N16147
Service difficulty reports · 177
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 = 'N16147' 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 = 'N16147' 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 ASOA20130202007CBattery · dischargedDURING ROUTINE MX THE SERVICE DOOR FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT BATTERY AND OPS CHECKS WERE GOOD.SDR ASOA20120212017Light · inoperativeTHE CREW REPORTED THE EXIT MARKER NEAR THE MAIN CABIN DOOR WAS INOPERATIVE. MX R & R THE AFFECTED LIGHTP, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120104003Skin · crackedDURING C-CK LT FUSELAGE SKIN HAS CRACKS FR 79-81, STR 8L-10L. REPAIRED SKIN IAW EC5330-02501. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120104002Support · corrodedDURING C-CK. BAGGAGE DOOR LOWER CUTOUT CORRODED. R & R LOWER CARGO DOOR CUT OUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120104001VSupport · corrodedDURING C-CHECK. WASTE DRAIN DUMP VALVE SUPPORT CORRODED. R & R WASTE DRAIN DUMP VALVE SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201112160010Fire Loop · failedCREW REPORTED ENGINE NR 2 FIRE DETECTOR FAIL IN FLT. MX R & R ENGINE NR 2 FIRE DETECTOR LOOP IAW AMM 26-11-0I WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11IA063Selector Switch · inoperativeVSA - FLIGHT 2964 THE CREW REPORTED THAT THE NUMBER ONE ELECTRIC HYDRAULIC PUMP CIRCUIT BREAKER POPPED WITH A STRONG ELECTRICAL SMELL. MAINTENANCE REMOVED AND REPLACED THE SELECTOR SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOSDR C2XA11RI047Unknown · smokeFLIGHT 2665 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN AFTER T/O FOLLOWED BY LAV SMOKE INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PERFORMED ENGINE NR 1 AND NR 2 RUN UP AT HIGH POWER WITH BLEED SYSTEM ON FOR 3 MIN (TWICE).SDR C2XA10RI091Unknown · odorFLIGHT 3070 - EWR - FLIGHT CREW REPORTED HEAVY AROMA OF LAV FLUID IN CARGO BIN. EWR MX OPENED CARGO FLOORBOARD AND INSPECTED FOR LAV FLUID LEAK. NO LEAKAGE FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA10CL057Line · looseIAH FLT 2738 THE CREW REPORTED A WING ANTI-ICE FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE-SECURED LOOSE LINE ON WING ASSY SWITCH. OPERATIONAL CHECKS WERE GOOD.SDR C2XA10SH118Skin · crackedSHV - DURING C-CHECK LT FUSELAGE SKIN HAS CRACK AROUND RIVET FR 77. REPAIRED SKIN IAW EC5330-02099. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH117Skin · crackedSHV - DURING C-CHECK RT FUSELAGE SKIN HAS CRACK AROUND RIVET FR 79. REPAIRED SKIN IAW EC5330-02099. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH116Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH115Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 24-25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH114Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH113Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10CL003Tat Probe · faultyCLE FLIGHT 2659 THE CREW REPORTED A "TAT 1 HEAT INOP" MESSAGE ON THE EICAS IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 TAT PROBE AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA09RI228Clamp · missingFLIGHT 2968 - EWR - FLIGHT CREW REPORTED THAT ON CLIMBOUT NR 2 ENGINE ITT ROSE INTO THE AMBER RANGE AT E-CLIMB POWER. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. E2 RUNS ABOUT 150 DEGREES HIGHER THAN E1. UPON LANDING, E2 EXCEEDANCE ON EICAS. E2SDR C2XA08RI122Inverter · inoperativeFLIGHT 2074 EWR FLIGHT CREW REPORTED EMERGENCY EXIT IDENTIFIER ABOVE FORWARD FLIGHT ATTENDANT SEAT INOPERATIVE. EWR MX R&R NR 1 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA08CL095Sleeve · blownEWR FLIGHT 2879, THE CREW REPORTED A BLEED VALVE 2 FAIL IN FLIGHT. THE ACFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED A BLOWN SLEEVE ON THE NR 2 ENVIRONMENTAL CONTROL UNIT. ALSO REPLACED THE NR 2 BLEED PUSH BUSDR C2XA08SH091Skin · gougedSHV - DURING C-CHECK IT WAS FOUND THAT THE CENTER FUSELAGE SKIN HAD AN INTERNAL GOUGE BETWEEN FRAMES 16 AND 17, AND STRINGERS 3R AND 4R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)SDR C2XA08SH090Fitting · wornSHV - DURING C-CHECK IT WAS FOUND THAT THE RT HORIZONTAL STAB HINGE PIN FITTING HAD MIGRATED PLAIN BUSHINGS. MAINTENANCE PERFORMED A REAMING PROCEDURE TO THE SECOND OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)SDR C2XA08SH089Fitting · gougedSHV - DURING C-CHECK IT WAS FOUND THAT THE LT HORIZONTAL STAB HINGE PIN FITTING WAS GOUGED. MAINTENANCE PERFORMED A REAMING PROCEDURE TO THE FIRST OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)SDR C2XA07IA097Light · inoperativeIAH - FLIGHT 2071, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE F/A HEADREST TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED SDR C2XA06CL039Charger · faultyCLE FLIGHT NR 2330, THE CREW REPORTED THE FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06IA032Wire · looseIAH - FLIGHT 2008, DURING POSTFLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REPAIRED A LOOSE WIRE ON GROUND BLOCK GS8506DC, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETUSDR C2XA04IA110Holder · shortedTHE CREW REPORTED THAT A SPRING BEHIND THE F/O'S MAP HOLDER MADE CONTACT WITH AN EXPOSED WIRE CAUSING SMOKE. MAINTENANCE REMOVED AND REPLACED THE F/O'S MAP HOLDER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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