# N1160C: 1953 Piper PA-20, registration cancelled 2012-06-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 7, 2012
- Exported to: New Zealand
- Status when cancelled: Valid registration
- Airframe: [Piper PA-20](https://openairdocs.org/model/piper-pa-20) (registry code 7102002)
- Engine: [Lycoming 0-290 series](https://openairdocs.org/engine/lycoming-0-290-series) (registry code 41506)
- Data sheets: [TCDS 1A4](https://openairdocs.org/tcds/1A4), [TCDS E-229](https://openairdocs.org/tcds/E-229) (OpenAirDocs)
- Serial number: 20-962
- Year built: 1953
- Type of aircraft: Fixed wing single engine
- Engine type: 4 cycle
- Airworthiness: Standard, normal
- Airworthiness date: February 24, 1956
- Certificate issued: April 5, 2010
- Last registry action: February 2, 2011
- Mode S code: A044D8
- Owner when cancelled: [Adams Patrick M](https://openairdocs.org/faa-owner/ADAMS%20PATRICK%20M)
- Location: [Havana, FL](https://openairdocs.org/faa-place/FL/Havana)
- Owner type: Individual
- Owner's area on the map: 30.6077° N, 84.4176° W: Placed by OpenAirDocs at the center of ZIP code 32333, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N1160C
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1160C
- Page: https://openairdocs.org/deregistered/N1160C-2012-06-07

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 Piper PA-20: https://openairdocs.org/model/piper-pa-20.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 98ZZZX2716](https://openairdocs.org/sdr/98ZZZX2716), Jul 9, 1998: CYLINDER. DEFECTIVE. TWO OF FOUR NEW COMPLETE CYLINDER ASSEMBLIES WERE DEFECTIVE. ONE CYLINDER HAD BEAT ROCKER SHAFT BOSSES, THE OTHER HAD A CRACK IN THE EXHAUST PORT.
- [SDR 98ZZZX2715](https://openairdocs.org/sdr/98ZZZX2715), Jul 9, 1998: CYLINDER. DEFECTIVE. TWO OF FOUR NEW COMPLETE CYLINDER ASSEMBLIES WERE DEFECTIVE. ONE CYLINDER HAD BEAT ROCKER SHAFT BOSSES, THE OTHER HAD A CRACK IN THE EXHAUST PORT.
- [SDR 98ZZZX2677](https://openairdocs.org/sdr/98ZZZX2677), Jul 9, 1998: CYLINDER. CRACKED. DURING THE ANUAL INSPECTION, DISCOVERED CRACKS IN THREE OF FOUR CYLINDERS. THE CRACKS WERE LOCATED IN THE EXHAUST PORT. A CYLINDER COMPRESSION CHECK DID NOT REV

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