# N620AW: 1989 Airbus Industrie A320-231, registration cancelled 2015-06-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 18, 2015
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (registry code 3930325)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 052
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: August 31, 1989
- Certificate issued: December 19, 1994
- Last registry action: January 17, 2013
- Mode S code: A81652
- Owner when cancelled: [Wilmington Trust Co Owner Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20OWNER%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N620AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=620AW
- Page: https://openairdocs.org/deregistered/N620AW-2015-06-18

From the FAA registry file of October 29, 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 A320-231: https://openairdocs.org/model/airbus-industrie-a320-231.md

## Service difficulty reports (195, newest 50)

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

- [SDR USAA2014081500005](https://openairdocs.org/sdr/USAA2014081500005), Aug 14, 2014: BOTTLE. LOW PRESSURE. L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.
- [SDR USAA2014052700043](https://openairdocs.org/sdr/USAA2014052700043), May 23, 2014: CYLINDER. LOW PRESSURE. L2 DOOR ASSIST BOTTLE PRESS LOW. SERVICED L2 DOOR ASSIST BOTTLE.
- [SDR USAA2014050200003](https://openairdocs.org/sdr/USAA2014050200003), May 1, 2014: HINGE FITTING. CHAFED. C1 CHECK CHAFING DAMAGE ON LT MLG FWD DOOR HINGE FITTING APPROX 3 INCHES AFT OF LE AT DOOR ACTUATOR ATTACH POINT UPPER END. REPLACED LT MLG FWD DOOR HINGE FITTI
- [SDR USAA2014042800018](https://openairdocs.org/sdr/USAA2014042800018), Apr 27, 2014: SHEAR PLATE. CRACKED. C1 CHECK CRACK ON SHEAR PLATE TRAY BETWEEN FRAME 68 TO FRAME 69, Z-500, -Y 1292. REPLACED SHEAR PLATE TRAY BETWEEN FRAME 68 TO FRAME 69, Z-500, -Y 1292 IAW SRM 
- [SDR USAA2014042500010](https://openairdocs.org/sdr/USAA2014042500010), Apr 25, 2014: STRINGER. CORRODED. C1 CHECK CORROSION ON FUSELAGE STRINGER 26R BETWEEN FRAME 65 TO FRAME 66. REPAIRED FUSELAGE STRINGER 26R BETWEEN FRAME 65 TO FRAME 66 IAW EA 207361.
- [SDR USAA2014042500006](https://openairdocs.org/sdr/USAA2014042500006), Apr 24, 2014: FLOOR PANEL. DELAMINATED. C1 CHECK DELAMINATION ON FLOOR PANEL 231CF BETWEEN FRAME 20 TO FRAME 24, -Z500 & BETWEEN Y 254 TO Y 765. REPLACED FLOOR PANEL 231CF IAW 9701, REV G.
- [SDR USAA2014042500005](https://openairdocs.org/sdr/USAA2014042500005), Apr 24, 2014: FLOOR PANEL. DELAMINATED. C1 CHECK DELAMINATION ON FLOOR PANEL 222EF BETWEEN FRAME 16 TO FRAME 20, -Z500 & BETWEEN -Y 345 TO -Y 1292. REPLACED FLOOR PANEL 222EF IAW 9701, REV G.
- [SDR USAA2014042400010](https://openairdocs.org/sdr/USAA2014042400010), Apr 23, 2014: FLOOR SUPPORT. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FRAME 51 TO FRAME 52, STRINGER 38L, -Z 1970. REPLACED FLOOR SUPPORT BETWEEN FRAME 51 TO FRAME 52
- [SDR USAA2014042400009](https://openairdocs.org/sdr/USAA2014042400009), Apr 23, 2014: FLOOR SUPPORT. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FRAME 49 TO FRAME 50, STRINGER 38L, -Z 1970. REPLACED FLOOR SUPPORT BETWEEN FRAME 49 TO FRAME 50
- [SDR USAA2014050700001](https://openairdocs.org/sdr/USAA2014050700001), Apr 22, 2014: SHEAR WEB. CRACKED. BC1 CHECK SHEAR WEB CRACKED BETWEEN FRAME 68 & FRAME 69 AT Y 1732 & Z -500. FABRICATED & INSTALLED NEW SHEAR WEB IAW SRM 51-72-00 & DWG D53480020.
- [SDR USAA2014042100030](https://openairdocs.org/sdr/USAA2014042100030), Apr 20, 2014: PANEL. CORRODED. C1 CHECK LEVEL 2 GALVANIC CORROSION ON RT WING LOWER FUEL PANEL 640HB BETWEEN WING RIB 13 TO WING RIB 14 & BETWEEN STRINGER 8R TO STRINGER 11R. REPLACED RT WING
- [SDR USAA2014042100026](https://openairdocs.org/sdr/USAA2014042100026), Apr 19, 2014: STRINGER. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON STRINGER BETWEEN FRAME 65 TO FRAME 66, STRINGER 25R, Z-575. REPLACED STRINGER SECTION BETWEEN FRAME 65 TO FRAME 66, ST
- [SDR USAA2014042800017](https://openairdocs.org/sdr/USAA2014042800017), Apr 18, 2014: FLOORBEAM. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 67, Z-500, -Y 1162.5. REPLACED FLOORBEAM AT FRAME 67, Z-500, -Y 1162.5 IAW SRM 51-72-11 & DWG 17D53
- [SDR USAA2014042400014](https://openairdocs.org/sdr/USAA2014042400014), Apr 18, 2014: FLOORBEAM. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, Y 1292. REPLACED FLOORBEAM AT FRAME 66, Z-500, Y 1292 IAW SRM 53-41-14, 53-00-14, 51-20-
- [SDR USAA2014042400012](https://openairdocs.org/sdr/USAA2014042400012), Apr 18, 2014: FLOORBEAM. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 68, Z-500, Y 1162.5. REPLACED FLOORBEAM AT FRAME 68, Z-500, Y 1162.5 IAW SRM 53-00-14, 53-41-14 & D
- [SDR USAA2014042400011](https://openairdocs.org/sdr/USAA2014042400011), Apr 18, 2014: FLOORBEAM. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FRAME 66 TO FRAME 68, Z-500 & -Y 1162.5. REPLACED FLOORBEAM BETWEEN FRAME 66 TO FRAME 68, Z -500, -Y
- [SDR USAA2014042200006](https://openairdocs.org/sdr/USAA2014042200006), Apr 18, 2014: SHEAR PLATE. CRACKED. C1 CHECK CRACK IN RT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500 & -Y1292. REPLACED RT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500 & -Y1
- [SDR USAA2014042100028](https://openairdocs.org/sdr/USAA2014042100028), Apr 18, 2014: SHEAR PLATE. CRACKED. C1 CHECK CRACK ON LT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500, Y 1162.5. REPLACED LT LATERAL SHEAR PLATE BETWEEN FRAME 69 TO FRAME 70, Z-500, Y 1
- [SDR USAA2014042800016](https://openairdocs.org/sdr/USAA2014042800016), Apr 16, 2014: SILL. CORRODED. C1CHECK, LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z-500, -Y 1162.5. REPLACED SILL PLATE BETWEEN FRAME 66 TO FRAME 68, Z-500, -Y
- [SDR USAA2014042400013](https://openairdocs.org/sdr/USAA2014042400013), Apr 16, 2014: FLOORBEAM. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 66, Z-500, -Y 464.8. REPLACED FLOORBEAM AT FRAME 66, Z-500, -Y 464.8 IAW SRM 51-72-11.
- [SDR USAA2014042100029](https://openairdocs.org/sdr/USAA2014042100029), Apr 16, 2014: SEAT TRACK. CORRODED. C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BEAM BETWEEN FRAME 64 TO FRAME 66+8 INCHES, Z-500 & -Y 765. REPLACED SEAT TRACK BEAM BETWEEN FRAME 64 TO FR
- [SDR USAA2014042100027](https://openairdocs.org/sdr/USAA2014042100027), Apr 16, 2014: SILL. CORRODED. C1 CHECK LEVEL 2 SURFACE CORROSION ON AFT LOWER CORNER SHAPE SILL ON LT PAX & CREW DOOR CUT OUT BETWEEN FRAME 66 TO FRAME 68, Z-500, Y 1584. REPLACED AFT LOWER 
- [SDR USAA2014031700020](https://openairdocs.org/sdr/USAA2014031700020), Mar 16, 2014: SPLICE. DEFECTIVE. FOUND EMERGENCY EXIT LIGHTS AT ROW 7 NOT WORKING. REPLACED PIN SPLICE FOR EMERGENCY EXIT LIGHTS AT ROW 7 IAW A320N ESPM 20-48-25, OPERATIONS CHECKED GOOD.
- [SDR USAA2014031300007](https://openairdocs.org/sdr/USAA2014031300007), Mar 12, 2014: POWER SUPPLY. FAULTY. AFT EMERGENCY POWER SUPPLY SHOWS INTERNAL FAULT. REPLACED AFT EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.
- [SDR USAA2014030300003](https://openairdocs.org/sdr/USAA2014030300003), Mar 1, 2014: LENS. MISSING. FORWARD LT FIRST CLASS WINDSCREEN MISSING RED EMERGENCY LIGHT LENS. REPLACED FWD LT FIRST CLASS WINDSCREEN RED EMERGENCY LIGHT LENS.
- [SDR USAA2014021900008](https://openairdocs.org/sdr/USAA2014021900008), Feb 16, 2014: FLOOR PANEL. DAMAGED. REGULAR OVERNIGHT VISIT, CARGO FLOOR PANEL AT BS 2616 BETWEEN STRINGER 38L & STRINGER 38R HAS A 1 INCH X 1 INCH PIECE OF MISSING HONEYCOMB CORE AT Y +763. R & R
- [SDR USAA2014021800004](https://openairdocs.org/sdr/USAA2014021800004), Feb 14, 2014: FLOOR PANEL. DELAMINATED. REGULAR OVERNIGHT VISIT DELAMINATION ON THE CORNER OF AFT CARGO FLOOR PANEL AT BS 2616, STRINGER 38R & -Y 765. REPLACED AFT CARGO FLOOR PANEL AT BS 2616, STRING
- [SDR USAA2014021700024](https://openairdocs.org/sdr/USAA2014021700024), Feb 14, 2014: FLOOR SUPPORT. MISSING. REGULAR OVERNIGHT VISIT, AFT CARGO COMPARTMENT FLOOR PANEL CROSS BEAM SUPPORT HAS PIECE OF MATERIAL MISSING AT FRAME 56, STRINGER 38R & -Y9.5. REPLACED AFT CARG
- [SDR USAA2014020600004](https://openairdocs.org/sdr/USAA2014020600004), Feb 5, 2014: BATTERY. DISCHARGED. FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY LOW. REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY.
- [SDR USAA2014020300004](https://openairdocs.org/sdr/USAA2014020300004), Feb 1, 2014: FLOOR PANEL. DELAMINATED. RON VISIT DELAMINATION ON FLOOR PANEL 232FF & CORROSION ON INSERTS BETWEEN FRAME 20 TO FRAME 24, STRINGER 23R - Y 1292. REPLACED FLOOR PANEL 232FF IAW AMM 53-12
- [SDR USAA2014020300006](https://openairdocs.org/sdr/USAA2014020300006), Jan 30, 2014: FLOOR SUPPORT. CORRODED. RON VISIT CORROSION ON FLOOR SUPPORT AT FRAME 20, STRINGER 23R, - Y 1030. REPLACED FLOOR SUPPORT AT FRAME 20, STRINGER 23R - Y 1030 IAW SRM 51-42-11 & DWG D5311
- [SDR USAA2014013100007](https://openairdocs.org/sdr/USAA2014013100007), Jan 30, 2014: GUST LOCK. CRACKED. L1 DOOR GUST LOCK BUTTON CRACKED FOUND WHEN ATTEMPTING TO ROB FOR ACFT. REPLACED L1 DOOR GUST LOCK BUTTON IAW AMM 52-11-12-000-802A STEP 4 A1-3 & INSTALLED IAW 
- [SDR USAA2014020300008](https://openairdocs.org/sdr/USAA2014020300008), Jan 28, 2014: FLOOR SUPPORT. CORRODED. RON VISIT CORROSION ON FLOOR SUPPORT AT FRAME 20, STRINGER 23R - Y 1292. REPLACED FLOOR SUPPORT AT FRAME 20, STRINGER 23R - Y 1292 IAW SRM 51-42-11.
- [SDR USAA2014020300007](https://openairdocs.org/sdr/USAA2014020300007), Jan 28, 2014: SEAT TRACK. CORRODED. RON VISIT CORROSION ON SEAT TRACK AT FRAME 20, STRINGER 23R - Y 1292. REPLACED SEAT TRACK AT FRAME 20, STRINGER 23R - Y 1292 IAW SRM 51-42-11.
- [SDR USAA2014020300005](https://openairdocs.org/sdr/USAA2014020300005), Jan 28, 2014: SEAT TRACK. CORRODED. RON VISIT CORROSION ON SEAT TRACK AT FRAME 20, STRINGER 23R - Y 765. REPLACED SEAT TRACK AT FRAME20, STRINGER 23R - Y 765 IAW SRM 51-42-11.
- [SDR USAA2013120900008](https://openairdocs.org/sdr/USAA2013120900008), Dec 7, 2013: LENS. MISSING. ROW 22L EMERGENCY LIGHT LENS MISSING. INSTALLED NEW ROW 22L EMERGENCY LIGHT LENS.
- [SDR USAA2013111300028](https://openairdocs.org/sdr/USAA2013111300028), Nov 9, 2013: FLOOR PANEL. DAMAGED. FORWARD CARGO BAY FORWARD EDGE CENTER FLOOR PANEL 131EF UPPER SKIN DAMAGED. REPLACED FLOOR PANEL IAW AMM 53-22-14.
- [SDR USAA2013111200005](https://openairdocs.org/sdr/USAA2013111200005), Nov 9, 2013: FLOOR PANEL. DELAMINATED. CARGO FLOOR PANEL 132FF DELAMINATED. R & R FLOOR PANEL IAW AMM 53-22-14.
- [SDR USAA2013092400007](https://openairdocs.org/sdr/USAA2013092400007), Sep 23, 2013: LENS. MISSING. COVER FOR EMERGENCY EXIT LIGHT ACFT RT REAR DOOR MISSING. REPLACED MISSING EMERGENCY LIGHT COVER AT DOOR L-2.
- [SDR USAA2013091600003](https://openairdocs.org/sdr/USAA2013091600003), Sep 15, 2013: LENS. MISSING. EMERGENCY LIGHT LENS AT SEAT ROW 19L IS MISSING. INSTALLED AISLE EMERGENCY LIGHT LENS AT SEAT ROW 19L.
- [SDR USAA2013081900004](https://openairdocs.org/sdr/USAA2013081900004), Aug 17, 2013: LENS. MISSING. EMERGENCY EXIT LIGHT LENS MISSING ON SEAT ROW 5. REPLACED LENS SEAT ROW 5.
- [SDR USAA2013081300008](https://openairdocs.org/sdr/USAA2013081300008), Aug 12, 2013: LENS. MISSING. RED LENS ON L2 DOOR EMERGENCY LIGHT MISSING. REPLACED LENS.
- [SDR USAA2013042500004](https://openairdocs.org/sdr/USAA2013042500004), Apr 24, 2013: OVERWING EXIT. NOT SEATED. SLIDE ARMED LIGHT OVERWING EXIT DOORS DOES NOT SHOW ARMED ON ECAM. REMOVED AND RE-INSTALLED RIGHT AFT OVERWING EXIT DOOR, OPERATIONAL CHECK GOOD REFERENCE AIRBU
- [SDR USAA2012112600007](https://openairdocs.org/sdr/USAA2012112600007), Nov 24, 2012: LENS. MISSING. DOOR 1L FIRST CLASS PARTITION LIGHT COVER MISSING. REPLACED EMERGENCY EXIT LIGHT LENS.
- [SDR USAA2012111900017](https://openairdocs.org/sdr/USAA2012111900017), Nov 18, 2012: BOTTLE. LOW PRESSURE. L1 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED L1 DOOR ASSIST BOTTLE TO PROPER PRESSURE.
- [SDR USAA2012101100009](https://openairdocs.org/sdr/USAA2012101100009), Oct 10, 2012: UNKNOWN. MALFUNCTIONED. C2 CHECK - EVACUATION SIGNALING SYSTEM FAILS OPERATIONAL TEST. NO RESPONSE TO COMMAND SWITCH. REPROGRAMMED CABIN LAYOUT SELECTION PERCENTAGE, PERFORMED OPERATIO
- [SDR USAA2012101600014](https://openairdocs.org/sdr/USAA2012101600014), Oct 8, 2012: DAMPER. LOW PRESSURE. BC2 CHECK - R2 DOOR OPEN ASSIST CYLINDER READ 0 PSI, UPON AIRCRAFT ARRIVAL. SERVICED R2 DOOR DAMPER & EMERGENCY OPERATIONS CYLINDER IAW A320 AMM 52-10-00.
- [SDR USAA2012100900028](https://openairdocs.org/sdr/USAA2012100900028), Oct 8, 2012: HOUSING. BROKEN. BC2 CHECK - PAX SEAT 22ABC EMERGENCY LIGHT HOUSING BROKEN. REPLACED EMERGENCY LIGHT HOUSING AT PAX SEAT 22ABC IAW A320 SRM 51-42-11.
- [SDR USAA2012100900027](https://openairdocs.org/sdr/USAA2012100900027), Oct 8, 2012: HOUSING. BROKEN. BC2 CHECK - PAX SEAT 7ABC EMERGENCY LIGHT HOUSING BROKEN. REPLACED EMERGENCY LIGHT HOUSING AT PAX SEAT 7ABC IAW A320 SRM 51-42-11.
- [SDR USAA2012100500007](https://openairdocs.org/sdr/USAA2012100500007), Oct 4, 2012: DIAPHRAGM. UNSERVICEABLE. BC2 CHECK - L2 DOOR OPEN ASSIST CYLINDER READS ZERO PSI. REMOVED DIAPHRAGM ON THE L2 DOOR OPEN ASSIST CYLINDER FOUND TO BE UNSERVICABLE. INSTALLED NEW DIAPHRAGM

All 195: https://openairdocs.org/deregistered/N620AW-2015-06-18/reports.md

## 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.

- [Incident 19940801030279I](https://openairdocs.org/incident/19940801030279I), Aug 1, 1994: Airbus A320231 (N620AW), Wichita, KS. Enroute fuel quantity indications abnormal. Diverted to Wichita. Fuel quanity indicator computer deferred.

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