# N224EA: 1980 Hawker Siddeley HS.125 SERIES 700A, registration cancelled 2019-01-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 16, 2019
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Hawker Siddeley HS.125 SERIES 700A](https://openairdocs.org/model/hawker-siddeley-hs-125-series-700a) (registry code 4230170)
- Engine: [Garrett TFE731-3R](https://openairdocs.org/engine/garrett-tfe731-3r) (registry code 29093)
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Serial number: 257088
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Experimental, research and development
- Airworthiness date: May 14, 2009
- Certificate issued: November 14, 2018
- Last registry action: November 14, 2018
- Mode S code: A1F042
- Owner when cancelled: [Vica Aviation Inc](https://openairdocs.org/faa-owner/VICA%20AVIATION%20INC)
- Location: [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle)
- Owner type: Corporation
- Owner's area on the map: 47.6005° N, 122.3322° W: Placed by OpenAirDocs at the center of ZIP code 98104, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N224EA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=224EA
- Page: https://openairdocs.org/deregistered/N224EA-2019-01-16

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 Hawker Siddeley HS.125 SERIES 700A: https://openairdocs.org/model/hawker-siddeley-hs-125-series-700a.md

## Service difficulty reports (5)

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

- [SDR 2007FA0000192](https://openairdocs.org/sdr/2007FA0000192), Feb 27, 2007: SKIN. CORRODED. RT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY, IT WAS DETERMNED TO BE BEYOND ECONOMICAL REPAIR. RT WING L
- [SDR 2007FA0000191](https://openairdocs.org/sdr/2007FA0000191), Feb 27, 2007: SKIN. CORRODED. RT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. RT WING L
- [SDR 2007FA0000194](https://openairdocs.org/sdr/2007FA0000194), Feb 21, 2007: SKIN. CORRODED. LT AND RT HORIXONTAL STABILIZER LEADING EDGES HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY, IT WAS DETERMINED TO BE BEYOND ECONO
- [SDR 2005FA0000010](https://openairdocs.org/sdr/2005FA0000010), Dec 7, 2004: CLAMP. CRACKED. THE DEFECT IS A FATIGUE CRACK, CAUSED BY BEING OVERSTRESSED DUE TO LOAD LIMITS, POSSIBLE OVERTORQUED. MAYBE THIS PART SHOULD BE MADE STRONGER, TO HANDLE THE STR
- [SDR 20000516SH008](https://openairdocs.org/sdr/20000516SH008), Feb 28, 2000: RIVET. MISINSTALLED. SKIN ATTACHING TO THE FWD MOST FRAME IS ''''''''DOUBLE FLUSH'''''''' RIVETED. THE RIVETS AT THIS AREA SECURE .0937 INCH WORTH OF MATERIAL. THIS AREA IS IN AN AR

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.