# N214F: 2022 Mark Duffy HIGHLANDER

- Status: Valid registration
- Airframe: [Mark Duffy HIGHLANDER](https://openairdocs.org/model/mark-duffy-highlander) (registry code 056400J, 2 seats)
- Engine: [Rotax 914ULS](https://openairdocs.org/engine/rotax-914uls) (registry code 55552)
- Serial number: JA532-10-18
- Year built: 2022
- Type: Fixed wing single engine
- Engine type: 4 cycle
- Kit: Just Aircraft LLC HIGHLANDER
- Airworthiness: Experimental, amateur built
- Airworthiness date: June 8, 2022
- Certificate issued: October 3, 2025
- Expires: October 31, 2032
- Mode S code: A1C8DB
- Registered owner: [Evans Scott A](https://openairdocs.org/faa-owner/EVANS%20SCOTT%20A)
- Location: [Van Horn, TX](https://openairdocs.org/faa-place/TX/Van%20Horn)
- Owner type: Individual
- Owner's area on the map: 30.9309° N, 104.8607° W: Placed by OpenAirDocs at the center of ZIP code 79855, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=214F
- Page: https://openairdocs.org/aircraft/N214F

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Mark Duffy HIGHLANDER)

None in force.

### Matched by engine (Rotax 914ULS)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N214F.

## FAA accident and incident reports

None matched to N214F.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty 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 20000425SH030](https://openairdocs.org/sdr/20000425SH030), Jan 14, 2000: SKIN. CORRODED. FOUND DURING SCHEDULED B-SERVICE CHECK, CORROSION ON INTERNAL SKIN AROUND LEFT SCAN LIGHT. CORROSION POSSIBLY CAUSED BY MOISTURE AROUND THE EDGES OF LIGHT ASSY 
- [SDR 20000425SH029](https://openairdocs.org/sdr/20000425SH029), Jan 14, 2000: STRINGER. CRACKED. FOUND 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 20000425SH028](https://openairdocs.org/sdr/20000425SH028), Jan 14, 2000: STRINGER. CRACKED. FOUND 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. 
- [SDR 20000425SH027](https://openairdocs.org/sdr/20000425SH027), Jan 14, 2000: STRINGER. CRACKED. FOUND DURING SCHEDULED B-SERVICE CHECK. CRACK AT END OF STR 15L, BS 720B FORWARD OF SCAN LIGHT. STRINGER CRACK POSSIBLY CAUSED BY CORROSION FOUND IN THIS AREA. 
- [SDR 20000425SH026](https://openairdocs.org/sdr/20000425SH026), Jan 14, 2000: FLOORBEAM. MISDRILLED. FOUND DURING SCHEDULED B-CHECK SERVICE CHECK AND ''G9'' BULKHEAD INSTALLATION, CABIN FLOORBEAM BS 344 UPER CAP HAS ELONGATED HOLES. SUBMITTER STATED HOLES MISDR
- [SDR 20000425SH025](https://openairdocs.org/sdr/20000425SH025), Jan 14, 2000: STRINGER. CRACKED. FOUND DURING SCHEUDLED B-SERVICE CHECK. STRINGER 15R CRACKED AT END BS 720C AFT AT SCAN LIGHT. STRINGER CRACK WAS CAUSED POSSIBLY BY CORROSION FOUND IN THIS ARE
- [SDR 20000425SH024](https://openairdocs.org/sdr/20000425SH024), Jan 14, 2000: SKIN. CORRODED. FOUND DURING SCHEDULED B-SERVICE CHECK AND ACCOMPLISHMENT OF AD 85-24-02, SB 727-51-17. APPROXIMATELY 1.50 INCH DIAMETER AREA OF EXFOLIATING CORROSION AT WING C
- [SDR 20000425SH023](https://openairdocs.org/sdr/20000425SH023), Jan 14, 2000: SKIN. CORRODED. FOUND DURING SCHEDULED B-MAINTENANCE CHECK, INNER SKIN HAS INTERGRANULAR CORROSION. BS 720B BL 12 INCHES, STR 15R BELOW SCAN LIGHT. CORROSION POSSIBLE CAUSED BY

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Mark Duffy HIGHLANDER aircraft: https://openairdocs.org/model/mark-duffy-highlander/aircraft.md
- The Rotax 914ULS engine: https://openairdocs.org/engine/rotax-914uls.md

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