# N113UW: 1999 Airbus Industrie A320-214, registration cancelled 2019-09-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 4, 2019
- 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: 1141
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 4, 2000
- Certificate issued: December 30, 2015
- Last registry action: July 31, 2019
- Mode S code: A0392F
- Owner when cancelled: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC)
- Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)
- Owner type: Corporation
- Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N113UW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=113UW
- Page: https://openairdocs.org/deregistered/N113UW-2019-09-04

From the FAA registry file of November 5, 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 (156, newest 50)

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

- [SDR USAA2014031400012](https://openairdocs.org/sdr/USAA2014031400012), Mar 13, 2014: TIRE. BLOWN. ABORTED TAKEOFF AFTER BLOWN NOSE TIRES. INVESTIGATING, SUPPLEMENTAL TO FOLLOW.
- [SDR USAA2014022400004](https://openairdocs.org/sdr/USAA2014022400004), Feb 23, 2014: MEGAPHONE. INOPERATIVE. AFT MEGA PHONE INOPERATIVE. REPLACED AFT MEGA PHONE, OK FOR SERVICE.
- [SDR USAA2013090500002](https://openairdocs.org/sdr/USAA2013090500002), Sep 4, 2013: BATTERY. INOPERATIVE. FLASHLIGHT AT L2 INOPERATIVE. REPLACED BATTERY.
- [SDR USAA2013061400002](https://openairdocs.org/sdr/USAA2013061400002), Jun 13, 2013: COVER. BROKEN. CLEAR EXIT LIGHT COVER BROKEN, 2R DOOR. REINSTALLED COVER FOR EXIT LIGHT AT 2R DOOR.
- [SDR USAA2013052300005](https://openairdocs.org/sdr/USAA2013052300005), May 22, 2013: LENS. MISSING. EXIT ROW LIGHTING ON SEAT 1A IS INOPERATIVE. REPLACED LENS COVER AT SEAT 1A, EMERGENCY LIGHTS OPERATES NORMALLY.
- [SDR USAA2013050800006](https://openairdocs.org/sdr/USAA2013050800006), May 7, 2013: LENS. MISSING. EMERGENCY LIGHT COVERS MISSING 1C & 3C. REPLACED LENS COVERS ON SEATS 1C AND 3C.
- [SDR USAA2013031800008](https://openairdocs.org/sdr/USAA2013031800008), Mar 16, 2013: LENS. MISSING. FIRST CLASS SEAT 3AC MISSING EMERGENCY LIGHT LENS. INSTALLED LENS ON FIRST CLASS SEAT 3AC. OPERATIONAL CHECK GOOD.
- [SDR USAA2013022500004](https://openairdocs.org/sdr/USAA2013022500004), Feb 22, 2013: LENS. BROKEN. SEAT 1C FLOOR EXIT LIGHT COVER BROKEN OFF. INSTALLED NEW LENS COVER ON SEAT 3C.
- [SDR USAA2012091800003](https://openairdocs.org/sdr/USAA2012091800003), Jun 28, 2012: AIR DATA MODULE. FAULTY. CAPTAIN REPORTED NO AIRSPEED INDICATION ON TAKEOFF ROLL. REJECTED TAKEOFF AT 80 KTS. REMOVED AND REPLACED NR 8 AIR DATA MODULE IAW AIRBUS MAINTENANCE MANUAL 34-
- [SDR USAA2012091800002](https://openairdocs.org/sdr/USAA2012091800002), Jun 28, 2012: AIR DATA MODULE. FAULTY. CAPTAIN REPORTED NO AIRSPEED INDICATION ON TAKEOFF ROLL. REJECTED TAKEOFF AT 80 KTS. REMOVED AND REPLACED NR 4 AIR DATA MODULE IAW AIRBUS MAINTENANCE MANUAL 34-
- [SDR USAA2012062900018](https://openairdocs.org/sdr/USAA2012062900018), Jun 28, 2012: PITOT TUBE. FAULTY. CAPTAIN REPORTED NO AIRSPEED INDICATION ON TAKEOFF ROLL. REJECTED TAKEOFF AT 80 KTS. REMOVED AND REPLACED CAPTAIN'S PITOT PROBE IAW AIRBUS MAINTENANCE MANUAL 34
- [SDR USAA2012060400019](https://openairdocs.org/sdr/USAA2012060400019), Jun 3, 2012: PLUG. LOOSE. UPON ARRIVAL AT GATE, TWO FLIGHT ATTENDANTS REPORTED FUMES DESCRIBED AS SCORCHING AND/OR VOMIT SMELL, AND SUFFERED BURNING / RED EYES, HEADACHE AND THROAT ISSUE
- [SDR USAA2011122700030](https://openairdocs.org/sdr/USAA2011122700030), Dec 23, 2011: LENS. BROKEN. EMERGENCY LIGHT LENS COVER BROKEN 11L. REMOVED AND REPLACED EMERGENCY LIGHT LENS 11L.
- [SDR USAA2011112500003](https://openairdocs.org/sdr/USAA2011112500003), Nov 24, 2011: RESERVOIR. FAILED. 2S CHECK, DURING OPERATIONAL TEST OF THE INFLATION RESERVOIR UTILIZING THE CIDS A FAILURE MESSAGE WAS RECIEVED FOR THE LEFT UNIT. REMOVED AND REPLACED THE LEFT 
- [SDR USAA2011112300028](https://openairdocs.org/sdr/USAA2011112300028), Nov 23, 2011: SLIDE RAFT. DEFECTIVE. 2S CHECK - OVER INFLATED SLIDE/RAFT AT DOOR 831. REPACKED SLIDE RAFT IAW A320 CMM 25-61-20 PAGE 309 SEC DISASSEMBLY AND FOLDING PROCEDURE P 11921.
- [SDR USAA2011112300001](https://openairdocs.org/sdr/USAA2011112300001), Nov 22, 2011: DAMPER. WEAK. 2S CHECK - DURING OPERATIONAL TEST DAMPING FUNCTION, BUFFER IMPACT HARD ON AIRCRAFT STRUCTURE AT DOOR 831. REPLACED DOOR-DAMPER & EMERGENCY OPERATION CYLINDER A
- [SDR USAA2011112200016](https://openairdocs.org/sdr/USAA2011112200016), Nov 21, 2011: SETSCREW. OUT OF ADJUST. 2S CHECK - OUT OF ADJUSTMENT RIGGING POINT OF REDUCER SHAFT BELLCRANK (UP POSITION) AT DOOR 831. PERFORMED ADJUSTMENT OF RIGGING POINT OF REDUCER SHAFT BELLCRAN
- [SDR USAA2011112200002](https://openairdocs.org/sdr/USAA2011112200002), Nov 21, 2011: SLIDE RAFT. DEFECTIVE. 2S CHECK - OVER INFLATED SLIDE/RAFT AT DOOR 832. REPACKED SLIDE/RAFT AT DOOR 832 IAW A320 CMM 25-61-20 PAGE 309 SEC. DISASSEMBLY & FOLDING PROCEDURE P-11915.
- [SDR USAA2011112200017](https://openairdocs.org/sdr/USAA2011112200017), Nov 20, 2011: BUSHING. WORN. 2S CHECK - EXCESSIVE PLAY IN UPPER CONNECTION LINK AT DOOR 832. REPLACED BUSHINGS IN UPPER CONNECTION LINK AT DOOR 832 IAW A320 AMM 52-10-00-915-001 PAR 4 STEP 
- [SDR USAA2011112100005](https://openairdocs.org/sdr/USAA2011112100005), Nov 19, 2011: DAMPER. DAMAGED. 2S CHECK - DURING OPERATIONAL TEST DAMPING FUNCTION BUFFER IMPACT HARD ON AIRCRAFT STRUCTURE AT DOOR 842. REPLACED DOOR DAMPER AND EMERGENCY-OPERATION CYLINDER 
- [SDR USAA2011111800001](https://openairdocs.org/sdr/USAA2011111800001), Nov 17, 2011: STRIKER. OUT OF ADJUST. 2S CHECK - OUT ADJUSTMENT AT DIMENSION 'B' BETWEEN FINGER & STRIKER LEVER AT DOOR 841. PERFORMED ADJUSTMENT DIMENSION "B" (J1) BETWEEN FINGER & STRIKER LEVER OF
- [SDR USAA2011111400020](https://openairdocs.org/sdr/USAA2011111400020), Nov 11, 2011: SLIDING WINDOW. BROKEN. 2S CHECK - BROKEN FRAME ON SLIDING WINDOW PANEL CAPTAINS SIDE. REPLACED SLIDING WINDOW PANE AT CAPTAINS SIDE IAW AMM 56-12-11. OPERATIONAL TEST OF THE WINDSHIEL
- [SDR USAA2011111000013](https://openairdocs.org/sdr/USAA2011111000013), Nov 9, 2011: STRIKER. OUT OF ADJUST. 2S CHECK - DOOR 831 IS OUT ADJUSTMENT AT DIMENSION B BETWEEN FINGER AND STRIKER LEVER AT DOOR 831. PERFORMED ADJUSTMENT AT DIMENSION B BETWEEN FINGER AND STRIKE
- [SDR USAA2011111600004](https://openairdocs.org/sdr/USAA2011111600004), Nov 6, 2011: PLATE. CORRODED. 2S CHECK - CORROSION ON CONNECTING SECTION AT FR68, -Y1162. REPLACED CONNECTING SECTION AT FR68, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53474250.
- [SDR USAA2011111500003](https://openairdocs.org/sdr/USAA2011111500003), Oct 26, 2011: ACCESS PANEL. CORRODED. 2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL ACCESS PANEL 540JB BETWEEN WS 7792 TO WS 8268, BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING FUEL ACCESS 
- [SDR USAA2011111500002](https://openairdocs.org/sdr/USAA2011111500002), Oct 26, 2011: ACCESS PANEL. CORRODED. 2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING FUEL ACCESS PANEL 540KB BETWEEN WS 8268 TO WS 8744, BETWEEN RIB 15 TO RIB 16. REPLACED LEFT WING FUEL ACCESS 
- [SDR USAA2011111100022](https://openairdocs.org/sdr/USAA2011111100022), Oct 26, 2011: SEAT TRACK. CORRODED. S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR27 TO FR29, -Y765. REPLACED SEAT TRACK BETWEEN FR27 TO FR29, -Y765 IAW A320 SRM 53-21-15.
- [SDR USAA2011111000031](https://openairdocs.org/sdr/USAA2011111000031), Oct 26, 2011: STRUT. CORRODED. 2S CHECK - CORROSION ON INTERCONNECT STRUT BETWEEN WS 375 TO WS 551 & BETWEEN RIB 7 TO RIB 10. REPLACED INTERCONNECT STRUT BETWEEN WS 375 TO WS 551 & BETWEEN RI
- [SDR USAA2011112300031](https://openairdocs.org/sdr/USAA2011112300031), Oct 25, 2011: ANGLE. CRACKED. 2S CHECK - MULTIPLE CRACKS IN SEGMENT ANGLE OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. ACCOMPLISHED MODIFICATION ON EMERGENCY E
- [SDR USAA2011112300030](https://openairdocs.org/sdr/USAA2011112300030), Oct 25, 2011: ANGLE. CRACKED. 2S CHECK - MULTIPLE CRACKS IN SEGMENT ANGLE OF EMERGENCY EXIT DOOR 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. ACCOMPLISHED MODIFICATION ON EMERGENCY E
- [SDR USAA2011112300029](https://openairdocs.org/sdr/USAA2011112300029), Oct 25, 2011: ANGLE. CRACKED. 2S CHECK - MULTIPLE CRACKS IN SEGMENT ANGLE OF EMERGENCY EXIT DOOR 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. ACCOMPLISHED MODIFICATION ON EMERGENCY E
- [SDR USAA2011112300004](https://openairdocs.org/sdr/USAA2011112300004), Oct 25, 2011: ANGLE. CRACKED. 2S CHECK - MULTIPLE CRACKS ON SEGMENT ANGLE OF EMERGENCY EXIT DOOR 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. REPLACED SEGMENT ANGLE OF EMERGENCY EXIT
- [SDR USAA2011110800012](https://openairdocs.org/sdr/USAA2011110800012), Oct 24, 2011: SUPPORT. CORRODED. S2 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23L. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11 & AIR
- [SDR USAA2011110400022](https://openairdocs.org/sdr/USAA2011110400022), Oct 24, 2011: HINGE PIN. CORRODED. 2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 1 SPOILER CENTER HINGE PIN. REPLACED LEFT WING NR 1 SPOILER CENTER HINGE PIN IAW A320 AMM 27-64-41-400-001
- [SDR USAA2011111000005](https://openairdocs.org/sdr/USAA2011111000005), Oct 23, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 212EF BETWEEN FR6 TO FR12 & BETWEEN -Y254 TO -Y765. REPLACED FLOOR PANEL 212EF IAW A320 SRM 53-12-00 & IRM 9701 REV G.
- [SDR USAA2011112300003](https://openairdocs.org/sdr/USAA2011112300003), Oct 22, 2011: DOOR FRAME. CORRODED. 2S CHECK - LEVEL 2 GALVANIC CORROSION ON INTERNAL AREA OF LOWER CURVED EDGE OF EMERGENCY EXIT DOOR 844 AT FR39, BEAM 4. REPLACED LOWER CURVED EDGE OF INTERNAL A
- [SDR USAA2011112300002](https://openairdocs.org/sdr/USAA2011112300002), Oct 22, 2011: DOOR FRAME. CORRODED. 2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER CURVED EDGE OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41, BEAM 4. REPLACED LOWER CURVED EDGE OF EMERGENCY EXIT
- [SDR USAA2011112200013](https://openairdocs.org/sdr/USAA2011112200013), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR20 TO FR24, BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232DF IAW TYPICAL REPAIR 320-2528-10-0011 & A320
- [SDR USAA2011112100010](https://openairdocs.org/sdr/USAA2011112100010), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 262BF BETWEEN FR64 TO FR66, BETWEEN -Y1732 TO Y765. REPLACED FLOOR PANEL 262BF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 
- [SDR USAA2011112100008](https://openairdocs.org/sdr/USAA2011112100008), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 222CF BETWEEN FR16 TO FR20, Y-1732 TO -Y254. REPLACED FLOOR PANEL 222CF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 REV G.
- [SDR USAA2011111600013](https://openairdocs.org/sdr/USAA2011111600013), Oct 22, 2011: FLOOR PANEL. CORRODED. 2S CHECK - CORROSION ON FLOOR PANEL 262FF AT FR66 TO FR68, S20L, -Y1732. REPLACED FLOOR PANEL 262FF IAW A320 SRM 53-42-12 & 51-72-11.
- [SDR USAA2011111000030](https://openairdocs.org/sdr/USAA2011111000030), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO Y254. REPLACED FLOOR PANEL 221EF IAW A320 SRM 53-12-00 AND MCGILL IRM 9701 
- [SDR USAA2011111000029](https://openairdocs.org/sdr/USAA2011111000029), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 232EF BETWEEN FR20 TO FR24 & BETWEEN -Y1242 TO -Y765. REPLACED FLOOR PANEL 232EF IAW A320 53-12-00 AND MCGILL IRM 9701 RE
- [SDR USAA2011111000014](https://openairdocs.org/sdr/USAA2011111000014), Oct 22, 2011: FLOOR PANEL. CORRODED. 2S CHECK - CORROSION ON FLOOR PANEL NR 222FF BETWEEN FR16 TO FR20, S23R, -Y1732. REPLACED FLOOR PANEL NR 222FF IAW A320 AMM 53-12-12-400-001 & JOB CARD 26C22053
- [SDR USAA2011111000006](https://openairdocs.org/sdr/USAA2011111000006), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 231BF BETWEEN FR20 TO FR24 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 231BF IAW A320 SRM 53-12-00 & IRM 9701 REV G.
- [SDR USAA2011111000004](https://openairdocs.org/sdr/USAA2011111000004), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN Y1242 TO -Y1242. REPLACED FLOOR PANEL 261PF IAW A320 SRM 53-12-00 & IRM 9701 REV G.
- [SDR USAA2011110900017](https://openairdocs.org/sdr/USAA2011110900017), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR20 TO FR24 & BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232FF IAW A320 SRM 53-12-00 & IRM 9701 REV G.
- [SDR USAA2011110900016](https://openairdocs.org/sdr/USAA2011110900016), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 221DF BETWEEN FR16 TO FR20 & BETWEEN Y254 TO -Y254. REPLACED FLOOR PANEL 221DF IAW A320 SRM 53-12-00 & IRM 9701 REV G.
- [SDR USAA2011110900015](https://openairdocs.org/sdr/USAA2011110900015), Oct 22, 2011: FLOOR PANEL. DELAMINATED. 2S CHECK - DELAMINATION ON FLOOR PANEL 231CF BETWEEN FR20 TO FR24 & BETWEEN Y765 TO Y254. REPLACED FLOOR PANEL 231CF IAW A320 SRM 53-12-00 & IRM 9701 REV G.
- [SDR USAA2011110900011](https://openairdocs.org/sdr/USAA2011110900011), Oct 22, 2011: FLOOR PANEL. CORRODED. 2S CHECK - CORROSION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20, S23L, Y1732. REPLACED FLOOR PANEL 221FF IAW A320 AMM 53-12-12-400-001 & JOB CARD 26C22053014.

All 156: https://openairdocs.org/deregistered/N113UW-2019-09-04/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA14MA081](https://openairdocs.org/ntsb/DCA14MA081), Mar 13, 2014: Airbus A320 - 214 (N113UW), Philadelphia, PA, substantial damage. Probable cause: the captain's decision to reject the takeoff after the airplane had rotated. Contributing to the accident was the flight crew's failure to follow standard operating procedures by not verifying that…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20140313003339A](https://openairdocs.org/incident/20140313003339A), Mar 13, 2014: Airbus Industrie A320-214 (N113UW), Philadelphia, PA, Substantial damage. As the crew taxied onto the runway for departure the captain noticed that the wrong departure runway (27R) was displayed on his navigation display (ND). The…

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