N708UW
Service difficulty reports · 218
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 = 'N708UW' 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 = 'N708UW' 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 USAA040135Floor Panel · delaminatedBFM - FOUND PANEL DELAMINATED AND CORRODED 7 SQUARE INCHES TOTAL, PANEL 261EG AFT CABIN FLOOR. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M)SDR USAA040134Floor Panel · delaminatedBFM - FOUND PANEL DELAMINATED APPROX 6 SQUARE INCHES TOTAL, PANEL 262HG AFT CABIN FLOOR. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M)SDR USAA040133Floor Panel · corrodedBFM - FOUND FLOOR PANEL CORRODED 2.20 INCHES LONG BY 2.40 INCHES WIDE, FRAME 66-68 AT ENTRY L-2 DOOR, NR 261FF. CORROSION LEVEL 2, TASK NR JA-260-53100. REMOVED AND REPLACED WITH NEW PART PER SRM 51-74-00, 51-42-11. (M)SDR USAASA04035Lanyard · damagedBFM - THE SLIDE GIRT BAR LANYARD CABLE BALLS DISENGAGED UPON INSTALLATION OF ESCAPE SLIDE ONTO AIRCRAFT. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (M)SDR USAA040124Beam · corrodedBFM - FOUND BEAM TRACK ASSEMBLY CORRODED 1.5 INCHES IN DIAMETER BY .03 INCH DEEP AREA, FRAME 1292 AND CROSSBEAM C66 -Z240. REMOVED AND REPLACED TRACK BEAM ASSEMBLY PER SRM 51-74-00, 53-00-14, 51-42-11. (M)SDR USAA040125Seat Track · corrodedBFM - OFUND SEAT TRACK CORRODED 2 INCHES BY 1.5 INCH BY .025 INCHE DEEP, FRAME 66-68, -Y1292, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-41-14, 53-00-14, 51-42-11, 51-74-00. (M)SDR USAA040131Stiffener · corrodedBFM - FOUND STIFFENER ASSEMBLY CORRODED 3.5 INCH BY 1.0 INCH BY .015 INCH DEEP, FRAME 12, BETWEEN Y-81 AND Y-1379.5, Z-240. REMOVED AND REPLACED STIFFENER ASSEMBLY PER SRM 53-11-14, 51-42-11, 51-74-00. CORRODED LEVEL 2, TASK NR JA-220-53500. (M)SDR USAA040129Crossbeam · corrodedBFM - FOUND BEAM CORRODED 2.5 INCHES LONG BY 1.5 INCHES WIDE BY .03 INCH DEEP AREA, FRAME Y1732 BETWEEN CROSSBEAM C68 AND C69 -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M0SDR USAA040126Beam · corrodedBFM - FOUND BEAM CORRODED 2 INCHES LONG BY 1.5 INCHES WIDE BY .040 INCHE DEEP AREA, FRAME -Y1292 BETWEEN CROSSBEAM C68 AND C69. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)SDR USAA040128Crossbeam · corrodedBFM - FOUND 1.5 INCH LONG BY 1 INCH WIDE BY .02 INCH DEEP 4 PLACES, FR 1732 BETWEEN CROSSBEAM C66 AND C68. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M)SDR USAA040130Shear Plate · corrodedBFM - FOUND SHEAR PLATE CORRODED 3.5 INCH IN DIAMETER AND .010 INCH DEEP AREA, FRAME 71292 BETWEEN CROSSBEAM C89 AND C70 -Z40. REMOVED AND REPLACED SHEAR PLATE PER SRM 51-74-00, 53-41-17 AND 51-42-11. (M)SDR USAA040139Beam · corrodedBFM - FOUND BEAM CORRODED 2 INCHES BY 1.5 INCHES BY .025 INCH AREA, Y-254, FR 66-68, -Z240. REMOVED AND REPLACED BEAM PE SRM 51-42-11, 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)SDR USAA040123Web · corrodedBFM - FOUND WEB CORRODED 1.5 INCHES BY 1.5 INCH BY .005 INCH AREA, BETWEEN FRAME 69 AND FRAME 70 BL Y1292. REMOVED AND REPLACED WEB PER SRM 53-41-17, 51-74-00, 51-42-11, 51-72-11. (M)SDR USAA040140Beam · corrodedBFM - FOUND BEAM CORRODED 2 INCHES BY 2 INCHES BY .020 INCH DEEP, BETWEEN FRAME 64 AND 65, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11. (M)SDR USAA040138Seat Track · corrodedBFM - FOUND SEAT TRACK BEAM CORRODED 2 INCHES IN DIAMETER BY .030 INCH DEEP AREA, BETWEEN FRAME 64 AND 65, -Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11, 51-44-00, 51-23-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)SDR USAASA03013Engine · failedTHE FLT WAS APPROXIMATELY 65 MILES FROM SJU, CLIMBING THROUGH FL200, WHEN A LOUD BANG WAS HEARD THROUGHOUT THE AIRCRAFT, FOLLOWED BY VIBRATION AND A LOSS OF N2 INDICATION. THE ENGINE WAS SHUTDOWN BY THE CREW WHILE THE ENGINE PARAMETERS BEGAN TO DECAY. FLIGHTSDR USAASA02077Computer · faultyGCM - FLT 1093 - EN ROUTE GCM-CLT, AFTER TAKEOFF, RECEIVED AN 'AVNCS SMOKE' MESSAGE ON THE ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SYSTEM. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE DISPLAY MANAGEMENT COMPUTER ISDR USAASA00023Engine · failedRNO - FLT 70 - EN ROUTE SFO-PHL, WHILE ON DOWNWIND FOR RUNWAY 16, THE NR 1 ENGINE OIL FILTER CLOG LIGHT CAME ON AS WELL AS A DROP IN OIL PRESSURE TO 5 PSI. THE NR 1 ENGINE WAS SHUTDOWN AND A SAFE LANDING WAS MADE. TOTAL SINGLE ENGINE TIME WAS 5 MINUTES. MAI
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