# N4269S: 1977 Beech 58P, registration cancelled 2020-11-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 12, 2020
- Exported to: Argentina
- Status when cancelled: Second renewal notice
- Airframe: [Beech 58P](https://openairdocs.org/model/beech-58p) (registry code 1152744)
- Engine: [Continental TSIO-520 series](https://openairdocs.org/engine/continental-tsio-520-series) (registry code 17040)
- Data sheets: [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS E8CE](https://openairdocs.org/tcds/E8CE) (OpenAirDocs)
- Serial number: TJ-96
- Year built: 1977
- Type of aircraft: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: April 7, 1977
- Certificate issued: December 4, 2017
- Last registry action: December 4, 2017
- Mode S code: A5158D
- Owner when cancelled: [Strong Tower Services LLC Trustee](https://openairdocs.org/faa-owner/STRONG%20TOWER%20SERVICES%20LLC%20TRUSTEE)
- Location: [New Castle, DE](https://openairdocs.org/faa-place/DE/New%20Castle)
- Owner type: LLC
- Owner's area on the map: 39.6466° N, 75.6048° W: Placed by OpenAirDocs at the center of ZIP code 19720, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N4269S
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=4269S
- Page: https://openairdocs.org/deregistered/N4269S-2020-11-12

From the FAA registry file of November 5, 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 Beech 58P: https://openairdocs.org/model/beech-58p.md

## Service difficulty reports (2)

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

- [SDR 20010223CW005](https://openairdocs.org/sdr/20010223CW005), Jan 23, 2001: PROBE. BROKEN. CUSTOMER REPORTED NR1 EGT ON HIS GEM 1200, INOPERATIVE. UPON REMOVAL OF EGT PROBE, ABOUT HALF OF THE PROBE TIP WAS BROKEN OFF AND MISSING. THE ONLY PATH OF EXIT
- [SDR 96ZZZX2771](https://openairdocs.org/sdr/96ZZZX2771), Apr 1, 1996: COUPLING. CRACKED. CLAMP WAS FOUND CRACKED WHEN REMOVED FOR OTHER MAINTENANCE ON THE EXHAUST SYSTEM. SUBMITTER SUSPECTS CLAMP WAS OVERTORQUED AT PRIOR INSTALLATION. FAILURE OF THI

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