N102UW

Service difficulty reports · 370

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 = 'N102UW' 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.

SDR USAASA04069Flow Valve · failedGJT - FLT 82 - EN ROUTE SFO-PHL, WITH THE NR 2 PACK ON MEL, A NR 1 PACK FAULT OCCURRED. PRESSURIZATION WAS LOST AS A RESULT. FLIGHT MADE A RAPID DESCENT TO 10,000 FEET THE DIVERTED TO GJT DUE TO TERRAIN CONTRAINTS. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. Jul 5, 2004 · N102UW · Airbus A320214 · Cabin Cooling SystemSDR USAA040251Sill · corrodedSILL, 2.0 INCH X 1.0 INCH X 0.06 INCH AREA, CORRODED. BETWEEN FR 66 & 68, BL Y11371, WL Z240. INSTALLED NEW SILL IAW SRM.Jun 4, 2004 · N102UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040255Sill · corrodedDOOR SILL, 1.0 INCH X 1.5 INCH X 0.07 INCH DEEP, CORROSION; LEVEL 2; FR 66 TO 68, -Y 1524, Z-240. REPLACED DOOR SILL IWA SRM.May 28, 2004 · N102UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040254Floorbeam · corrodedFLOORBEAM, 2.5 INCH X 1.5 INCH X .030 INCH DEEP, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 28, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040253Angle · corrodedANGLE CORROSION, 2.0 INCH X 2.0 INCH X .02 INCH DEEP. REMOVED AND REPLACED PART IAW SRM.May 27, 2004 · N102UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040252Plate · corrodedPLATE CORROSION, 4 INCH X 4 INCH X .70 INCH DEEP. REMOVED AND REPLACED PORT IAW SRM.May 27, 2004 · N102UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040249Floorbeam · corrodedFLOORBEAM, 2.0 INCH X 2.0 INCH X .025 INCH D, BETWEEN FR 68-69, Y1270, Z240, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 26, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040248Floorbeam · corrodedFLOORBEAM, 2.0 INCH X 2.0 INCH X .035 INCH D, CORROSION BETWEEN FR 64 &66, +Y 1270, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 26, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040247Floorbeam · corrodedFLOORBEAM, 3.0 INCH X 1.5 INCH X .03 INCH AREA. CORROSION; LEVEL 2. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 26, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040250Seat Track · corrodedSEAT TRACK, 5.45 INCH X 0.813 INCH X .047 INCH D, CORROSION, FR17 AT Y 1270, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM.May 25, 2004 · N102UW · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040260Pad · corrodedADAPTER PAD, 11 INCH X 2 INCH X 0.050 INCH, CORROSION; LEVEL 2; AFT GIRT BAR FITTING, R1 DOOR, FR 19-20, Z240, Y1293. REPLACED PORT GIRT BAR FITTING ADAPTER IAW SRM.May 24, 2004 · N102UW · Airbus A320214 · Escape SlideSDR USAA040259Floorbeam · corrodedFLOORBEAM, 1.5 INCH X 1.0 INCH X .02 INCH DEEP, CORROSION; LEVEL 2; FR 66-68, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 22, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040256Floorbeam · corrodedFLOORBEAM, 1.0 INCH X 1.0 INCH X .03 INCH D, CORROSION; LEVEL 2; FR64-66, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 22, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040258Floorbeam · corrodedFLOORBEAM, 3.0 INCH X 2.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FR66-68, +Y762,Z240. REPLACED FLOORBEAM IAW SRM.May 21, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040257Floorbeam · corrodedFLOORBEAM, 1.0 INCH X 1.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FRAME 64 & 66, +Y787, Z240.May 21, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAASA03123Battery · failedFORWARD LEFT EPSU FAILED TEST. MAINTENANCE REPLACED THE EPSU BATTERY. (M)Oct 18, 2003 · N102UW · Airbus A320214 · Emergency LightingSDR USAASA03124Power Supply · inoperativeLEFT CENTER EPSU FAILED TEST. MAINTENANCE REPLACED THE EPSU. (M)Oct 18, 2003 · N102UW · Airbus A320214 · Emergency LightingSDR USAASA03088Slide · defectivePHL - RECEIVED 'EPSU EXT LOAD AFT L' FAULT DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE AFT LEFT SERVICE DOOR EMERGENCY ESCAPE SLIDE. OPERATIONALLY CHECKS OK. (M)Aug 9, 2003 · N102UW · Airbus A320214 · Escape SlideSDR USAASA03087Battery · dischargedPHL - THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND DISCHARGED. MAINTENANCE REPLACED THE BATTERY ON THE RIGHT OVERWING EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)Aug 9, 2003 · N102UW · Airbus A320214 · Emergency LightingSDR USAASA01041Windshield · crackedDCA - FLT 6875 - EN ROUTE LGA-DCA, WHILE CLIMBING THROUGH FL180, THE CAPTAINS WINDSHIELD OUTER PANEL SHATTERED, ACCOMPANIED WITH BRIEF ARCING. QRH PROCEDURES WERE FOLLOWED. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAug 4, 2001 · N102UW · Airbus A330202 · Window/Windshield System
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