# N8411P: Piper PA-24-250, registration cancelled 1991-01-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 29, 1991
- Status when cancelled: Triennial form not returned
- Airframe: [Piper PA-24-250](https://openairdocs.org/model/piper-pa-24-250) (registry code 7102404)
- Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15) (OpenAirDocs)
- Serial number: 243666
- Type of aircraft: Fixed wing single engine
- Certificate issued: March 7, 1981
- Last registry action: January 4, 1991
- Mode S code: AB8619
- Owners when cancelled: [Falter Dale H](https://openairdocs.org/faa-owner/FALTER%20DALE%20H), [Dionne Alfred F](https://openairdocs.org/faa-owner/DIONNE%20ALFRED%20F), [Falter Joan C](https://openairdocs.org/faa-owner/FALTER%20JOAN%20C)
- Location: [El Cajon, CA](https://openairdocs.org/faa-place/CA/El%20Cajon)
- Owner type: Partnership
- Owner's area on the map: 32.8329° N, 116.8734° W: Placed by OpenAirDocs at the center of ZIP code 92021, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8411P
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8411P
- Page: https://openairdocs.org/deregistered/N8411P-1991-01-29

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 Piper PA-24-250: https://openairdocs.org/model/piper-pa-24-250.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19840616044279I](https://openairdocs.org/incident/19840616044279I), Jun 16, 1984: Piper PA24250 (N8411P), Calistoga, CA, Minor damage. Blamed distraction of glider activity and landed gear up. The landing gear warning horn was inoperative.

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