# N101UW: 1998 Airbus Industrie A320-214, registration cancelled 2005-10-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 28, 2005
- Exported to: Philippines
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-214](https://openairdocs.org/model/airbus-industrie-a320-214) (registry code 3930316)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 0936
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 26, 1999
- Certificate issued: November 21, 2003
- Last registry action: November 21, 2003
- Mode S code: A00A42
- Owner when cancelled: [Afs Investments 59 LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%2059%20LLC)
- Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford)
- Owner type: Corporation
- Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N101UW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=101UW
- Page: https://openairdocs.org/deregistered/N101UW-2005-10-28

From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Airbus Industrie A320-214: https://openairdocs.org/model/airbus-industrie-a320-214.md

## Service difficulty reports (28)

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

- [SDR USAA050153](https://openairdocs.org/sdr/USAA050153), Jan 26, 2005: FLOORBEAM. CORRODED. 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), Jul 5, 2004: WIRE. BROKEN. 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), Jul 5, 2004: LIGHT. INOPERATIVE. 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), May 14, 2004: RING. LEAKING. 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 DURI
- [SDR USA2004F00035](https://openairdocs.org/sdr/USA2004F00035), May 14, 2004: APU. SHUTDOWN. 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
- [SDR USAA040178](https://openairdocs.org/sdr/USAA040178), Apr 29, 2004: SEAT TRACK. CORRODED. 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,
- [SDR USAA040177](https://openairdocs.org/sdr/USAA040177), Apr 29, 2004: WEB. CORRODED. 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 51-74-0
- [SDR USAA040176](https://openairdocs.org/sdr/USAA040176), Apr 29, 2004: FLOOR SUPPORT. CORRODED. 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-
- [SDR USAA040175](https://openairdocs.org/sdr/USAA040175), Apr 29, 2004: FLOOR SUPPORT. CORRODED. 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, REMOV
- [SDR USAA040174](https://openairdocs.org/sdr/USAA040174), Apr 29, 2004: SILL. CORRODED. 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, 
- [SDR USAA040172](https://openairdocs.org/sdr/USAA040172), Apr 28, 2004: FLOOR PANEL. DELAMINATED. 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. FABR
- [SDR USAA040171](https://openairdocs.org/sdr/USAA040171), Apr 28, 2004: FLOOR PANEL. DELAMINATED. 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), Apr 28, 2004: FLOOR PANEL. DELAMINATED. 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), Apr 28, 2004: FLOOR SUPPORT. CORRODED. 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 
- [SDR USAA040164](https://openairdocs.org/sdr/USAA040164), Apr 28, 2004: FLOOR SUPPORT. CORRODED. 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 5
- [SDR USAA040166](https://openairdocs.org/sdr/USAA040166), Apr 27, 2004: TRACK. CORRODED. 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 TR
- [SDR USAA040167](https://openairdocs.org/sdr/USAA040167), Apr 26, 2004: SEAT TRACK. CORRODED. 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), Apr 25, 2004: FLOORBEAM. CORRODED. 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 I
- [SDR USAA040169](https://openairdocs.org/sdr/USAA040169), Apr 25, 2004: FLOOR SUPPORT. CORRODED. 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. DEFECTIV
- [SDR USAA040168](https://openairdocs.org/sdr/USAA040168), Apr 24, 2004: FLOOR SUPPORT. CORRODED. 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
- [SDR USAA040163](https://openairdocs.org/sdr/USAA040163), Apr 24, 2004: FLOOR SUPPORT. CORRODED. 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), Feb 20, 2003: POWER SUPPLY. MALFUNCTIONED. 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/P
- [SDR USAASA03014](https://openairdocs.org/sdr/USAASA03014), Feb 11, 2003: BATTERY PACK. INOPERATIVE. CLT - DURING THE WEEKLY CHECK, THE RIGHT WING BATTERY PACK FOR THE EMERGENCY LIGHTS WAS FOUND FAULTY. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECK
- [SDR USAASA02117](https://openairdocs.org/sdr/USAASA02117), Dec 31, 2002: POWER SUPPLY. DISCHARGED. 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 CABI
- [SDR USAASA02109](https://openairdocs.org/sdr/USAASA02109), Dec 13, 2002: SOCKET. LOOSE. TPA - FOUND EMERGENCY LIGHTS IN AFT GALLEY INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY CEILING LIGHT, FIN 207WL, DUE TO AN INTERMITTENTLY LOOSE SOCKET. 
- [SDR USA2002F00035](https://openairdocs.org/sdr/USA2002F00035), May 24, 2002: SENSOR. FAULTY. EN ROUTE, AFTER DEPARTING, RECEIVED BOTH RED AND GREEN LANDING GEAR INDICATIONS. THE CREW RECYCLED THE GEAR AND CONTINUED, WHERE THE AIRCRAFT LANDED WITHOUT FUR
- [SDR USAASA01053](https://openairdocs.org/sdr/USAASA01053), Oct 6, 2001: CONNECTOR. DISCONNECTED. 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 CHEC
- [SDR USAASA00003](https://openairdocs.org/sdr/USAASA00003), Jan 14, 2000: WIRE. BROKEN. LAX - THE EMERGENCY LIGHT AT ROW 1A WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE WALL CONNECTOR. (M)

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