N12540
Service difficulty reports · 86
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 = 'N12540' 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 = 'N12540' 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 ASOA201902274011Wire · brokenLCH - FLIGHT 4264 THE VERY LAST EMERGENCY PROX LIGHT STRIP WAS FOUND TO BE INOPERATIVE DUE TO A BROKEN WIRE ON THE LIGHT ASSEMBLY. MAINTENANCE PLACED THE ITEM OM MEL 33-50-00-2 AND THE AIRCRAFT WAS APPROVED OF RETURN TO SERVICE. ON 03/09/19 IAH MAINTENANCE REMSDR ASOA201710134054Acm · frozenTHE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NR 2 ACM, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVSDR ASOA201710047018Rib · crackedLEFT WING RIB 21 CRACKED. CUT OUT THE SECTION AND INSTALLED FILLER AND DOUBLER.SDR ASOA201710047016Floor Support · corrodedRIGHT OMEGA BEAM, FRAME 23 CORRODED BEYOND LIMITS AT SCREW HOLES. REMOVED AND REPLACED THE OMEGA BEAM.SDR ASOA201805264030Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION THE UPPER EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR ASOA201702134006Light · disconnectedFLIGHT 4045, THE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT TO BE OUT IN THE AISLE NEAR THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND RECONNECTED THE AFFECTED EMERGECY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TSDR ASOA201701163003Axle · brokenDURING ROUTINE MAINTENANCE, THE RIGHT MAIN LANDING GEAR SHOCK ABSORBER LOWER AXLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT SHOCK ABSORBER LOWER AXLE SPECIAL BOLT.SDR ASOA20150727039CInverter · inoperativeDURING ROUTINE MAINTENANCE THE GALLEY EMERGENCY LIGHT WOULD NOT TURN ON. MAINTENANCE REPLACED THE NR 2 AND NR 3 EMERGENCY LIGHT INVERTERS. OPS CHECKS WERE GOOD.SDR ASOA20150506109VBeam · corrodedDURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150506108VFloor Support · corrodedDURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED DOUBLER REPAIRS IAW EC5320-02037. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150506107Frame · corrodedDURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-17L. MAINTENANCE PERFORMED A FRAME SEGMENT SPLICE REPAIR IAW SRM 53-31-04, FIGURE 212. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150428102Shear Tie · corrodedDURING C-CHECK SHEAR TIE AT FRAME 68 CARGO DOOR LOWER BEAM HAS CORROSION. REPAIRED SHEAR TIE AT FRAME 68 IAW SRM 53-31-04. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130514315TFloor Support · corrodedCORROSION AT RT OMEGA BEAM AT NUTPLATE HOLES CORRODED BEYOND LIMITS. R & R HAT SECTION ASSY.SDR ASOA20130514314Profile · corrodedCORROSION AT "T" PROFILE BEYOND LIMITS. R & R T PROFILE LT SIDE AT OMEGA BEAM.SDR ASOA20130514313Gusset · corrodedCORROSION AT GUSSET Y=0.00 CORRODED AROUND SCREW HOLES BEYOND LIMITS. R & R GUSSETSDR ASOA20130514312Gusset · corrodedCENTER OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS. R & R GUSSET.SDR ASOA20130513311Gusset · corrodedCORROSION BEYOND LIMITS ON GUSSET. R & R GUSSET.SDR ASOA20130513310Floor Support · corrodedFLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.SDR ASOA20130513309Floor Support · corrodedRT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.SDR ASOA20130513308Floor Support · corrodedCORROSION BEYOND LIMITS AT FLOOR SUPPORT. R & R FLOOR SUPPORT.SDR ASOA20130513307Floor Support · corrodedRT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.SDR ASOA20130513306Sill · corrodedRT SILL CORRODED BEYOND LIMITS. R & R SILL.SDR ASOA20130513305Sill · corrodedLT SILL CORRODED BEYOND LIMITS. R & R SILL.SDR ASOA20130513304Sill · corrodedLT SILL CORRODED BEYOND LIMITS. R & R SILL.SDR ASOA20130123005CLight · inoperativeDURING ROUTINE MX, THE LT EXTERNAL AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE LIGHT ASSY AND OPS CHECKED GOOD.SDR ASOA20121126155Battery · inoperativeNR 4 BATTERY FOR EMERGENCY LIGHT IN CEILING IS INOPERATIVE. R & R NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.SDR ASOA20121127158Skin · damagedTHE REAR FUSELAGE RT SKIN WAS DAMAGED DURING GROUND OPERATIONS. THE DAMAGE IS LOCATED BETWEEN FRAMES 62 & 63, STR 15R & 17R. REPAIRED DENT WITH FILLER AND DOUBLER. CUTOUT DAMAGED PORTION OF FRAME. FABRICATED AND INSTALLED FRAME SPLICE. REMOVED DAMAGED SECSDR ASOA20121010091Fmu · faultyCREW REPORTED ENGINE NR 2 STARTED SURGING (ERRATIC ACCEL & DECEL) ON DESCENT BETWEEN FL 260& FL250 N1 SPIKE 45-65 ITT SPIKE BETWEEN 400-600. MX R & R ENGINE NR 2 FPMU WITH OPS AND LEAK CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120827114Light · malfunctionedDURING POSTFLIGHT INSP THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. THE EMERGENCY LIGHT SYS WAS OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120827113Light · malfunctionedDURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120519040RController · faultyCREW REPORTED LOSS OF CABIN PRESSURIZATION AT FL330. CREW MANUALLY DEPLOYED PAX O2 MASK AT 12,100 FT WITH CABIN ALT SHOWING 20,000 FT IAW ENGINEERING INSTRUCTIONS AND ASSISTANCE MX R & R THE DIGITAL PRESSURIZATION CONTROLLER, CABIN PRESS. AQUISITION MODULE (CSDR ASOA20120121008Unknown · odorTHE CREW REPORTED SEVERE TURBULANCE AT FL360. LOST ABOUT 1000FT, AP DISENGAGED AND THEY ALSO REPORTED A BURNING ODOR FOR ABOUT A MINUTE. MX COMPLIED WITH TURBULENCE INSPECTION. NO DEFECTS WERE NOTED. AUTOPILOT OPS CHECKED GOOD. NO DEFECTS FOUND. PERFORMESDR C2XA11RI178Flashlight · meltedFLT 4154 EWR - CREW REPORTED A ELECTRICAL SMELL NEAR MAIN CABIN DOOR WITH OBSERVATION OF F/A FLASHLIGHT MELTED. EWR MX REMOVED AND REPLACED THE FWD F/A FLASHLIGHT AND CRADLE ASSY IAW EMB 145 AMM 33-50-16 WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FSDR C2XA11RI176Light · malfunctionedDURING SCHEDULED MAINTENANCE INSPECTION, ROW 12 CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX RESET SYSTEM AND OPERATIONALLY CHECKED THE LIGHT SUCCESSFULLY IAW EMB145 AMM 33-50-00-700-801A. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11CL227Strut · wornCLE FLT 5850 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL, AND A ENGINE 1/2 REV DISAGREE MESSAGE DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NOSE STRUT DEFLATED. DURING REPACK OF THE NOSE STSDR C2XA11CL154Proximity Switch · faultyAVP - FLT 6089 THE CREW REPORTED A LOUD BANGING NOISE FROM UNDER FIRST OFFICER'S FLOOR. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH AND THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.SDR C2XA11TY080Structure · corrodedMINOR CORROSION FWD AND AFT OF THE CARGO DOOR SILL. REMOVED CORROSION AND FOUND TO BE SERVICABLE IAW EC5330-01458 ALODINE, PRIMED AND PAINTED IAW EMB 135/145 CPM 51-21-04, 05&06.SDR C2XA10RI066Switch · defectiveFLIGHT 2183 - EWR - FLIGHT CREW REPORTED BLEED NR 2 LOW TEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BLEED NR PUSH BUTTON SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN SDR C2XA10TY027Line · leakingTYS - A/C WAS EN ROUTE TO ATL FROM EWR WHEN A STAB ANTI ICE FAIL MESSAGE SHOWED. CREW DIVERTED TO TYS AND CHANGE PLANES AND CONTINUED. MAINTENANCE FOUND A LINE LEAKING GOING TO A PRESSURE SWITCH.SDR C2XA10IA026Connector · defectiveIAH - DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE OUTSIDE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EMERGENCY EXIT LIGHT CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS ASDR C2XA10RI001Unknown · odorFLIGHT 2603 - EWR - FLIGHT CREW REPORTED FUEL SMELL IN COCKPIT AFTER APU START. EWR MX PROCEEDED WITH APU OPERATIONAL CHECK BUT COULD NOT DUPLICATE ANY TYPE OF SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09IA204Light · inoperativeGSP - FLIGHT 2675 - THE FLIGHT ATTENDANT REPORTED THE PASSENGER READING LIGHT AT 18C STARTED SMOKING MIDWAY THROUGH THE FLIGHT AND WOULD NOT TURN OFF. THE FLIGHT ATTENDANT USED THE RESET SWITCH BUTTON, AND THE LIGHT EXTINGUISHED AND SMOKE STOPPED. THE AIRCRASDR C2XA09SH241Sill · corrodedSHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH238Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED AND COMPLETED REPAIR AT CENTER OMEGA BEAM FRAME 20 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH237Floor Support · crackedSHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON LT OMEGA BEAM FACE AND FLANGE BETWEEN FRAMES 20-23 AND CRACKED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED AND COMPLETED REPAIR OF LT OMEGA BEAM BETWEEN FRAME 20-22 BY INSTALLING A BEAM SPLICE AT FRAME 19.5 SDR C2XA09SH183Floor Support · corrodedSHV - DURING C-CK, CENTER OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH182Floor Support · corrodedSHV - DURING C-CK, LT OMEGA BEAM HAS CORROSION BETWEEN FR 20 AND 23. REPAIRED OMEGA BEAM IAW EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH181Beam · corrodedSHV - DURING C-CK, CARGO DOOR LOWER CUTOUT HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH180Bracket · damagedSHV - DURING C-CK, LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED LT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH179Bracket · damagedSHV - DURING C-CK, RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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