N14939, cancelled Aug 13, 2015
Service difficulty reports · 135
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 = 'N14939' AND deregistration_id = 'N14939-2015-08-13' 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 = 'N14939' AND deregistration_id = 'N14939-2015-08-13' 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 ASOA20140801100Light · inoperativeDURING PREFLIGHT INSPECTION, THE CREW REPORTED EXIT ROW EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140318066Frame · crackedDOOR 123BL CRACKED UNDER HINGE POINT MOUNT. REMOVED CRACKED FRAME AND INSTALLED NEW HALF FRAME ON DOOR 123BL IAW SRM 51-40-02.SDR ASOA20140318065TChannel · corrodedCORROSION ON RT OMEGA BEAM AT NUTPLATE JUST AFT OF FRAME 59. REMOVED CORROSION, REPAIRED OMEGA BEAM IAW EC5320-01910.SDR ASOA20140318064Floorbeam · crackedFLOORBEAM FRAME 61 NUTPLATE HOLE CRACKED. R & R TEE ON FLOORBEAM IAW SRM 51-40-02.SDR ASOA20140318063Shear Tie · crackedSHEAR TIE CRACKED AT FRAME 24 BETWEEN STRINGERS 15 & 16R. R & R SHEAR TIE IAW SRM 51-40-02.SDR ASOA20140318062Shear Tie · crackedCRACK AT RIVET IN SHEAR TIE AT FRAME 81, APU FIREWALL, BETWEEN S1 & 2R. REMOVED CRACKED SHEAR TIE AND INSTALLED NEW IAW SRM 51-40-02.SDR ASOA20140318061Attach Angle · crackedCRACK IN ANGLE JOINING FRAME 46 TO WING BOX ON RT SIDE AT FLOOR LEVEL. R & R ANGLE IAW SRM 51-40-02.SDR ASOA20140318060TChannel · crackedLEFT OMEGA GUSSET OTBD SPLICE CRACKED BETWEEN FRAMES 16 & 17. R & R OMEGA GUSSET IAW 51-40-02.SDR ASOA20140318059Channel · corrodedRIGHT OMEGA BEAM CORROSION AROUND NUTPLATE FRAME 23. REMOVED CORROSION AND FABRICATED REPAIR IAW EC5320-01443, REV C.SDR ASOA20140318058Floor Support · chafedLEFT FLOOR SUPPORT AT FRAME 72 HAS CHAFED METAL IN MULTIPLE AREAS WITH EXPOSED BARE METAL. R & R FLOOR SUPPORT IAW 51-40-02.SDR ASOA20140318057Shear Tie · crackedFRAME 46 SHEAR TIE CRACKED.SDR ASOA20140318056Floor Support · corrodedRT FORWARD FLOOR SUPPORT HAS CORROSION OTBD OF NUTPLATE BETWEEN FRAMES 23 & 24. FOUND OUT OF LIMITS IAW SRM 53-21-10.SDR ASOA20140318055Floor Support · crackedRT OMEGA BEAM SUPPORT FLANGE CRACKED NEAR FOOT RADIUS AT FRAME 47 ON OTBD SIDE OF BEAM.SDR ASOA20140318054Channel · corrodedC-CHECK, THE CENTER OMEGA BEAM GUSSET WAS CORRODED AT NUTPLATES AT FRAME 16. MAINTENANCE REMOVED THE CORROSION AND FABRICATED A NEW REPAIR IAW EC 5320-01215, REV ORIGINAL.SDR ASOA20140318053TChannel · corrodedDURING C-CHECK, THE RT SIDE OMEGA BEAM TOPCAP WAS FOUND CORRODED AT FRAME 59. MAINTENANCE R & R THE RT SIDE OMEGA BEAM GUSSET AT FRAME 59 IAW SRM 51-40-02SDR ASOA20140318052TShear Tie · crackedDURING C-CHECK, LT CENTER FUSELAGE FRAME 46 HAS A SHEAR TIE CRACKED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-40-02.SDR ASOA20140318051Floor Support · crackedC-CHECK, THE LT FLOOR SUPPORT SPLICE WAS FOUND CRACKED AT FRAMES 23 AND 24. MAINTENANCE R & R IAW SRM 51-40-02.SDR ASOA20130830158Gcu · malfunctionedTHE CREW REPORTED AN ELECTRICAL PROBLEM WITH THE MAIN BUSS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL ODOR CAME IN THE COCKPIT) AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING IN BPT WITHOUT INCIDENT. SDR ASOA20130830157Starter Gen · malfunctionedTHE CREW REPORTED AN ELECTRICAL PROBLEM WITHTHE MAIN BUS SHORTING OUT AT 23K FT ALT WITH A LOUD BANG WHICH SHOOK THE ENTIRE ACFT. SMOKE, ELECTRICAL SMELL CAME IN THE COCKPIT, AFTER THE BANG. THE ACFT PERFORMED AN EMERGENCY LANDING WITHOUT INCIDENT. MX INSPESDR ASOA20130209010HSkin · crackedDURING SCHEDULED MX, THE AFT FUSELAGE AFT UPPER SKIN WAS FOUND TO BE CRACKED AT FRAME NR 75 NEAR STRINGER NR 2. THE FUSELAGE SKIN WAS REPAIRED BY INSTALLATION OF A DOUBLER IAW EC5330-02353.SDR ASOA20120323043Cdu · shortedTHE CREW REPORTED A STRONG ELECTRICAL ODOR FROM BEHIND THE CAPTAIN`S SEAT AREA. MX INSPECTED AND FOUND THE FMS, CMU TO BE CAUSING THE ODOR. MX R & R THE FMS CDU, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120229029Sensor · inoperativeDURING TAKEOFF ROLL AT APPROX 90KTS, THE CREW REPORTED THAT THEY SMELLED SMOKE AND RECEIVED A BRAKE OVERHEAT MESSAGE. TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE GATE WHERE MX INSPECTED THE ACFT R & R A FAULTY BRAKE TEMP SENSOR, OPERATIONALLY TESTED WITH SDR ASOA2011112600005Skin · damagedDURING C-CHECK, WORKING RIVETS AT FRAME 77, STRINGER 4R-10R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 77, STRINGER 4R-10R IAW EC5330-02501 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA2011112600004Skin · crackedDURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 6R-7R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 78, STRINGER 6R-7R IAW EC5330-02501 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA2011112600003Skin · crackedDURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 7R-8R. MX PERFORMED REPAIR OF FUSELAGE AT FRAME 78, STRINGER 7R-8R IAW EC5330-02501 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201111260002Skin · crackedDURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 4R-5R. MX PERFORMED REPAIR OF FUSELAGE SKIN IAW EC5330-02501 ORIG. AIRCRAFT RETURNED TO SERVICE.SDR ASOA201111261009Threshold · corrodedDURING C-CHECK SERVICE DOOR THRESHOLD CORRODED AROUND NUTPLATES. MX R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201111261008Skin · crackedDURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 5R-6R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 79 STRINGER 5R-6R IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201111261006Skin · crackedDURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 75 STRINGER 3R-4R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 75 STRINGER 3R-4R IAW EC5330-02353. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11IA244Indication Sys · malfunctionedIAH - FLIGHT 4664 THE CREW REPORTED THAT FUEL QUANTITY NR 1 DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY TESTED THE FUEL QUANTITY SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TSDR C2XA11IA129Bracket · brokenIAH - FLIGHT 2481, THE CREW REPORTED AN INFLIGHT ABNORMAL VIBRATION IN THE YOKE WHILE AIRBORNE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE SPRING TAB FAIRING BRACKET, OPERATIONALLSDR C2XA11IA078Computer · faultyIAH - FLIGHT 3127, THE CREW REPORTED THAT AHRS NR 1 FAILED IN FLIGHT TWICE FOR 30 SECONDS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ASDR C2XA11IA059Engine · vibrationIAH - FLIGHT 2482 IAH-GPT, THE CREW REPORTED ENGINE TWO VIBRATION IN AMBER FOR 2-3 SECONDS DURING CLIMB, AND AFTER POWERING BACK THE VIBE RETURNED TO GREEN RANGE, RETURNED AIRCRAFT TO CLIMB POWER AND VIBRATION STABILIZED BETWEEN 2.0 AND 2.4 IPS. THE AIRCRAFT SDR C2XA11IA007Light · overheatedFLIGHT 2967, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRIC BURNING ODOR AROUND ROW 5 OR 6. MAINTENANCE INSPECTED THE AIRCRAFT, FOUND A BAD LIGHT SOCKET AT ROW 5A LATERAL LIGHT. MAINTENANCE REMOVED THE BULB AND PLACED THE LIGHT ON MEL, AND THE AIRSDR C2XA10IA089Ecu · inoperativeLCH - FLIGHT 2214, THE CREW REPORTED A FLAP FAIL DURING CRUISE. THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WASDR C2XA09SH343Fitting · crackedDURING C-CHECK, NR 1 ENG FWD LOWER YOKE FITTING CRACKED. REMOVED AND REPLACED FWD LOWER YOKE FITTING IAW EC5450-01021. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA216Splice · brokenIAH - DURING MAINTENANCE INSPECTION THE AFT SECTION OF AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BROKEN SPLICES, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA178Light · inoperativeIAH - FLIGHT 2115 - DURING POST FLIGHT INSPECTION THE LEFT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA09TY137ASocket · brokenEMERGENCY LIGHT IN THE MAIN DOOR AND THE SERVICE DOOR INOP. REMOVED AND REPLACED THE LIGHT SOCKETS IAW EMB AMM 33-50-06. OPS CHECK GOOD.SDR C2XA09IA153Fan · inoperativeIAH - FLIGHT 3042, ON CLIMB, THE CREW REPORTED AN AHRS 1 OVERHEAT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS FAN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETUSDR C2XA09CL075Turbine Wheel · crackedDURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.SDR C2XA09SH169Frame · damagedSHV - DURING C-CHECK FRAME 10 JUST ABOVE STRINGER 10L WAS CRACKED AND PIECE MISSING. MAINTENANCE REMOVED AND REPLACED FRAME 10 STRINGER 10L IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH168Frame · damagedSHV - DURING C-CHECK RT CARGO FRAME 64 HAD A DAMAGED RIVET BETWEEN STRINGER 8R-9R. MAINTENANCE REPAIRED FRAME 64 STRINGER 8R-9R WITH REPAIR IAW IC2009-145/03545. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH167Beam · corrodedSHV - DURING C-CHECK CARGO CUTOUT LOWER BEAM HAD CORROSION. MAINTENANCE REMOVED AND REPLACED CARGO LOWER BEAM AT FRAME 65-68 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH166Floor Support · corrodedSHV - DURING C-CHECK RT OMEGA BEAM HAD CORROSION AT NUT PLATE HOLES AT FRAME 20. MAINTENANCE REPAIRED RT OMEGA BEAM AT FRAME 20 IAW EC5320-01461. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH165Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAD CORROSION AT FRAME 20. MAINTENANCE REPAIRED LT OMEGA BEAM WITH REPAIR AT FRAME 20 IAW EMB-145 SRM 51-40-02 AND CPM 51-21-04/05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09TY027Battery · dischargedNR 2 EMERGENCY LIGHT BATTERY LOW VOLTAGE. REMOVED AND REPLACED BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA09IA043Light · inoperativeIAH - FLIGHT 2931, DURING PREFLIGHT INSPECTION THE AISLE PATH EMERGENCY LIGHT STRIP BY THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MX R&R THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS NOTED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2X2008F00006Wire · brokenIAH - FLIGHT 3056 ON TAKEOFF ROLL THE CREW REPORTED SEEING HOT EMBERS AND DETECTING SMOKE FROM UNDER THE CAPTAINS DASH, WITH THE CIRCUIT BREAKER ON THE OVERHEAD POPPING. THE CREW ABORTED TAKEOFF, AND TAXIED BACK TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPSDR C2XA08IA103Uplock · malfunctionedIAH - FLIGHT 2106, THE CREW REPORTED A LOUD BANGING NOISE UNDER THE FLIGHT COMPARTMENT FLOOR, AND THAT THE RIGHT MAIN LANDING GEAR INDICATION CYCLING BETWEEN UP AND AMBER. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND
Back to N14939, cancelled Aug 13, 2015