# Service difficulty reports: N101UW, cancelled Oct 28, 2005

A list on [N101UW, cancelled Oct 28, 2005](https://openairdocs.org/deregistered/N101UW-2005-10-28.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR USAA050153](https://openairdocs.org/sdr/USAA050153.md): Floorbeam · corroded · Jan 26, 2005 · N101UW · Airbus A320214 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, FR 66 (Y765). INSTALLED REPAIR ANGLES IAW EA 96224. (M)
- [SDR USAASA04068](https://openairdocs.org/sdr/USAASA04068.md): Wire · broken · Jul 5, 2004 · N101UW · Airbus A320214 · Light System Wiring
  > PHL - 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)
- [SDR USAASA04067](https://openairdocs.org/sdr/USAASA04067.md): Light · inoperative · Jul 5, 2004 · N101UW · Airbus A320214 · Emergency Lighting
  > PHL - DURING WEEKLY CHECK, FOUND THE EMERGENCY LIGHT AT ROW 8ABC INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECKS OK. (M)
- [SDR USAASA04049](https://openairdocs.org/sdr/USAASA04049.md): Ring · leaking · May 14, 2004 · N101UW · Airbus A320214 · APU Core Engine
  > PIT - 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 NR
- [SDR USA2004F00035](https://openairdocs.org/sdr/USA2004F00035.md): Apu · shutdown · May 14, 2004 · N101UW · Airbus A320214 · APU Oil System
  > ENROUTE, 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 M
- [SDR USAA040178](https://openairdocs.org/sdr/USAA040178.md): Seat Track · corroded · Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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.
- [SDR USAA040177](https://openairdocs.org/sdr/USAA040177.md): Web · corroded · Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > WEB, 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.
- [SDR USAA040176](https://openairdocs.org/sdr/USAA040176.md): Floor Support · corroded · Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR USAA040175](https://openairdocs.org/sdr/USAA040175.md): Floor Support · corroded · Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR USAA040174](https://openairdocs.org/sdr/USAA040174.md): Sill · corroded · Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > SILL, 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.
- [SDR USAA040172](https://openairdocs.org/sdr/USAA040172.md): Floor Panel · delaminated · Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor Panel
  > FLOOR 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.
- [SDR USAA040171](https://openairdocs.org/sdr/USAA040171.md): Floor Panel · delaminated · Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor Panel
  > FLOOR 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.
- [SDR USAA040170](https://openairdocs.org/sdr/USAA040170.md): Floor Panel · delaminated · Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor Panel
  > FLOOR 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.
- [SDR USAA040165](https://openairdocs.org/sdr/USAA040165.md): Floor Support · corroded · Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR USAA040164](https://openairdocs.org/sdr/USAA040164.md): Floor Support · corroded · Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR USAA040166](https://openairdocs.org/sdr/USAA040166.md): Track · corroded · Apr 27, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > TRACK, 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.
- [SDR USAA040167](https://openairdocs.org/sdr/USAA040167.md): Seat Track · corroded · Apr 26, 2004 · N101UW · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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.
- [SDR USAA040173](https://openairdocs.org/sdr/USAA040173.md): Floorbeam · corroded · Apr 25, 2004 · N101UW · Airbus A320214 · Fuselage Main, Floor Beam
  > FLOORBEAM, 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.
- [SDR USAA040169](https://openairdocs.org/sdr/USAA040169.md): Floor Support · corroded · Apr 25, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR USAA040168](https://openairdocs.org/sdr/USAA040168.md): Floor Support · corroded · Apr 24, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR 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.
- [SDR USAA040163](https://openairdocs.org/sdr/USAA040163.md): Floor Support · corroded · Apr 24, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BETWEEN FRAME 68 AND 69 AT Y1244.6, Z240. CORROSION: LEVEL 2; TASK NR JA-250-53500. REMOVED AND REPLACED NEW FLOORBEAM.
- [SDR USAASA03018](https://openairdocs.org/sdr/USAASA03018.md): Power Supply · malfunctioned · Feb 20, 2003 · N101UW · Airbus A320214 · Emergency Lighting
  > DCA - 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
- [SDR USAASA03014](https://openairdocs.org/sdr/USAASA03014.md): Battery Pack · inoperative · Feb 11, 2003 · N101UW · Airbus A320214 · Emergency Lighting
  > CLT - 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)
- [SDR USAASA02117](https://openairdocs.org/sdr/USAASA02117.md): Power Supply · discharged · Dec 31, 2002 · N101UW · Airbus A320214 · Emergency Lighting
  > PHL - 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 POWE
- [SDR USAASA02109](https://openairdocs.org/sdr/USAASA02109.md): Socket · loose · Dec 13, 2002 · N101UW · Airbus A320214 · Emergency Lighting
  > TPA - 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)
- [SDR USA2002F00035](https://openairdocs.org/sdr/USA2002F00035.md): Sensor · faulty · May 24, 2002 · N101UW · Airbus A320214 · Landing Gear Position and Warning
  > EN 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.
- [SDR USAASA01053](https://openairdocs.org/sdr/USAASA01053.md): Connector · disconnected · Oct 6, 2001 · N101UW · Airbus A320214 · Light System Wiring
  > TPA - 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)
- [SDR USAASA00003](https://openairdocs.org/sdr/USAASA00003.md): Wire · broken · Jan 14, 2000 · N101UW · Airbus A320214 · Light System Wiring
  > LAX - THE EMERGENCY LIGHT AT ROW 1A WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE WALL CONNECTOR. (M)

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N101UW-2005-10-28/reports

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