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Aircraft record

N224EA1980 Hawker Siddeley HS.125 SERIES 700A

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jan 16, 2019.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched5 service difficulty reports

Registration
Deregistered
Last based in
Seattle, WA
owner city / state
Owners
1
since 2018
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
5
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Vica Aviation INC
Owner type
Corporation
City, state
Seattle, WA
Certificate issued
Nov 14, 2018
Canceled
Jan 16, 2019
Airworthiness
Experimental · Research and Development
Airworthiness date
May 14, 2009

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Hawker Siddeley
Model
HS.125 SERIES 700A
Year
1980
Serial number
257088
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
15
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
A1F042

Engine

Make and model
Garrett Tfe731-3r
Type
Turbo-fan
Power
3,880 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2018 – 2019Vica Aviation INCSeattle, WA

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (5)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Wings · skin · corrodedFeb 27, 2007

    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 LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEAR PRIOR TO THIS DISCOVERY. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedFeb 27, 2007

    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 LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · corrodedFeb 21, 2007

    LT AND RT HORIXONTAL STABILIZER LEADING EDGES HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY, IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. THIS AREA HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reports
  • Exhaust · clamp · crackedDec 7, 2004

    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 STRESS. THIS DEFECT WAS FOUND BY A PENETRANT INSPECTION. THE LOCKING NUT NEEDS TO BE REMOVED, IN THIS CASE THE DEFECT WOULD NOT HAVE BEEN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · rivet · misinstalledFeb 28, 2000

    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 AREA WHERE A LOT OF VIBRATION EXISTS FROM THE ENGINE FAN; ALSO, IT IS SUSCEPTIBLE TO CHAFING WHERE IT MATES WITH INLET COWL. THESE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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