# N680TA: 2008 Airbus A320-233, registration cancelled 2020-12-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 7, 2020
- Exported to: Pakistan
- Status when cancelled: Valid registration
- Airframe: [Airbus A320-233](https://openairdocs.org/model/airbus-a320-233) (registry code 3940329)
- Engine: [IAE V2527-A5](https://openairdocs.org/engine/iae-v2527-a5) (registry code 34604)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM), [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs)
- Serial number: 3538
- Year built: 2008
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 4, 2008
- Certificate issued: August 5, 2020
- Last registry action: August 5, 2020
- Mode S code: A904E1
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N680TA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=680TA
- Page: https://openairdocs.org/deregistered/N680TA-2020-12-07

From the FAA registry file of November 3, 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 A320-233: https://openairdocs.org/model/airbus-a320-233.md

## Service difficulty reports (3)

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

- [SDR SOKF20191208007](https://openairdocs.org/sdr/SOKF20191208007), Dec 4, 2019: FITTING. WORN. DURING CLIMB, THE AIRCRAFT RETURN TO LIM DUE TO HIGH VIBRATION DURING CLIMB BETWEEN FL 050 AND FL 270 . SPEED BETWEEN 200-300 KTS. VIBRATION MODERATE FELT IN AL
- [SDR SOKF20130828012](https://openairdocs.org/sdr/SOKF20130828012), Aug 26, 2013: SOLENOID VALVE. MALFUNCTIONED. NR 2 ENGINE EGT OVER LIMIT DURING CLIMB, THRUST EGT EXCEEDED LIMITS. EGT WENT CLOSE TO 670 CELSIUS DEGREES FOR 10 SECONDS THEN REDUCED TO LOWER EGT. R & R HPC 1
- [SDR SOKF20130605003](https://openairdocs.org/sdr/SOKF20130605003), Jun 1, 2013: CHECK VALVE. FAILED. LOSS OF HYD YELLOW SYS DUE TO RESERVOIR LOW LEVEL. FOLLOWED TSM 29-13-00-810-016 WAS R & R CHECK VALVE (3050GM) PERFORMED IDLE LEAK TEST OK NORMAL IAW AMM 29-13

## Other aircraft with N680TA

- [Registered now](https://openairdocs.org/aircraft/N680TA): Costruzioni Aeronautiche Tecna P2012 TRAVELLER, S/N 086/US

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.