# N232TA: 1980 Boeing 737-296, registration cancelled 2013-08-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 6, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Boeing 737-296](https://openairdocs.org/model/boeing-737-296) (registry code 1384486)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22277
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 19, 1994
- Last registry action: June 18, 2010
- Mode S code: A21198
- Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie)
- Owner type: Individual
- Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N232TA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=232TA
- Page: https://openairdocs.org/deregistered/N232TA-2013-08-06

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 Boeing 737-296: https://openairdocs.org/model/boeing-737-296.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 2001F00149](https://openairdocs.org/sdr/2001F00149), Jul 5, 2001: ENGINE. DAMAGED. SAL - FLT TA220 - DURING INITIAL TAKEOFF, A STRONG NOISE WAS HEARD, WHEN APPLYING TAKEOFF TRUST, REJECTED THE TAKEOFF AND STRONG VIBRATION WAS FELT IN THE NR 2 
- [SDR 2001F00081](https://openairdocs.org/sdr/2001F00081), Apr 16, 2001: HOSE. LEAKING. FLT 410 - SAL - DURING CLIMB, THE CAPTAIN REPORTED THAT DURING INITIAL CLIMB THERE WAS A DIFFERENCE OF 100 FEET BETWEEN CAPTAIN AND FIRST OFFICER ALTIMETER, AT 
- [SDR 20001212SH001](https://openairdocs.org/sdr/20001212SH001), Nov 26, 2000: LINE. DAMAGED. SAL - FLT TA-380 - AFTER TAKEOFF, THE FIRST OFFICER AIRSPEED INDICATOR WENT TO ZERO KNOTS AND FIRST OFFICER''S ALTIMETER HAD A READ-OUT OF 4,000 FEET AT FL 260.
- [SDR 20001004AP002](https://openairdocs.org/sdr/20001004AP002), Jun 23, 2000: CONTROL BOX. INOPERATIVE. SAL-MIA - FLT TA314 - DURING CRUISE, THE AIRCRAFT HAD PITCH OSCILLATIONS WITH AUTOPILOT ENGATED, DUE THIS SITUATION THE AIRCRAFT RETURNED TO SAL AIRPORT. AFTER 
- [SDR 20000424AP011](https://openairdocs.org/sdr/20000424AP011), Mar 19, 1999: FIRE DETECTOR. MALFUNCTIONED. CUN - FLT TA410 - ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLISHED BY THE CREW, DUE THIS SITUATION THE 
- [SDR 20000420AP003](https://openairdocs.org/sdr/20000420AP003), Mar 19, 1999: FIRE LOOP. DAMAGED. DURING FLIGHT TA410 (SAL-IAH) ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLISHED BY THE CREW, DUE TO THIS

## Other aircraft with N232TA

- [Registered now](https://openairdocs.org/aircraft/N232TA): Cessna 650, S/N 650-0128

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