# N628AW: 1989 Airbus Industrie A320-231, registration cancelled 2014-01-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 28, 2014
- Exported to: South Africa
- 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: 67
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: November 17, 1989
- Certificate issued: January 8, 2014
- Last registry action: January 8, 2014
- Mode S code: A8340A
- Owner when cancelled: [Aircraft Support Group Inc](https://openairdocs.org/faa-owner/AIRCRAFT%20SUPPORT%20GROUP%20INC)
- Location: [Hollywood, FL](https://openairdocs.org/faa-place/FL/Hollywood)
- Owner type: Corporation
- Owner's area on the map: 26.0231° N, 80.1865° W: Placed by OpenAirDocs at the center of ZIP code 33021, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N628AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=628AW
- Page: https://openairdocs.org/deregistered/N628AW-2014-01-28

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 (256, newest 50)

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

- [SDR USAA2014F00046](https://openairdocs.org/sdr/USAA2014F00046), Oct 22, 2013: BULB. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHTS CONTROL PANEL HAD SEVERAL BULBS OUT. R & R PANEL.
- [SDR USAA2013080800015](https://openairdocs.org/sdr/USAA2013080800015), Aug 7, 2013: LENS. MISSING. EMERGENCY LIGHT LENS MISSING ON ROWS 10 & 11. INSTALLED NEW LENS FOR EMERGENCY EXIT LIGHTS ROWS 10 AND 11 LT.
- [SDR USAA2013072400007](https://openairdocs.org/sdr/USAA2013072400007), Jul 23, 2013: LENS. MISSING. EMERGENCY LIGHT LENS MISSING AT 17C. REPLACED EMERGENCY LIGHT LENS AT 17C.
- [SDR USAA2013070100010](https://openairdocs.org/sdr/USAA2013070100010), Jun 28, 2013: LENS. MISSING. ROW 26, ACFT LT, FLOOR EXIT LIGHT MISSING COVER. REPLACED LENS ON EMERGENCY LIGHT AT 26L.
- [SDR USAA2013053000005](https://openairdocs.org/sdr/USAA2013053000005), May 29, 2013: LENS. MISSING. ROW 1, LT MISSING SEAT MOUNTED EMERGENCY LIGHT LENS. REPLACED MISSING LIGHT LENS.
- [SDR USAA2013040800017](https://openairdocs.org/sdr/USAA2013040800017), Apr 6, 2013: LENS. MISSING. ROW 26L EMERGENCY LIGHT LENS MISSING. INSTALLED NEW LIGHT LENS AS NEEDED.
- [SDR USAA2013040200027](https://openairdocs.org/sdr/USAA2013040200027), Apr 1, 2013: LENS. MISSING. EMERGENCY LIGHT LENS AT ROW 19L IS MISSING. INSTALLED EMERGENCY LIGHT LENS AT ROW 19L.
- [SDR USAA2013021100027](https://openairdocs.org/sdr/USAA2013021100027), Feb 9, 2013: POWER SUPPLY. FAILED. CABIN FORWARD EMERGENCY POWER SUPPLY UNIT FAILED BITE TEST. REMOVED AND REPLACED CABIN FORWARD EMERGENCY POWER SUPPLY UNIT.
- [SDR USAA2013020800019](https://openairdocs.org/sdr/USAA2013020800019), Feb 6, 2013: LENS. DETACHED. EMERGENCY EXIT SIGN ON THE LOWER DOOR 2R FELL OFF DURING LANDING. REPLACED EMERGENCY EXIT LENS ON DOOR 2R.
- [SDR USAA2013013100016](https://openairdocs.org/sdr/USAA2013013100016), Jan 30, 2013: LENS. MISSING. SEAT MOUNTED EMERGENCY LIGHT AT ROW 9R IS MISSING THE LENS. INSTALLED LENS ON SEAT MOUNTED EMERGENCY LIGHT AT ROW 9R IAW AIRBUS MAINTENANCE MANUAL 33-51-13.
- [SDR USAA2013011400020](https://openairdocs.org/sdr/USAA2013011400020), Jan 12, 2013: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY UNIT 10WL INOPERATIVE. REMOVED AND REPLACED EPSU IAW MM 33-51-38.
- [SDR USAA2013010300018](https://openairdocs.org/sdr/USAA2013010300018), Dec 31, 2012: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS DO NOT TEST CORRECTLY L1 AND R1 DOOR. REMOVED AND REPLACED POWER SUPPLY PER AMM 33-51-38 - OPS CHECKED GOOD.
- [SDR USAA2013010300017](https://openairdocs.org/sdr/USAA2013010300017), Dec 31, 2012: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS DO NOT TEST CORRECTLY L1 & R1 DOOR. REMOVED AND REPLACED POWER SUPPLY 10WL PER 33-51-38-000-001. SYSTEM OPS CHECKED GOOD.
- [SDR USAA2012110200025](https://openairdocs.org/sdr/USAA2012110200025), Nov 1, 2012: SIGN. CRACKED. THE 2L EXIT SIGN CRACKED. REMOVED & REPLACED 2L EXIT SIGN.
- [SDR USAA2012100500037](https://openairdocs.org/sdr/USAA2012100500037), Oct 4, 2012: LENS. DETACHED. EXIT PATH LIGHTING LENS COVER OFF LEFT SIDE LAST ROW. REPLACED EMERGENCY LIGHT LENS ROW 26 LEFT.
- [SDR USAA2012100500032](https://openairdocs.org/sdr/USAA2012100500032), Oct 2, 2012: LENS. MISSING. EMERGENCY LIGHT LENS MISSING NEAR ROW 25ABC FLOORING. INSTALLED LENS AT ROW 25ABC.
- [SDR USAA2012071600004](https://openairdocs.org/sdr/USAA2012071600004), Jul 12, 2012: WIRE. BROKEN. BC1 CHECK - FORWARD LEFT WINDSCREEN EMERGENCY LIGHT WIRES BROKEN. REPAIRED FORWARD LEFT WINDSCREEN EMERGENCY LIGHT WIRES IAW A320 ESPM 20-48-25. OPS CHECK GOOD 
- [SDR USAA2012071600003](https://openairdocs.org/sdr/USAA2012071600003), Jul 12, 2012: WIRE. BROKEN. BC1 CHECK - NR 1 LEFT AND NR 3 LEFT EMERGENCY LIGHT WIRES BROKEN. REPAIRED NR 1 LEFT AND NR 3 LEFT EMERGENCY LIGHT WIRES IAW A320 AMM 33-51-19-0401 AND AIRBUS E
- [SDR USAA2012071600012](https://openairdocs.org/sdr/USAA2012071600012), Jul 4, 2012: SKIN. SATURATED. BC1 CHECK - WATER INGRESS ON UPPER SURFACE OF LEFT ELEVATOR AT ZONE 1 AND ZONE 3. REPAIRED UPPER SURFACE OF LEFT ELEVATOR AT ZONE 1 AND ZONE 3 IAW A320 SRM 55-2
- [SDR USAA2012071600015](https://openairdocs.org/sdr/USAA2012071600015), Jul 3, 2012: SKIN. SATURATED. BC1 CHECK - WATER INGRESS ON UPPER SURFACE OF RIGHT ELEVATOR AT ZONE 1 AND ZONE 5. REPAIRED UPPER SURFACE OF RIGHT ELEVATOR AT ZONE 1 AND ZONE 5 IAW A320 SRM 55
- [SDR USAA2012031200025](https://openairdocs.org/sdr/USAA2012031200025), Mar 11, 2012: BRACKET. BROKEN. SLIDE BUSTLE DOOR 2R NEEDS TO BE REFITTED. FOUND LATCHING BRACKET BROKEN. REPAIRED SLIDE COVER DOOR R2 IAW STRUCTURAL REPAIR MANUAL 51-42-11.
- [SDR USAA2012030800016](https://openairdocs.org/sdr/USAA2012030800016), Mar 2, 2012: BATTERY. DISCHARGED. AFT FLIGHT ATTENDANT SWIVEL SEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY AFT SWIVEL JUMPSEAT. OPS CHECKED GOOD.
- [SDR USAA2012021300020](https://openairdocs.org/sdr/USAA2012021300020), Feb 11, 2012: LENS. MISSING. LENS MISSING FROM EMERGENCY SEAT MOUNTED LIGHT ROW 11L. INSTALLED LENS ON SEAT MOUNTED EMERGENCY LIGHT ROW 11L.
- [SDR USAA2012012600005](https://openairdocs.org/sdr/USAA2012012600005), Jan 25, 2012: LIGHT. BROKEN. SMALL EMERGENCY LIGHT AT EDGE OF FORWARD BULKHEAD BROKEN. REPLACED FORWARD WINDSCREEN EMERGENCY LIGHT ASSEMBLY.
- [SDR USAA2012010400021](https://openairdocs.org/sdr/USAA2012010400021), Jan 1, 2012: TRANSDUCER. FAILED. AFTER TAKEOFF PRIOR TO 1000', ENGINE NR 1 SURGED TWICE AND SELF-RECOVERED WITH NORMAL INDICATIONS. ON LANDING ROLLOUT, RECEIVED ECAM MESSAGES FOR ENG 1 COMPRESS
- [SDR USAA2011101000008](https://openairdocs.org/sdr/USAA2011101000008), Oct 8, 2011: CONNECTOR. DEFECTIVE. RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND RE-INSTALLED BAYONET CONNECTOR - OPERATIONAL CHECK NORMAL IAW AIRBUS MAINTENANCE M
- [SDR USAA2011100400017](https://openairdocs.org/sdr/USAA2011100400017), Oct 3, 2011: SPRING. BROKEN. CABIN DOOR 2L ARMED INDICATION INTERMITTENT. MAINTENANCE REPLACED BROKEN SPRING IN AFT GIRT BAR FLOOR FITTING.
- [SDR USAA2011092900013](https://openairdocs.org/sdr/USAA2011092900013), Sep 28, 2011: WIRE. LOOSE. EMERGENCY LIGHT WIRING IS HANGING LOOSE UNDER SEAT ROW 11L. MAINTENANCE SECURED LIGHT WIRING FOR SEAT 11L - OPERATIONAL CHECK NORMAL.
- [SDR USAA2011091200016](https://openairdocs.org/sdr/USAA2011091200016), Sep 9, 2011: CONTAINER. BROKEN. SEAT ROW 12L PASSENGER EMERGENCY O2 PANEL WILL NOT LATCH - SEAT ROW 18R PASSENGER EMERGENCY O2 PANEL TEST BUTTON IS BROKEN. MAINTENANCE REPLACED PASSENGER EMERG
- [SDR USAA2011061400004](https://openairdocs.org/sdr/USAA2011061400004), Jun 13, 2011: CONTROL UNIT. MALFUNCTIONED. LAS - EEL - EMERGENCY EXIT LIGHT TEST FAULTS 'AFT L'. RESET 'AFT L' POWER CONTROL UNIT, OPERATIONAL CHECK GOOD.
- [SDR USAA2010121793113](https://openairdocs.org/sdr/USAA2010121793113), Dec 17, 2010: PROFILE. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTRAL FUSELAGE. REPLACED LOWER FLA
- [SDR USAA2010121793112](https://openairdocs.org/sdr/USAA2010121793112), Dec 17, 2010: PROFILE. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER
- [SDR USAA2010121793111](https://openairdocs.org/sdr/USAA2010121793111), Dec 17, 2010: PROFILE. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTIG PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER
- [SDR USAA2010121793125](https://openairdocs.org/sdr/USAA2010121793125), Dec 16, 2010: SILL. CORRODED. SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 66, S23L IAW E
- [SDR USAA2010121793124](https://openairdocs.org/sdr/USAA2010121793124), Dec 16, 2010: SILL. CORRODED. SAL - MAJOR REPAIR - S5 CHECK - CORROSION ON LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R. REPAIRED LOWER SILL AROUND GIRT BAR FITTING AT FR 68, S23R IAW E
- [SDR USAA2010121793118](https://openairdocs.org/sdr/USAA2010121793118), Dec 16, 2010: FLOORBEAM. CRACKED. SAL - S5 - MAJOR REPAIR - CRACK ON FLOORBEAM BETWEEN FR46 TO FR47, -Y254. REPAIRED FLOORBEAM BETWEEN FR46 TO FR47, -Y254 IAW EA 133198.
- [SDR USAA2010121793117](https://openairdocs.org/sdr/USAA2010121793117), Dec 16, 2010: PROFILE. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE LEFT AFT EMERGENCY EXIT (834) AT CENTER FUSELAGE. REPLACED LOWER FLANG
- [SDR USAA2010121793116](https://openairdocs.org/sdr/USAA2010121793116), Dec 16, 2010: PROFILE. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF RIGHT LOAD TRANSMITTING PROFILE OF THE RIGHT AFT EMERGENCY EXIT (844) AT CENTRAL FUSELAGE. REPLACED LOWER FL
- [SDR USAA2010121793115](https://openairdocs.org/sdr/USAA2010121793115), Dec 16, 2010: PROFILE. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD LEFT EMERGENCY EXIT (833) AT CENTRAL FUSELAGE. REPLACED LOWER 
- [SDR USAA2010121793114](https://openairdocs.org/sdr/USAA2010121793114), Dec 16, 2010: PROFILE. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS ON LOWER FLANGE OF LEFT LOAD TRANSMITTING PROFILE OF THE FORWARD RIGHT EMERGENCY EXIT (843) AT CENTRAL FUSELAGE. REPLACED LOWER
- [SDR USAA2010121793123](https://openairdocs.org/sdr/USAA2010121793123), Dec 14, 2010: SKIN. CORRODED. SAL - S5 - MAJOR REPAIR - CORROSION ON INTERNAL SKIN AT FR58 + 15 INCHES BETWEEN S43R & S44R AFT CARGO COMPARTMENT. REPAIRED INTERNAL SKIN AT FR58 + 15 INCHES B
- [SDR USAA2010121793122](https://openairdocs.org/sdr/USAA2010121793122), Dec 13, 2010: FRAME. CRACKED. SAL - S5 - MAJOR REPAIR - CRACK ON UPPER FLANGE OF FRAME 25 AT LEVEL S31L FWD C.C. REPAIRED UPPER FRAME FLANGE AT FR25, S31L IAW A320 SRM 53-00-12.
- [SDR USAA2010121793120](https://openairdocs.org/sdr/USAA2010121793120), Dec 13, 2010: ANGLE. CORRODED. SAL - S5 - MAJOR REPAIR - CORROSION ON ANGLE AT FR71 CUTOUT ACCESS DOOR 312AR BETWEEN S27R TO S30R TAIL SECTION AFT FUSELAGE. REPLACED ANGLE AT FR71 CUTOUT ACCE
- [SDR USAA2010121793142](https://openairdocs.org/sdr/USAA2010121793142), Dec 4, 2010: SLIDE RAFT. FAULTY. SAL - EES - S5 CHECK - PASSENGER CREW DOOR 842 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 842 IAW TASK CARD 26C84252006.
- [SDR USAA2010121793141](https://openairdocs.org/sdr/USAA2010121793141), Dec 4, 2010: SLIDE RAFT. FAULTY. SAL - EES - S5 CHECK - PASSENGER CREW DOOR 832 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 832 IAW TASK CARD 26C83252008.
- [SDR USAA2010121793140](https://openairdocs.org/sdr/USAA2010121793140), Dec 4, 2010: SLIDE RAFT. FAULTY. SAL - EES - S5 CHECK - PASSENGER CREW DOOR 841 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 841 IAW TASK CARD 26C84152006.
- [SDR USAA2010120792901](https://openairdocs.org/sdr/USAA2010120792901), Dec 4, 2010: FITTING. CORRODED. SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR30 BETWEEN S39L TO S40L. REPLACED CLEAT AT FR30 BETWEEN S39L TO S40L IAW A320 SRM 51-72-11 & 
- [SDR USAA2010121793119](https://openairdocs.org/sdr/USAA2010121793119), Dec 3, 2010: STIFFENER. CRACKED. SAL - S5 - MAJOR REPAIR - CRACKS FRONT SPAR OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER INTERNAL AREA OF ACCESS PANEL 331AB. REPAIRED STIFFENER BETWEEN RIB 4 
- [SDR USAA2010120892925](https://openairdocs.org/sdr/USAA2010120892925), Dec 3, 2010: SHEAR PIN. CORRODED. SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). 
- [SDR USAA2010120892924](https://openairdocs.org/sdr/USAA2010120892924), Dec 3, 2010: SHEAR PIN. CORRODED. SAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1).

All 256: https://openairdocs.org/deregistered/N628AW-2014-01-28/reports.md

## NTSB investigations (2)

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 LAX99LA323](https://openairdocs.org/ntsb/LAX99LA323), Sep 17, 1999: Airbus Industrie A-320-231 (N628AW), Beatty, NV, no damage. Probable cause: the failure of the injured passengers to remain seated with their seat belts fastened as directed by the captain.
- [NTSB NYC99IA062](https://openairdocs.org/ntsb/NYC99IA062), Feb 16, 1999: Airbus Industrie A-320-231 (N628AW), Columbus, OH, incident, minor damage. Probable cause: a failure of the external o-rings in the nose landing gear steering module.

## FAA accident and incident reports (2)

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 19990916037259A](https://openairdocs.org/incident/19990916037259A), Sep 16, 1999: Airbus A320231 (N628AW), Las Vegas, NV. (.19) On September 16, 1999, at 2147 hours pacific daylight time, an america west Airbus A320-321, N628AW, flight 2569, encountered turbulence while on descent…
- [Incident 19990216021179I](https://openairdocs.org/incident/19990216021179I), Feb 16, 1999: Airbus A320321 (N628AW), Columbus, OH, Minor damage. During approach and after calling for "gear down" crew received ecam message "lgciu #1 fault", then received "lgciu #2 fault". Crew made fly-by and tower…

## Other aircraft with N628AW

- [Registered now](https://openairdocs.org/aircraft/N628AW): Piper PA-23-160, S/N 23-1790, built 1959

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