# N2164S: 1975 Cessna T210L, registration cancelled 2015-01-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 13, 2015
- Exported to: Mexico
- Status when cancelled: First renewal notice
- Airframe: [Cessna T210L](https://openairdocs.org/model/cessna-t210l) (registry code 2073449)
- Engine: [Continental TSIO-520 series](https://openairdocs.org/engine/continental-tsio-520-series) (registry code 17040)
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS E8CE](https://openairdocs.org/tcds/E8CE) (OpenAirDocs)
- Serial number: 21061125
- Year built: 1975
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: December 16, 1975
- Certificate issued: April 26, 2012
- Last registry action: April 26, 2012
- Mode S code: A1D2C1
- Owner when cancelled: [Red Horse Properties LLC](https://openairdocs.org/faa-owner/RED%20HORSE%20PROPERTIES%20LLC)
- Location: [Livingston, TX](https://openairdocs.org/faa-place/TX/Livingston)
- Owner type: Corporation
- Owner's area on the map: 30.7178° N, 94.8172° W: Placed by OpenAirDocs at the center of ZIP code 77351, within about 14 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N2164S
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2164S
- Page: https://openairdocs.org/deregistered/N2164S-2015-01-13

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 Cessna T210L: https://openairdocs.org/model/cessna-t210l.md

## Service difficulty reports (1)

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

- [SDR 2005FA0000697](https://openairdocs.org/sdr/2005FA0000697), Dec 14, 2004: PRESSURE SWITCH. FAILED. LANDING GEAR FAILED TO FULLY RETRACT AFTER TAKEOFF. FOUND THAT THE WIRE SOLDERED TO THE HYDRAULIC POWER PACK PRESSURE SWITCH HAD CORRODED BENEATH THE HEAT-SHRIN

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