- Registered owner
- Evans Scott A
- Location
- Van Horn, TX
- Owner type
- Individual
- Serial number
- JA532-10-18
- Year built
- 2022
- Type
- Fixed wing single engine
- Engine
- 4 cycle
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- June 8, 2022
- Certificate issued
- October 3, 2025
- Expires
- October 31, 2032
- Mode S code
- A1C8DB
- Kit
- Just Aircraft LLC HIGHLANDER
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N214FMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Mark Duffy HIGHLANDER aircraft
FAA incident reports
No FAA accident or incident reports matched to N214FMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Mark Duffy HIGHLANDER aircraft
Service difficulty reports
No reports matched to N214FGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Mark Duffy HIGHLANDER aircraft
Reports on N214F not matched to an aircraft · 8
They name N214F, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 20000425SH030Skin · corrodedFOUND DURING SCHEDULED B-SERVICE CHECK, CORROSION ON INTERNAL SKIN AROUND LEFT SCAN LIGHT. CORROSION POSSIBLY CAUSED BY MOISTURE AROUND THE EDGES OF LIGHT ASSY LEAKING INTO FUSELAGE AREA. (X)SDR 20000425SH029Stringer · crackedFOUND DURING SCHEDULED B-CHECK, CRACK AT END OF STR 15L BS 720C AFT OF SCAN LIGHT. STRINGER CRACK WAS POSSIBLY CAUSED BY CORROSION FOUND IN THIS AREA. (X)SDR 20000425SH028Stringer · crackedFOUND DURING SCHEDULED B-CHECK, STRINGER 15R CRACKED AT END. BS 720B FORWARD OF SCAN LIGHT. STRINGER CRACK WAS POSSIBLY CAUSED BY CORROSION FOUND IN THIS AREA. (X)
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.