE ILLUMINATED. PRESSURIZATION WAS STABLE. THE CREW FOLLOWED THE QRH AND ELECTED TO RETURN TO XNA. MAINTENANCE FOUND THE CARGO DOOR HANDLE POPPED OUT. THE HANDLE WAS INSPECTED AND OPERATIONALLY CHECKED. NO DEFFeb 7, 2006 · N220PS · Cndair CL6002B19 · Door Warning SystemSDR ASOA06158Light · damagedDURING A HANGAR INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT, AT ROW 9 AND AFT END CAP, WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK LIGHT AT ROW 9 AND AFT END CAP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 7, 2006 · N921EV · Cndair CL6002B19 · Emergency LightingSDR ASOA06154Placard · unsecureDURING A HANGAR INSPECTION, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO BE UNSECURED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.(K)Feb 6, 2006 · N904EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA06155Handle · crackedDURING A HANGAR INSPECTION, THE AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE. OPERATINAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 6, 2006 · N852AS · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR ASOA06156Windshield · crackedDURING CRUISE, AT APPROXIMATELY 30,000 FEET, THE CREW HEARD A LOUD NOISE AND SAW THAT THE CAPTAINS NR 2 WINDSHIELD HAD SHATTERED. THE CREW DECLARED AN EMERGENCY AND DESCENDED TO 25, 500 FT. THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL, AND THE AC LANDED SAFELYFeb 6, 2006 · N909EV · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA06152Door · bindingDURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR AND NSPECTED THE CABLES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 5, 2006 · N979EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA06153Anchor Fitting · crackedDURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANCHOR FITTING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR AFT ANCHOR FITTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 5, 2006 · N932EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR MASA200600354Engine · overtempASH 6330 BFL - PILOT ABORTED TAKEOFF DUE TO NR 2 ENGINE HIGH ITT. MOC COORDINATING WITH ENGINE SHOP FOR DISPOSITION. AC CURRENTLY OUT OF SERVICE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE.Feb 5, 2006 · N77260 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA06147Step · brokenDURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 4, 2006 · N877AS · Cndair CL6002B19 · Entrance StairsSDR ASOA06149Doubler · crackedDURING A HANGAR INSPECTION, THE RT 640 FRAME DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT 640 FRAME DOUBLER IAW SRM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Feb 4, 2006 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06150Cable · inoperativeDURING A GROUND INSPECTION, THE PASSENGER DOOR HANDLE DID NOT CLOSE PROPERTY AND THE DOOR LOCKING BOLTS REMAINED EXTENDED, PREVENTING THE DOOR FROM CLOSING. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ICE BREAKER CABLE. OPERATIONAL CHECKS GOOD. AIRCFeb 4, 2006 · N916EV · Cndair CL6002B19 · Passenger/Crew Doors
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