# N7247Y: 1975 Beech A200, registration cancelled 2026-02-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 4, 2026
- Exported to: Brazil
- Status when cancelled: Sale reported
- Airframe: [Beech A200](https://openairdocs.org/model/beech-a200) (registry code 1152921)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Serial number: BC-03
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, normal
- Airworthiness date: March 21, 2023
- Last registry action: January 21, 2026
- Mode S code: A9B5CC
- Location: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx)
- Owner type: Individual
- The mark today: https://openairdocs.org/aircraft/N7247Y
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7247Y
- Page: https://openairdocs.org/deregistered/N7247Y-2026-02-04

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 A200: https://openairdocs.org/model/beech-a200.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 B3OR20041029](https://openairdocs.org/sdr/B3OR20041029), Sep 22, 2004: ATTACH FITTING. DAMAGED. ON 22 SEPTEMBER 2004 A 5 YEAR WING BOLT INSPECTION WAS COMPLIED WITH ON A BEECHCRAFT A200 AIRCRAFT. THREE OF THE WING ATTACH FITTINGS WERE FOUND TO HAVE DAMAGE 
- [SDR B3OR20033014](https://openairdocs.org/sdr/B3OR20033014), Aug 4, 2003: FLAP TRACK. CORRODED. DURING A 14 DAY CORROSION INSPECTION THE LEFT OUTBOARD FLAP TACK WAS FOUND TO HAVE EXIFOLIATION FLAKING CORROSION ON THE FLAP TRACK. THE FLAKING WAS SEVERE ENOU
- [SDR B3OR20033013](https://openairdocs.org/sdr/B3OR20033013), Aug 4, 2003: FLAP TRACK. CORRODED. DURING A 14 DAY CORROSION INSPECTION THE RIGHT HAND OUTBOARD FLAP TRACK WAS FOUND TO HAVE EXIFOLIATION FLAKING CORROSION ON THE FLAP TRACK. THE FLAKING WAS SEVE
- [SDR B3OR20033012](https://openairdocs.org/sdr/B3OR20033012), Aug 4, 2003: FLAP TRACK. CORRODED. DURING A 14 DAY CORROSION INSPECTION THE RIGHT HAND INBORAD FLAP TRACK WAS FOUND TO HAVE DEEP EXIFOLLIATION FLAKING CORROSION ON THE INBOARD SIDE OF THE TRACK.T
- [SDR B3OR2003009](https://openairdocs.org/sdr/B3OR2003009), Jun 5, 2003: HINGE BRACKET. CORRODED. MECH NOTICED (PAINT BUBBLING) ON, UPPER RUDDER HINGE BRACKET. ON INVESTIGATION, CORROSION WAS FOUND. FLAKING, CORROSION WAS TOO DEEP INTO METAL OF HINGE BRACKET
- [SDR B3OR2003008](https://openairdocs.org/sdr/B3OR2003008), Jun 5, 2003: HINGE. CORRODED. DURING A 15 DAY CORROSION INSP, MECH NOTICED "PAINT BUBBLEING" ON MIDDLE RUDDER HINGE BRACKET. UPON INVESTIGATION, CORROSION FOUND. ATTEMPT WAS MADE TO CLEAN & 
- [SDR B3OR2003006](https://openairdocs.org/sdr/B3OR2003006), Jun 5, 2003: HINGE BRACKET. CORRODED. MECH NOTICED (PAINT BUBBLING) ON LT AND RT, MIDDLE ELEVATOR HINGE. FURTHER INVESTIGATION BY SCRAPEING-OFF PAINT BUBBLE, CORROSION WAS FOUND. ATTEMPT WAS MADE TO

## 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 20250213001389I](https://openairdocs.org/incident/20250213001389I), Feb 13, 2025: Beech A200 (N7247Y), Hays, KS, Minor damage. While in cruise flight, FL270, the left front windscreen cracked/shattered. The pilot executed an emergency descent and landed safely at khys without further…

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