# N645AW: 1991 Airbus Industrie A320-231, registration cancelled 2006-05-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 10, 2006
- Status when cancelled: Triennial form not returned
- Airframe: [Airbus Industrie A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (registry code 3930325)
- Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 238
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 8, 1997
- Certificate issued: October 28, 1996
- Last registry action: July 30, 2003
- Mode S code: A877E3
- Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%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/N645AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=645AW
- Page: https://openairdocs.org/deregistered/N645AW-2006-05-10

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 (51, newest 50)

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

- [SDR AWXA200501150](https://openairdocs.org/sdr/AWXA200501150), Sep 29, 2005: CIRCUIT BOARD. FALSE INDICATION. LAS - EMERGENCY LANDING - FLT 176 - DURING GEAR EXTENSION RECEIVED NOSE LANDING GEAR LIGHT ON UPPER PANEL, ALL OTHER INDICATIONS WERE NORMAL. CREW PERFORMED FLY
- [SDR AWXA200501012](https://openairdocs.org/sdr/AWXA200501012), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 20+10" Y-765. MAINTENANCE REMOVED CORROSION AND FOU
- [SDR AWXA200501011](https://openairdocs.org/sdr/AWXA200501011), Aug 15, 2005: FITTING. CORRODED. SAL - MAJOR REPAIR - CORROSION FOUND ON C3 CHECK LOCATED AROUND FITTING AT THE LOWER SILL OF THE FORWARD CARGO DOOR CUTOUT. NO ALLOWABLE DAMAGE LIMITS FOUND IN 
- [SDR AWXA200501010](https://openairdocs.org/sdr/AWXA200501010), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 36" Y-765. MAINTENANCE REMOVED CORROSION AND FOUND 
- [SDR AWXA200501005](https://openairdocs.org/sdr/AWXA200501005), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT OUTBOARD SIDE AT FR 39 +3" Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO
- [SDR AWXA200501004](https://openairdocs.org/sdr/AWXA200501004), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT INBOARD SIDE AT FR 39 +10" Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO B
- [SDR AWXA200501003](https://openairdocs.org/sdr/AWXA200501003), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 42 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO
- [SDR AWXA200501002](https://openairdocs.org/sdr/AWXA200501002), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 36 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO
- [SDR AWXA200501001](https://openairdocs.org/sdr/AWXA200501001), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT LT INBOARD SIDE AT FR 44+7, Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT 
- [SDR AWXA200501000](https://openairdocs.org/sdr/AWXA200501000), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT INBOARD SIDE AT FR 42+17, -Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT
- [SDR AWXA200500999](https://openairdocs.org/sdr/AWXA200500999), Aug 15, 2005: SEAT TRACK. CORRODED. SAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT OUTBOARD SIDE AT FR 42+17, -Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE 
- [SDR AWXA200401002](https://openairdocs.org/sdr/AWXA200401002), Sep 10, 2004: WIRE. OPEN. FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, AND 5 REMAIN ON AND WILL NOT RESET. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY P
- [SDR AWXA200400578](https://openairdocs.org/sdr/AWXA200400578), May 27, 2004: WIRE. CHAFED. ON CLIMBOUT, RECEIVED ECAM INDICATION NR 2 ENG NACELLE TEMP VARIES BETWEEN 315 & 380 DEGREES, INDICATION INTERMITTENT, DIVERTED TO PHX FOR REPAIR. MX TROUBLESHO
- [SDR AWXA200400507](https://openairdocs.org/sdr/AWXA200400507), May 12, 2004: TERMINAL. DEFECTIVE. PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE TERMINALS AT EMERGENCY ESCAPE 
- [SDR AWXA200400134](https://openairdocs.org/sdr/AWXA200400134), Feb 1, 2004: WIRE. BROKEN. DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW
- [SDR AWXA200400025](https://openairdocs.org/sdr/AWXA200400025), Jan 9, 2004: LIGHT. BROKEN. PHX - EEL - FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH FIXTURE AT FORWARD BULKHEAD WAS BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSE
- [SDR AWXA200400022](https://openairdocs.org/sdr/AWXA200400022), Jan 4, 2004: EPSU. DEFECTIVE. MCN - EEL - DURING C-02 CHECK FOUND EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, & 4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY
- [SDR AWXA200400006](https://openairdocs.org/sdr/AWXA200400006), Dec 24, 2003: RIB. CRACKED. MCN - MINOR REPAIR - DURING C-02 CHECK A 1.25 INCH CRACK WAS FOUND ON NR 2 PYLON AFT FIXED FAIRING (RIB 12) AT OUTBOARD ANGLE. MAINTENANCE REMOVED CRACKED RIB A
- [SDR AWXA200400007](https://openairdocs.org/sdr/AWXA200400007), Dec 22, 2003: SKIN. ERODED. MCN - MINOR REPAIR - DURING C-02 CHECK THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN WAS FOUND ERODED. MAINTENANCE REMOVED ERODED NR 2 PYLON AFT FIXED FAIRING I
- [SDR AWXA200301197](https://openairdocs.org/sdr/AWXA200301197), Oct 9, 2003: SMOKE. DETECTED. EN ROUTE FROM PHX TO ATL THE FLIGHT ATTENDANT REPORTED A STRONG BURNING ODOR AND ANOTHER FLIGHT ATTENDANT SAID SHE SAW SMOKE AT SEAT ROWS 9 AND 10 RT SIDE. ODOR
- [SDR AWXA200301122](https://openairdocs.org/sdr/AWXA200301122), Oct 2, 2003: COFFEEMAKER. MALFUNCTIONED. EN ROUTE, REPORTED STRONG ELECTRICAL BURNING ODOR IN CABIN & COCKPIT. MX INSPECTED WIRING IN MAIN FWD GALLEY AREA BEHIND C/B PANEL, NR 1 & 2 OVENS, COFFEEMAKERS
- [SDR AWXA200300805](https://openairdocs.org/sdr/AWXA200300805), Jul 16, 2003: EEC. FAILED. DURING TAKEOFF AT PHX EN ROUTE FOR DEN THE CREW PUSHED POWER UP FOR TAKEOFF AND THE NR 2 ENGINE DID NOT RESPOND, POWER REMAINED AT IDLE, REJECTED TAKEOFF. FLIGH
- [SDR AWXA200300736](https://openairdocs.org/sdr/AWXA200300736), Jun 25, 2003: ACTUATOR. FAULTY. AT CRUISE FL 360, NR 2 ENG COMPRESSOR VANE ECAM MSG, AT FL 290 NR 2 ENG STALLED. SHUTDOWN ENG, EMERGENCY EQUIP TO STANDBY. LANDED, TAXIED TO GATE. REPORT INDICA
- [SDR AWXA200300370](https://openairdocs.org/sdr/AWXA200300370), Apr 14, 2003: ENGINE. MALFUNCTIONED. DURING TOGA POWER APPLICATION NR 2 ENGINE SPOOLED UP SLOWER THAN NR 1 ENGINE CAUSING AN ISSUE ON WET RUNWAY, REJECTED TAKEOFF APPROX 15 KTS. INITIAL SPOOL DIFFE
- [SDR AWXA200201014](https://openairdocs.org/sdr/AWXA200201014), Oct 14, 2002: CYLINDER. LEAKING. DURING C-01 CHECK THE R-2 DOOR WAS FOUND TO HAVE NO DAMPING ACTION WHEN CLOSING DUE TO INTERNAL LEAKAGE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR DAMPING A
- [SDR AWXA200200999](https://openairdocs.org/sdr/AWXA200200999), Oct 4, 2002: FITTING. CRACKED. MCN - MAJOR REPAIR - DURING C-01 CHECK A 1 1/2" CRACK WAS FOUND ON THE R/H MAIN LANDING GEAR DOOR FORWARD HINGE FITTING. MAINTENANCE REMOVED DAMAGED R/H MAIN LA
- [SDR AWXA200200883](https://openairdocs.org/sdr/AWXA200200883), Sep 12, 2002: SKIN. CORRODED. PHX - MAJOR REPAIR - DURING INSPECTION THE FUSELAGE SKIN WAS FOUND CORRODED BENEATH AFT AIRPHONE ANTENNA. MAINTENANCE REMOVED CORRODED SECTION OF SKIN FR 63, FA
- [SDR AWXA200200785](https://openairdocs.org/sdr/AWXA200200785), Aug 21, 2002: FLASHLIGHT. INOPERATIVE. SAN - EMERGENCY EQUIPMENT - DURING INSPECTION THE AFT FLIGHT ATTENDANTS FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTEND
- [SDR AWXA200100517](https://openairdocs.org/sdr/AWXA200100517), Oct 6, 2001: VALVE. LEAKING. PHX - AIR TURNBACK - FLT 27 - AFTER T/O THE LANDING GEAR WOULD NOT RETRACT. CREW RESET LGCIU 1 & 2 PER MAINTENANCE CONTROL, NO HELP. THE AIRCRAFT APPEARED TO RE
- [SDR AWXA0001953](https://openairdocs.org/sdr/AWXA0001953), Jul 9, 2001: FLOOR SUPPORT. CORRODED. AFT CABIN FLOOR PANEL SUPPORT AT Y-1732R/H FR 66 SCREWS HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .100 (BEYOND LIMITS AS PER A320 SRM 51-72-11 PG 1). 
- [SDR AWXA0001999](https://openairdocs.org/sdr/AWXA0001999), Jul 7, 2001: FLOORBEAM. CORRODED. AFT CABIN FLOOR PANEL SUPPORT AT Y-1732 RT FR 66 SCREW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .100 INCH (BEYOND LIMITS AS PER SRM 51-72-11 PG 1). R
- [SDR AWXA0001998](https://openairdocs.org/sdr/AWXA0001998), Jul 7, 2001: FLOOR SUPPORT. CORRODED. AFT CABIN FLOOR PANEL SUPPORT AT Y-765 LT FR 66 TO FR68 SCEW HOLES CORRODED. REMOVED CORROSION, MATERIAL REMOVED .035 INCH (BEYOND LIMITS AS PER A320 SRM 53-41-
- [SDR AWXA0001997](https://openairdocs.org/sdr/AWXA0001997), Jun 29, 2001: FLOOR SUPPORT. CORRODED. FWD GALLEY FLOOR SUPPORT AT Y-81 FR 14R, 15R AND 16R CORRODED. FWD GALLEY FLOOR SUPPORT AT Y-81 FR12R-16R REPLACED AS PER A320 SRM 53-11-15 FIG 203.
- [SDR AWXA0001996](https://openairdocs.org/sdr/AWXA0001996), Jun 29, 2001: FLOOR SUPPORT. CORRODED. AFT CABIN FLOOR SUPPORT AT Y1162 FR 66R AND 69R SCREW CLIP ATTACH HOLE CORRODED. AFT GALLEY FLOOR SUPPORT AT Y1162 FR66R-69R REPLACED AS PER A320 SRM 51-42-11 P
- [SDR AWXA0001995](https://openairdocs.org/sdr/AWXA0001995), Jun 29, 2001: SEAT TRACK. CORRODED. D: Fwd galley floor support at Y1292 Fr 14R and 16R corrodedC: Fwd galley support/seat track at Y1292 FR12R-16R replaced as per A320 SRM 53-11-15 fig. 203
- [SDR AWXA0001994](https://openairdocs.org/sdr/AWXA0001994), Jun 29, 2001: STRINGER. MISDRILLED. D: Fr 66 L/H STR 43 has double drilled holesC: Stringer repaired as per SRM 53-00-13 Fig. 201 from sta .3152 to 3167
- [SDR AWXA0001993](https://openairdocs.org/sdr/AWXA0001993), Jun 29, 2001: FLOOR SUPPORT. DAMAGED. AFT CABIN FLOOR SUPPORT AT Y1292 RT FR 68 SCREW HOLES DAMAGED. REPLACED FLOOR SUPPORT PER SRM 53-41-11.
- [SDR AWXA0001374](https://openairdocs.org/sdr/AWXA0001374), Feb 19, 2001: ACTUATOR. CONTAMINATED. PHX - EMERGENCY LANDING - 2/12/01 - ON APPROACH, THE CREW GOT AN ECAM WARNING, F/CTL SLATS FAULT AND THE CREW DECLARED AN EMERGENCY; AN UNEVENTFUL LANDING WAS M
- [SDR AWXA0001282](https://openairdocs.org/sdr/AWXA0001282), Feb 8, 2001: RESOLVER. MALFUNCTIONED. MAINTENANCE TROUBLESHOT IAW TSR 73-22-00-810-851 AND IAE TELEX; CELL CODE FAULT OF 59 ON FMU/HC/EEC 1 MESSAGE; (WFXCF) FUEL FLOW RESOLVER FAULT; CH B ON CONNECT
- [SDR AWXA0001281](https://openairdocs.org/sdr/AWXA0001281), Feb 8, 2001: FMU. MALFUNCTIONED. PHX - AIR TURNBACK - 2/3/01 - DURING INITIAL CLIMB, LEFT ENG UNCOMMANDED THRUST INCREASE ABOVE CLIMB EPR LIMIT WITH DEFINITE YAW TO THE RIGHT; EVENT WAS MOMENTA
- [SDR AWXA0000575](https://openairdocs.org/sdr/AWXA0000575), Aug 21, 2000: WINDOW. CRACKED. AIR TURNBACK, F/O WINDSHIELD CRACKED IN FLIGHT AT APPROX 23000 FT AT 290 KTS IN THE CLIMBOUT. PRESSURE IN THE CABIN WAS NORMAL. REPLACED F/O WINDSHIELD, REMOVED
- [SDR AWXA0000186](https://openairdocs.org/sdr/AWXA0000186), Mar 30, 2000: POWER SUPPLY. FAILED. EMERGENCY LIGHTS AT SEAT ROW 3 & 7 INOP. WHEN COMMANDED FROM COCKPIT OR FWD FLT ATTENDANT PANEL--WORKS WITH BREAKER H5 PULLED. REPLACED PWR SUPPLY UNIT AT 11 WL
- [SDR AWXA0000153](https://openairdocs.org/sdr/AWXA0000153), Mar 22, 2000: STRAP. CORRODED. C-CHECK, CABIN FLOOR PANEL 22FF JOIN STRIP CORRODED. CLEANED, PRIMED, AND PAINTED FLOOR STRIP IAW A320 SRM 51-75-00.
- [SDR AWXA0000152](https://openairdocs.org/sdr/AWXA0000152), Mar 22, 2000: SEAT TRACK. CORRODED. C-CHECK, CABIN SEAT TRACK NR 2 Y765 LT FRAME 20 CORRODED. REPAIRED CORROSION IAW A320 SRM 53-00-15 FIG 101.
- [SDR AWXA9900313](https://openairdocs.org/sdr/AWXA9900313), Sep 13, 1999: PWR SUPPLY. INOP. EMERGENCY EXITS OVERWING RIGHT AND AISLE AFT CENTER REMAIN ON. REMOVED AND REPLACED RT OVERWING EMERG LIGHT POWER SUPPLY.
- [SDR AWXA9900297](https://openairdocs.org/sdr/AWXA9900297), Sep 5, 1999: ACTUATOR. LEAKING. CREW REPORTED GREEN HYDRAULIC SYSTEM LOW IN FLIGHT. AT CRUISE, LF 370, HYD GREEN LOW LEVEL ECAM MESSAGE. ACCOMPLISHED ECAM ACTIONS AND CONTINUED FLIGHT FOR UNEV
- [SDR AWXA9900276](https://openairdocs.org/sdr/AWXA9900276), Aug 30, 1999: HYD LINE. LOOSE. EMERGENCY DECLARED, HYD GREEN LOW LEVEL RESULTING IN LOSS OF GREEN HYDRAULIC SYSTEM. INSPECTED SYSTEMS, NO LEAKS NOTED. FOUND GREEN SYS 5 QTS LOW. SERVICED QTY,
- [SDR AWXA9700653](https://openairdocs.org/sdr/AWXA9700653), Nov 1, 1997: MANIFOLD. LEAKING. YELLOW HYDRAULIC SYSTEM LOST QUANTITY IN FLIGHT. DECLARED AN EMERGENCY LANDING. FOUND THE SERVICE MANIFOLD LEAKING. REMOVED AND REPLACED MANIFOLD.
- [SDR AWXA9700454](https://openairdocs.org/sdr/AWXA9700454), Aug 2, 1997: FAN. INOPERATIVE. ON DEPARTURE, NOTICED SLIGHT BURNING ODOR IN COCKPIT. CHECKED COND PAGE AND FOUND COCKPIT FAN INOP. REMOVED AND REPLACED FWD CABIN RECIRCULATION FAN, OPS CHECK 
- [SDR AWXA9700284](https://openairdocs.org/sdr/AWXA9700284), May 7, 1997: BATTERY PACK. DISCHARGED. DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT BATTERY PACK 11WL INOP. REMOVED AND REPLACED BATTERY PACK 11WL, OPS CHECK NORMAL AT THIS TIME.

All 51: https://openairdocs.org/deregistered/N645AW-2006-05-10/reports.md

## Other aircraft with N645AW

- [Registered now](https://openairdocs.org/aircraft/N645AW): Piper PA-28-161, S/N 28-8116305, built 1981

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