# N2437S: 1976 Cessna 210L, registration cancelled 2020-05-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 6, 2020
- Exported to: Bolivia
- Status when cancelled: Valid registration
- Airframe: [Cessna 210L](https://openairdocs.org/model/cessna-210l) (registry code 2073448)
- Engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032)
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS E5CE](https://openairdocs.org/tcds/E5CE) (OpenAirDocs)
- Serial number: 21061281
- Year built: 1976
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard
- Last registry action: March 26, 2020
- Mode S code: A23E82
- Owner when cancelled: [Aviasol LLC](https://openairdocs.org/faa-owner/AVIASOL%20LLC)
- Location: [Lees Summit, MO](https://openairdocs.org/faa-place/MO/Lees%20Summit)
- Owner type: LLC
- Owner's area on the map: 38.9844° N, 94.3396° W: Placed by OpenAirDocs at the center of ZIP code 64064, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N2437S
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2437S
- Page: https://openairdocs.org/deregistered/N2437S-2020-05-06

From the FAA registry file of October 31, 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 210L: https://openairdocs.org/model/cessna-210l.md

## Service difficulty reports (7)

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

- [SDR FPI2012F00011](https://openairdocs.org/sdr/FPI2012F00011), Jun 29, 2012: CYLINDER HEAD. CRACKED. DURING 100 HR INSPECTION, COMPRESSION TEST, LEAK CHECK WITH SOAPY WATER FOUND A CRACK IN CYLINDER HEAD FROM TOP OF SPARK PLUG HOLE TO INTAKE VALVE. REPLACED WIT
- [SDR FPI2012F00010](https://openairdocs.org/sdr/FPI2012F00010), Jun 29, 2012: CYLINDER. LEAKING. DURING A 100 HOUR INSPECTION, COMPRESSION TEST LEAK CHECK WITH SOAPY WATER, A CRACK WAS FOUND AT FIRST FIN, INTO COMBUSTION CHAMBER. REPLACED WITH NEW CYLINDER 
- [SDR FPI2012F00005](https://openairdocs.org/sdr/FPI2012F00005), Mar 2, 2012: CYLINDER. CRACKED. DURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LON
- [SDR FPIA2012F00004](https://openairdocs.org/sdr/FPIA2012F00004), Mar 2, 2012: CYLINDER. CRACKED. DURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LON
- [SDR FPI2006F00002](https://openairdocs.org/sdr/FPI2006F00002), Jan 10, 2006: CYLINDER HEAD. CRACKED. CRACKED AT BARREL AND HEAD. (K)
- [SDR FPI2006F00001](https://openairdocs.org/sdr/FPI2006F00001), Jan 10, 2006: CYLINDER. CRACKED. CRACKED AT BARREL AND HEAD. (K)
- [SDR 20000811SH007](https://openairdocs.org/sdr/20000811SH007), Jul 27, 2000: MOUNT. DEFECTIVE. PART LABELLED/MANUFACTURED WRONG. NOTICED LT FORWARD ENGINE MOUNT SAGGING. UPON FURTHER INSPECTION, FOUND PART LABELLED ''TOP FORWARD MTG'', BUT DID NOT HAVE RE

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