N101UW, cancelled Oct 28, 2005

Service difficulty reports · 28

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 = 'N101UW' AND deregistration_id = 'N101UW-2005-10-28'
  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 USAA050153Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, FR 66 (Y765). INSTALLED REPAIR ANGLES IAW EA 96224. (M)Jan 26, 2005 · N101UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAASA04068Wire · brokenPHL - DURING THE WEEKLY CHECK, FOUND THE EMERGENCY LIGHT AT ROW 19ABC INOPERATIVE. MAINTENANCE REPAIRED THE BROKEN PIN/WIRE UNDER THE SEAT. OPS CHECKS GOOD. (M)Jul 5, 2004 · N101UW · Airbus A320214 · Light System WiringSDR USAASA04067Light · inoperativePHL - DURING WEEKLY CHECK, FOUND THE EMERGENCY LIGHT AT ROW 8ABC INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECKS OK. (M)Jul 5, 2004 · N101UW · Airbus A320214 · Emergency LightingSDR USAASA04049Ring · leakingPIT - FLT 127 - EN ROUTE PHL-SAN, WITHT NE NR 2 ENGINE INTEGRATED DRIVE GENERATOR IDG ON MINIMUM EQUIPMENT LIST MEL, THE AUXILIARY POWER UNIT APU, SHUTDOWN DURING FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NRMay 14, 2004 · N101UW · Airbus A320214 · APU Core EngineSDR USA2004F00035Apu · shutdownENROUTE, WITH THE NR 2 ENGINE INTEGRATED DRIVE GEN (IDG) ON MINIMUM EQUIPMENT LIST (MEL), THE AUXILARY POWER UNIT (APU) SHUT DOWN DURING FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACE THE NR 2 ENGINE IDG AND REMOVED MMay 14, 2004 · N101UW · Airbus A320214 · APU Oil SystemSDR USAA040178Seat Track · corrodedSEAT TRACK, 1.5 INCH X 1.3 INCH X .032 INCH DEEP. CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y765, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-11-14, 51-42-11.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040177Web · corrodedWEB, 3 INCHES L X 2INCHES W X .020 INCHES D, CORROSION, LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 69-70 + Y1244.6, Z240. REMOVED AND REPLACED WEB IAW SRM 51-74-00, 53-00-14, 51-42-11.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040176Floor Support · corrodedFLOOR SUPPORT, .8 INCH X .6 INCH X .030 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y254, Z240. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-74-00, 53-11-14, 51-21-11, 51-75-12.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040175Floor Support · corrodedFLOOR SUPPORT, 1.9 INCHES X .6 INCH X .040 INCH DEEP AREA, CORROSION; LEVEL 2, TASK NR JA-220-53500, FR 22, Y254, Z240. INSTALLED REPAIR ANGLE AND FILLER, REMOVED DAMAGE IAW SRM 51-74-00, 51-21-11, 51-75-12.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040174Sill · corrodedSILL, 4.25 INCHES X 2.5 INCHES X .042 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 66, Z240, Y1972. REMOVED AND REPLACED SILL IAW SRM 51-74-00, 53-41-14, 51-42-11.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040172Floor Panel · delaminatedFLOOR PANEL, 6 INCHES X .2500 INCH W, DELAMINATION, FLOOR PANEL NR 241 AF, FR 34 AND 35 AT Y24, Z240. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor PanelSDR USAA040171Floor Panel · delaminatedFLOOR PANEL 4 INCH X 4 INCH AREA, DELAMINATION, 31.25 CM FWD OF FR 68, Y 756.25. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor PanelSDR USAA040170Floor Panel · delaminatedFLOOR PANEL, 4.5 INCH X 5.5 INCH OB AFT CORNER, DELAMINATION FR 66, Y1182, FLOOR PANEL 261 HG. NEW PANEL FABRICATED IAW SRM 53-02-00, FIG 309.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor PanelSDR USAA040165Floor Support · corrodedFLOOR SUPPORT, 1.3 INCHES X .90 INCH X .021 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON - FR 16, Y-254. INSTALLED FILLER AND REPAIR ANGLES IAW SRM 53-11-14, FIG 201.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040164Floor Support · corrodedFLOOR SUPPORT, 1.8 INCH X .70 INCH X .037 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON-FR 20, Y-254. INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-00-14, FIG 204.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040166Track · corrodedTRACK, 3.5 INCHES X 3.5 INCHES X .170 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 64 TO 70, Y736.6, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-14, 51-42-11, 51-71-12.Apr 27, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040167Seat Track · corrodedSEAT TRACK, 2 INCHES X 1 INCH X .100 INCHES AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 20, Y-1292, Z240. REMOVED AND REPLACED TRACK IAW SRM.Apr 26, 2004 · N101UW · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040173Floorbeam · corrodedFLOORBEAM, 1.0 INCH L X 1.5 INCH W X .022 INCH D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 65-68, -Y 1244.6, Z240. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-00-14 & 51-42-11.Apr 25, 2004 · N101UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040169Floor Support · corrodedFLOOR SUPPORT, 1.5 INCH L X 1 INCH W X .030 INCHES D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 TWO AREAS FLOOR SUPPORT, FR 64-68 AT Y1244.6, Z240. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW 53-00-14, 51-42-11.Apr 25, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040168Floor Support · corrodedFLOOR SUPPORT, 3 INCHES X 1.5 INCHES W X .020 INCH D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 FLOOR SUPPORT BETWEEN FR 68 AND 69 AT Y1244.6, Z240. REMOVED AND REPLACED NEW FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14.Apr 24, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040163Floor Support · corrodedFLOOR SUPPORT BETWEEN FRAME 68 AND 69 AT Y1244.6, Z240. CORROSION: LEVEL 2; TASK NR JA-250-53500. REMOVED AND REPLACED NEW FLOORBEAM.Apr 24, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAASA03018Power Supply · malfunctionedDCA - WHEN THE 'NO SMK/PED' SWITCH IS TURNED OFF, THE RIGHT OVERWING EXIT SIGN AND OVERHEAD EMERGENCY LIGHTS FLASH ON AND OFF INTERMITTENTLY. WHEN THE 'NO SMK/PED' SWITCH IS TURNED ON, THE RIGHT EXIT LEFT OVERWING SIGN IS OFF. MAINTENANCE REPLACED THE RIGHT Feb 20, 2003 · N101UW · Airbus A320214 · Emergency LightingSDR USAASA03014Battery Pack · inoperativeCLT - DURING THE WEEKLY CHECK, THE RIGHT WING BATTERY PACK FOR THE EMERGENCY LIGHTS WAS FOUND FAULTY. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECK OK. (M)Feb 11, 2003 · N101UW · Airbus A320214 · Emergency LightingSDR USAASA02117Power Supply · dischargedPHL - THE EMERGENCY LIGHTS FLASH ON AND OFF. MAINTENANCE REPLACED A BATTERY PACK AND THE 'A' CHANNEL AND 'B' CHANNEL DECODER/ENCODER UNITS, AND PERFORMED A CABIN INTERCOMMUNICATION DATE SYSTEM RESET FOR TROUBLESHOOTING. MAINTENANCE REPLACED AN EMERGENCY POWEDec 31, 2002 · N101UW · Airbus A320214 · Emergency LightingSDR USAASA02109Socket · looseTPA - FOUND EMERGENCY LIGHTS IN AFT GALLEY INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY CEILING LIGHT, FIN 207WL, DUE TO AN INTERMITTENTLY LOOSE SOCKET. OPERATIONALLY CHECKS OK. (M)Dec 13, 2002 · N101UW · Airbus A320214 · Emergency LightingSDR USA2002F00035Sensor · faultyEN ROUTE, AFTER DEPARTING, RECEIVED BOTH RED AND GREEN LANDING GEAR INDICATIONS. THE CREW RECYCLED THE GEAR AND CONTINUED, WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SENSOR 34GA. OPERATIONALLY CHECKED OK.May 24, 2002 · N101UW · Airbus A320214 · Landing Gear Position and WarningSDR USAASA01053Connector · disconnectedTPA - RECEIVED 'EPSU EX LOAD FORWARD L ER LOAD AFT LT' FAULT DURING CHECK. MAINTENANCE RECONNECTED THE AFT LEFT EMERGENCY ESCAPE SLIDE LIGHT CONNECTOR. OPS CHECKED NORMAL. (M)Oct 6, 2001 · N101UW · Airbus A320214 · Light System WiringSDR USAASA00003Wire · brokenLAX - THE EMERGENCY LIGHT AT ROW 1A WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE WALL CONNECTOR. (M)Jan 14, 2000 · N101UW · Airbus A320214 · Light System Wiring
Back to N101UW, cancelled Oct 28, 2005