# N478TA: 2004 Airbus A319-132, registration cancelled 2018-09-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 8, 2018
- Status when cancelled: First renewal notice
- Airframe: [Airbus A319-132](https://openairdocs.org/model/airbus-a319-132) (registry code 3940015)
- Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 2339
- Year built: 2004
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 20, 2004
- Certificate issued: November 19, 2004
- Last registry action: December 22, 2015
- Mode S code: A5E07C
- 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/N478TA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=478TA
- Page: https://openairdocs.org/deregistered/N478TA-2018-09-08

From the FAA registry file of November 4, 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 A319-132: https://openairdocs.org/model/airbus-a319-132.md

## Service difficulty reports (6)

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

- [SDR 5TTY2018011700001](https://openairdocs.org/sdr/5TTY2018011700001), Jan 16, 2018: SWITCH. FAULTY. LIM TO MEX. PER TSM, IT WAS FOUND A FAULTY GREEN HYD SYSTEM LOW LEVEL SW. FAULTY SWITCH WAS REPLACED AND TEST PERFORMED PER AMM WITH NOT DUPLICATION OF FAILURE.
- [SDR RJEF20170929001](https://openairdocs.org/sdr/RJEF20170929001), Sep 27, 2017: IDG. OVERSERVICED. DURING CLIMB, THE IDG 1 TEMPERATURE INCREASED AND THE ECAM MESSAGE ELEC IDG1 OIL OVERHEAT DISPLAYED, THE AIRCRAFT RETURNED TO DEPARTURE. UNEVENTFUL LANDING. MAI
- [SDR 5TTY2017050300001](https://openairdocs.org/sdr/5TTY2017050300001), May 3, 2017: HYDRAULIC LINE. DAMAGED. DURING THE FIRST 2,000 FT AND BEFORE FLAP RETRACTION IN FLIGHT TAI 365 DEPARTED FROM SAL TO BOG, GREEN LOW PRESS AND PTU INOP. INDICATIONS WERE DISPLAYED ON ECA
- [SDR RJEF20140815001](https://openairdocs.org/sdr/RJEF20140815001), Aug 14, 2014: VALVE. DEFECTIVE. AT THE ARRIVAL OF THE ACFT THE PILOT REPORTED ENG 1 BEARING 4 OIL SYS HIGH PRESS. CONSEQUENTLY, THE ACFT WAS DECLARED AOG FOR MX. IAW TSM 79-20-00-810-809A, BEA
- [SDR RJEF20131210011](https://openairdocs.org/sdr/RJEF20131210011), Dec 8, 2013: ANTI-ICE SYSTEM. MALFUNCTIONED. DURING THE DISPATCH OF FLIGHT TA583 FROM IAD TO SAL, THE PILOT REPORTED THAT THE ACFT HAVE FAILURES, WING ANTI ICE SYS FAULT & ENG 1 FIRE LOOP B FAULT, DUE TO T
- [SDR RJEF2012071202](https://openairdocs.org/sdr/RJEF2012071202), Jul 10, 2012: TRANSCEIVER. INOPERATIVE. DURING CLIMB OF THE AIRCRAFT AS FLIGHT LR-604 FROM SJO TO LAX, THE PILOT IN COMMAND REPORTED: DURING CLIMB WEATHER RADAR STOPPED AT LEAST 4 TIMES, ALL RADAR IND

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