N14933
Service difficulty reports · 101
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N14933' AND registry_match = 'registration' 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.
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 n_number = 'N14933' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR C2XA04TY176Frame · damagedDURING C CHECK, THE FASTENER HOLES AT FRAME 61, STRINGER 11R WHERE FOUND DAMAGED. INSTALLED A REPAIR DOUBLER IAW 51-40-02 AND CMP 51-21-04/05. AIRCRAFT RETURNED TO SERVICESDR C2XA04TY174Floor Support · corrodedDURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 22. REMOVED THE CORRODED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5320-01131 AND SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.SDR C2XA03CL164Inverter · inoperativeCLE FLIGHT NR 2278 THE CREW REPORTED THE EMERGENCY EXIT SIGN BEHIND THE F/A SEAT WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA03CL108Light · inoperativeTHE CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT MARKING SIGN. OPERATIONAL CHECKS WERE GOOD.SDR C2XA03BT012Windshield · crackedBWI---CO2476, CREW REPORTED FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT AIRCRAFT DIVERTED TO BWI. AIRCRAFT LANDED UNEVENTFULLY. EWR MAINTENANCE WORKING WINDSHIELD CHANGE AT THIS TIME.SDR C2XA02IA248Duct · damagedFLIGHT 3789, THE CREW NOTED A FIRE INDICATION NR 2 ENGINE AFTER TAKEOFF. THE CREW SHUTDOWN NR 2 ENGINE, DECLARED EMERGENCY, AND, RETURNED TO HSV, AND, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ANTI ICE BLEED DUCT, PERFORMED A SDR C2XA02IA239Pressure Switch · failedTHE CREW NOTED THAT THE RUDDER SYSTEMS NR 1 AND NR 2, INOPERATIVE. ON DEPARTURE, THE CREW DECLARED EMERGENCY. PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER SYSTEM PRESSURSDR C2XA02IA238Pressure Switch · inoperativeIAH- FLIGHT 3558, THE CREW NOTED THAT THE RUDDER SYSTEMS #1 & #2 INOPERATIVE, ON DEPARTURE FOR (TYS), THE CREW DECLAIRED EMERGENCY, AND, PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED TO (IAH), AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED SDR C2XA02IA237Circuit Card · malfunctionedTHE CREW NOTED THAT THE AUTOPILOT/YAW DAMPER FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC-600. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA02SH123Beam · crackedDURING C CHECK LT OMEGA BEAM WAS FOUND TO HAVE A CRACK ON RIVET AT FRAME 22. MAINTENANCE REPAIRED CRACK ON RIVET IAW CONTINENTAL EXPRESS EC 5320-01081. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH121Angle · corrodedDURING C CHECK, LT FLOORBEAM RAMP ANGLE INBOARD AT FRAME 20 HAS CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH120Strap · corrodedSHV- DURING C CHECK CENTER FLOOR BEAM STRAP AT DOUBLER WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND16. MAINTENANCE REMOVED DAMAGE AND PEFPORMED A DOUBLER REPAIR IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH119Beam · corrodedSHV-DURING C CHECK CROSS BEAM BETWEEN FRAMES 23 AND 24 FROM CENTER OMEGA BEAM T O RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION. MAITENANCE REMOVED DAMAGE AND REPLACED AFFECTED CROSS BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVISDR C2XA02SH118Sill · corrodedSHV-DURING C CHECK LEFT HAND SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 23 AND 24. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH117Sill · corrodedSHV- DURING C CHECK NUTPLATES WITH CORROSION WERE FOUND JUST FOWARD OF SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH116Support · corrodedSHV-DURING C CHECK THE SUPPORT RAMP ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACE SUPPORT RAMP IAW EMB SRM51-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH115Floor Support · corrodedSHV DURING C CHECK THE CENTER OMEGA BEAM STRAP BETWEEN FRAMES 18 AND 23 WAS FOUND HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED OMEGA BEAM STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XAO2SH114Threshold · corrodedDURING C CHECK AFT SUPPORT UNDER MAIN DOOR THRESHOLD WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SUPPORT IAW 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH113Floorbeam · corrodedDURING C CHECK, THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE.SDR C2XA02BT033Light · faultyEWR---CO4085, CREW REPORTED, "BOTH EMERGENCY LIGHTS OVER WING INOPERATIVE....MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT UNITS FOR BOTH EMERGENCY LIGHTS OVER THE WINGS IAW EMB145 AMM #33-50-04. OPS.CHECKED GOOD.SDR C2XA02IA115Wire · brokenIAH- WHILE PERFORMING PREFLIGHT INSPECTION THE CREW NOTED THAT A SECTION OF EMERGENCY LIGHTING DID NOT ILLUMINATE. IAH- MAINTENANCEREPAIRED A BROKEN WIRE ON THE EMEMGENCY LIGHT STRIP, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTSDR C2XA02IA112Apu · leakingAMA- THE CREW NOTED THAT AN ELECTRICAL SMELL WAS PRESENT IN THE CABIN/COCKPIT WHILE THE APU IS RUNNING, WITH THE APU BLEED SELECTED OFF. MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED AND THE AIRCRASDR C2XA01BT132Control Handle · faultyEWR---CO4292, CREW REPORTED LANDING GEAR DID NOT RETRACT ON TAKEOFF. INDICATIONS SHOWED GEAR DOWN. CYCLED HANDLE, LANDING GEAR CAME UP AND INDICATED UP. NOSE GEAR DOORS STAYED OPEN. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 MM SDR C2XA01CL132Connector · looseCLE FLIGHT 3690 THE CREW REPORTED THE 2ND STRIP OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR OF THE 2ND STRIP OF EMERGENCY LIGHTS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA01CL122Acm · failedCLE FLIGHT 3992 THE CREW REPORTED A HEAVY BURNING ODOR IN THE COCKPIT AND CABIN FOLLOWED BY SMOKE DURING TAKEOFF AND AFTER LANDING. RECEIVED A PACK NR 1 OVERHEAT MESSAGE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AIR CYCLE SDR C2XA01CL083Wire · brokenCLE FLIGHT NR 3623 THE CREW REPORTED AISLE PATH EMERGENCY LIGHTS BY SEATS 8 AND 9 INOPREATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND OPERATIOMAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR C2XA01CL060Fire Bottle · inoperativeCLE FLIGHT 4089 THE CREW REPORTED EXTINGUISHER BOTTLE-B INOP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE FIRE BOTTLE. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA01IA033A/C Pack · failedDAL - FLIGHT 4061, THE CREW REPORTED THAT ON INITIAL CLIMBOUT, THE COCKPIT AND CABIN FILLED WITH SMOKE ACCOMPANIED BY AN ELECTRICAL BURNING SMELL. THE AIRCRAFT RETURNED TO DAL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THATSDR C2XA00IA424Frame · chafedDURING C CHECK INSPECTION, FRAME 65 RIGHT SIDE FLANGE WAS FOUND TO BE CHAFED BY A CARGO LINER FASTENER. MX REPAIRED THE FRAME AND REPOSITIONED THE CARGO LINER FASTENER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01146SDR C2XA00IA423Angle · crackedDURING C-CHECK INSPECTION, REAR SECTION II, STRINGER #16 RIGHT AT APU FIREWALL. THE SUPPORT ANGLE WAS FOUND TO BE CRACKED. MX REMOVED/REPLACED THE CRACKED ANGLE WITH A FABRICATED PART IAW EMB145 SRM 51-40-02 AND 51-30-01. A/C WAS APPROVED FOR RETURN FOR SERVICSDR C2XA00IA422Strap · corrodedDURING C-CHECK INSPECTION, RIGHT SIDE FLOORBEAM BUTT-STRAP BETWEEN FRAMES 59 TO 61 WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED CORRODED SECTION OF FLOORBEAM IAW EMB145 SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA421Strap · corrodedDURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM BUTT-STRAP BETWEEN FRAMES 60 TO 61 WAS FOUND TO BE CORRODED. MX REMOVED/REPLACED CORRODED SECTION OF THE FLOOR BEAM IAW EMB145 SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA401Floorbeam · corrodedIAH-DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM WAS FOUND TO BE CORRODED FROM FRAME 60-61. MX REMOVED/REPLACED AFFECTED FLOOR BEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02 AND A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAOOIA402Floorbeam · corrodedIAH-DURING C-CHECK INSPECTION, RH FLOOR BEAM WAS FOUND TO BE CORRODED FROM FRAME 59-61. MX REMOVED/REPLACED THE AFFECTED FLOOR BEAM IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA339Strap · corrodedYYZ-DURING MOD-LINE INSPECTION, THE FORWARD CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01107, AND THE AIRCRAFT WAS APPROVED FOR RESDR C2XA00TY011Engine · malfunctionedBTV - FLT 4201 - CREW REPORTED SMOKE IN THE COCKPIT AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO TYS WHERE ROLLS ROYCE SERVICE BULLETIN NR AE3007A-A-72-156 WAS COMPLIED WITH ON THE LEFT ENGINE. SDR C2XA00BT048Seal · leakingBTV-TYS - FLT 4201 - CREW REPORTED SMOKE IN COCKPIT AFTER TAKEOFF. AIR RETURNED TO BTV. TROUBLESHOT AND DETERMINED THAT OIL WAS LEAKY FAN SEAL. AIRCRAFT MAINTENANCE FERRIED TO TYS MAINTENANCE COMPLIED WITH ROLLS ROYCE SERVICE BULLETIN AND REPLACED TELFON LISDR 99ZZZX3197Duct · weakCLE - FLT 3942 - SMOKE FROM CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. AIRCRAFT RELEASED IAW MEL 36-11-05 CONTROL NR 184831. MAINTENANCE REMOVED AND REPLACED THE LT PACK DTV DUCT AND REPLACED THE BROKEN CLAMP IAW EMB-145 MM 36-11-9. OPS AND SDR C2XA99CL074Clamp · brokenCLE - FLT 3942 - SMOKE FROM CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. AIRCRAFT RELEASED IAW MEL 36-11-05 CONTROL NR 184831. MAINTENANCE REMOVED AND REPLACED THE LT PACK DTV DUCT AND REPLACED THE BROKEN CLAMP IAW EMB-145 MM 36-11-9. OPS AND SDR C2XA99CL073Duct · looseMSP/CLE - FLT 4012 - THE CREW REPORTED SMOKE FROM THE CENTER CONSOLE ALONG WITH SMOKE IN THE CABIN AND COCKPIT. THE AIRCRAFT DIVERTED TO GRB AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A DUCT HAD BLOWN OFF THE LEFT PACK SYSTEM, THEY RELEASED THE ASDR C2XA99BT066Engine · leakingBTV - FLT 4201 - CRWE REPORTED, 'LAV SMOKE INDICATION FOLLOWED BY BAG SMOKE IN INDICATION AFTER TAKEOFF, BOTH INDICATIONS EXTINGUISHED ON GROUND AFTER AREA RETURN. CAUSED OVERWEIGHT LANDING'. PRESENTLY MAINTENANCE IS TROUBLESHOOTING CAUSE OF INDICATIONS. PESDR C2XA99BT061Smoke Detector · fodBTV - MAINTENANCE TROUBLESHOT AND REPAIRED BAGGAGE SMOKE WARNING ON LANDING REPORT FROM CREW. FOUND SCREW STUCK IN BAGGAGE FORWARD SMOKE DETECTOR. REMOVED SCREW, OPS CHECKED SYSTEM GOOD AND RETURNED TO SERVICE. (M)SDR C2XA99IA293Bulb · failedIAH - DURING C-CHECK INSPECTION, FOUR OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULBS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA292Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC553SDR C2XA99IA291Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FUSELAGE TO VERTICLE STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC553SDR C2XA99IA290Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20 EXTENDING UNDER THE BUTT STRAP. MAINTENANCE REMOVED THE CORROSION AND INSTALLED REINFORCEMENTS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC53SDR C2XA99CL027Air Dist · odorCLE - FLT 4059 - CREW REPORTED THAT AFTER SETTING TAKEOFF POWER THEY RECEIVED A SMOKE SMELL IN THE COCKPIT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IT IAW MEL 21-51-00 CONTROL NR 173359. ON 3/24/99 MAINTENANCE PERFORMESDR C2XA98BT086Skin · crackedSMALL CRACK IN SECTION OF FUSELAGE BEHIND PASSENGER DOOR. REPAIRED DAMAGED SECTION OF FUSELAGE IAW SRM. PRESSURE CHECKED GOOD. (M)SDR C2XA98BT076Air Distribution · smokeFLT 4251 - CREW REPORTED SMOKE IN COCKPIT IMMEDIATELY AFTER ADVANCING THRUST LEVER FOR TAKEOFF. TAKEOFF WAS REJECTED. MAINTENANCE INSPECTED NR 1 AND NR 2 ENGINES, APU COMPARTMENT, AVIONIC BAYS FORWARD AND AFT, HYD COMPARTMENTS, LAV AND BAGGAGE COMPARTMENTS FOSDR C2XA97CL072Engine · failedCLE - FLT 4006 - CREW REPORTED WHEN THE POWER LEVERS WERE PLACED IN THE TAKEOFF OR CONTINUAL THRUST DETENT, THE LEFT HAND AND RIGHT HAND ENGINES' OIL PRESSURE REMAINED HIGH. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGI
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