N709UW
Service difficulty reports · 376
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 = 'N709UW' 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 = 'N709UW' 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 USAA040329Seat Track · corrodedBFM - FOUND SEAT TRACK CORRODED 1 INCH BY 5 INCH BY .032 INCH AREA, FRAME 24 BL Y-1292. INSTALLED NEW SEAT TRACK SEGMENT AND SPLICES. (M)SDR USA2004F00088Seat Track · corrodedFOUND CORROSION ON SEAT TRACK, 1 INCH X 5 INCHES X .032 INCH. INSTALLED NEW SEAT TRACK SEGMENT AND SPLICES IAW SRM.SDR USA2004F00086Support · corrodedFOUND CORROSION ON SUPPORT PLATE, 6 INCH X 0.5 INCH X .020 INCH. INSTALLED NEW R2 DOOR FORWARD GIRT BAR FITTING SUPPORT PLATE.SDR USAA040319Frame · corrodedFRAME, .090 INCH X .090 INCH X .026 INCH AREA, CORROSION; LEVEL 2; FR16, Y81, Z240. NEW FRAME ASSY INSTALLED IAW SRM.SDR USAA04343Plate · corrodedFOUND CORROSION ON PLATE ASSEMBLY, 2 INCHES BY 2 INCHES BY .040 INCHES. REPLACED PLATE. (M)SDR USAA04342Plate · corrodedFOUND CORROSION ON PLATE ASSEMBLY, 2 INCHES PLUS 2 INCHES BY .040 INCH. REPLACED PLATE. (M)SDR USAA040323Web · corrodedBFM - FOUND WEB CORRODED 5 INCHES BY 3 INCHES BY .040 INCH DEEP AREA, C69 TO C70 -Y1292. REMOVED AND REPLACED WEB PER SRM 53-14-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M)SDR USAA040331Plate · corrodedBFM - FOUND PLATE ASSEMBLY CORRODED 2 INCHES BY 2 INCHES BY .40 INCH AREA, Y1732, -Z240, FRAME 68. INSTALLED NEW PLATE ASSEMBLY PER SRM 53-12-00. (M)SDR USAA040332Plate · corrodedBFM - FOUND PLATE ASSEMBLY CORRODED 4 INCHES BY .50 INCH BY .020 INCH AREA, Y1732, -Z240, FRAME 66. INSTALLED NEW PLATE ASSEMBLY PER SRM 53-12-00. (M)SDR USA2004F00090Floor Panel · corrodedFOUND CORROSION THROUGH MAIN FLOOR DECK PANEL, 2 INCH X 2 INCH X .040 INCH. REPLACED PANEL.SDR USAA040321Frame · corrodedFRAME, 1.0 INCH X 5 INCHES X 0.71 INCH AREA, CORROSION; LEVEL 2; FR 21 AT Y254. INSTALLED NEW FRAME IAW SRM. INSTALLED NEW FRAME IAW SRM.SDR USAA040311Floor Panel · delaminatedFLOOR PANEL, EXCEEDS 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK PANEL 221 PF. FABRICATED NEW FLOOR PANEL IAW SRM.SDR USAA040310Floor Panel · delaminatedFLOOR PANEL, 10 PERCENT OF TOTAL AREA, MAIN DECK FLOOR PANEL 262HG, DELAMINATION. FABRICATED NEW PANEL IAW SRM.SDR USAA040309Floor Panel · delaminatedFLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, PANEL 262EF. FABRICATED NEW FLOOR PANEL 262 EF.SDR USAA040308Floor Panel · delaminatedFLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, FLOOR PANEL 261DF. FABRICATED NEW FLOOR PANEL IAW SRM.SDR USAA040317Floor Support · corrodedFLOOR SUPPORT, 2.0 INCH X 1.0 INCH X .026 INCH D, CORROSION; LEVEL 2 BETWEEN FR 21-22, Y1292, Z240. REMOVED AND REPLACED PART IAW SRM.SDR USAASA04028Bearing · spalledEN ROUTE, DURING APPROACH, AT 12000 FT, RECEIVED (ENG 1 OIL FILTER CLOG) ECAM MESSAGE, THEN, THE NR 1 ENGINE BEGAN TO FLUCTUATE, VIBRATE AND SURGE UNTIL IT QUIT. CREW ACCOMPLISHED, THE SHUTDOWN PROCEDURES GIVEN BY ECAM ACTIONS. FLIGHT LANDED WITHOUT FURTHERSDR USA2004F00029Engine · failedENROUTE, DURING APPROACH, AT 12,000 FEET, RECEIVED (ENG 1 OIL FILTER CLOG) ECAM MESSAGE. THEN THE NUMBER ONE ENGINE BEGAN TO FLUCTUATE, VIBRATE AND SURGE UNTIL IT QUIT. CREW ACCOMPLISHED THE SHUT DOWN PROCEDURES GIVEN BY ECAM ACTIONS. FLIGHT LANDED WITHOUT SDR USAASA03028Battery · inoperativeLGA - THE EMEGENCY LIGHTS SYSTEM FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED THE BATTERY AT THE RIGHT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)SDR USAASA03023Power Supply · inoperativeLGA - THE EMERGENCY LIGHT TEST INDICATED THAT THE LEFT EMERGENCY POWER SUPPLY UNIT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)SDR USAASA01003Oven · fireCLT-LGA- FLT 1886 - AFTER DEPARTING CLT, AND CLIMBING THROUGH FL170,FIRE WAS REPORTED TO BE COMING FROM THE FORWARD GALLEY OVEN. THE FIRE WAS EXTINGUISHED USING A PORTABLE FIRE EXTINGUISHER. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCSDR USAASA00042Unknown · odorLAX-CLT - FLT 34 - AN ELECTRICAL ODOR WAS NOTICED DURING FLIGHT. THE ODOR DISSIPATED AFTER SEVERAL MINUTES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE E/E COMPARTMENT, OXYGEN COMPARTMENT, AIR CONDITIONING PACKS INLET AND EXHAUST AREA, APU ISDR USAASA00030Switch · leakingBWI-PIT - FLT 179 - OIL ODOR WAS PRESENT IN CABIN AND COCKPIT DURING FLIGHT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A LEAKING APU LOW OIL PRESSURE SWITCH AND RAN PACKS TO PURGE OIL FROM THE SYSTEM. OK FOR SERVICE. (M)SDR USAASA00028Unknown · odorDCA-PVD - FLT 1928 - DURING THE FLIGHT, RECEIVED THE ECAM MESSAGE SMOKE-LAV SMOKE, FOR LESS THAN ONE-HALF A SECOND. ALSO, NOTICED A SLIGHT ODOR OF OIL IN AIRCRAFT CABIN/COCKPIT. MAINTENANCE PERFORMED A BITE CHECK OF THE CIDS SYSTEM. ALSO, RAN THE APU AND AISDR USAASA00005Oven · contaminatedPIT-LAX - FLT 5 - EN ROUTE THE CREW REPORTED AN ELECTRICAL SMELL AND THE SMELL OF MELTING PLASTIC IN THE FORWARD GALLEY. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FORWARD OVEN FOR PLASTIC ON THE HEATING ELEMENT,SDR USAASA99005Slide · low pressurePHL - THE 'EMERG R' MESSAGE APPEARED ON THE CIDS DURING THE OVERNIGHT MAINTENANCE CHECK. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY SLIDE PRESSURE BOTTLE. (X)
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