# N9628E: 1946 Aeronca 11AC, registration cancelled 2008-02-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 27, 2008
- Status when cancelled: Triennial form not returned
- Airframe: [Aeronca 11AC](https://openairdocs.org/model/aeronca-11ac) (registry code 0191102)
- Engine: [Continental A&C65 series](https://openairdocs.org/engine/continental-a-c65-series) (registry code 17003)
- Data sheets: [TCDS A-761](https://openairdocs.org/tcds/A-761), [TCDS E-205](https://openairdocs.org/tcds/E-205) (OpenAirDocs)
- Serial number: 11AC-1266
- Year built: 1946
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard
- Certificate issued: September 24, 2002
- Last registry action: September 20, 2005
- Mode S code: AD6709
- Owners when cancelled: [Schicora William](https://openairdocs.org/faa-owner/SCHICORA%20WILLIAM), [Schicora Karen](https://openairdocs.org/faa-owner/SCHICORA%20KAREN)
- Location: [Winchester, CA](https://openairdocs.org/faa-place/CA/Winchester)
- Owner type: Co-owned
- Owner's area on the map: 33.6626° N, 117.0439° W: Placed by OpenAirDocs at the center of ZIP code 92596, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N9628E
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9628E
- Page: https://openairdocs.org/deregistered/N9628E-2008-02-27

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 Aeronca 11AC: https://openairdocs.org/model/aeronca-11ac.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 2004FA0000562](https://openairdocs.org/sdr/2004FA0000562), Jul 13, 2004: SPAR. CRACKED. LT AFT WING SPAR HAD A VERTICAL COMPRESSION CRACK AT THE OB EDGE OF THE LIFT STRUT PLATE. ALSO, IT WAS CRACKED HORIZONTALLY FROM THE COMPRESSION CRACK TO THE OB

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