# N127MC: Hood Tech Corp Mechanical HTMC-40-PLUS

- Status: Valid registration
- Airframe: [Hood Tech Corp Mechanical HTMC-40-PLUS](https://openairdocs.org/model/hood-tech-corp-mechanical-htmc-40-plus) (registry code 061013S)
- Serial number: HTMC-0021
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: August 31, 2021
- Expires: August 31, 2028
- Mode S code: A06EC9
- Registered owner: [Hood Tech Corp Mechanical Inc](https://openairdocs.org/faa-owner/HOOD%20TECH%20CORP%20MECHANICAL%20INC)
- Location: [Hood River, OR](https://openairdocs.org/faa-place/OR/Hood%20River)
- Owner type: Corporation
- Owner's area on the map: 45.6068° N, 121.6023° W: Placed by OpenAirDocs at the center of ZIP code 97031, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=127MC
- Page: https://openairdocs.org/aircraft/N127MC

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 (Hood Tech Corp Mechanical HTMC-40-PLUS)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N127MC.

## FAA accident and incident reports

None matched to N127MC.

## 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 N127MC not matched to an aircraft (3)

They name N127MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2009FA0000161](https://openairdocs.org/sdr/2009FA0000161), Dec 17, 2008: HINGE. CORRODED. PREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION
- [SDR 2009FA0000134](https://openairdocs.org/sdr/2009FA0000134), Dec 17, 2008: FORK. CRACKED. PREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED N
- [SDR 2009FA0000123](https://openairdocs.org/sdr/2009FA0000123), Dec 17, 2008: TORQUE TUBE. CORRODED. PREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSP DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE 

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Hood Tech Corp Mechanical HTMC-40-PLUS aircraft: https://openairdocs.org/model/hood-tech-corp-mechanical-htmc-40-plus/aircraft.md

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