# N247AC: Gteex Revolution R-40

- Status: N-number assigned, not yet registered
- Airframe: [Gteex Revolution R-40](https://openairdocs.org/model/gteex-revolution-r-40) (registry code 06102NL)
- Serial number: 1596A08321892D
- Type: Rotorcraft
- Engine type: Electric
- Mode S code: A24A03
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=247AC
- Page: https://openairdocs.org/aircraft/N247AC

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 (Gteex Revolution R-40)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N247AC.

## FAA accident and incident reports

None matched to N247AC.

## 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 N247AC not matched to an aircraft (5)

They name N247AC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR JYDR20181130332](https://openairdocs.org/sdr/JYDR20181130332), Nov 28, 2018: BLADES. BROKEN. THIS IS A PRELIMINARY REPORT TO MEET REPORTING REQUIREMENTS. THE ENGINE IS CURRENTLY BEING SHIPPED TO THIS REPAIR STATION FROM CANADA. MORE INFORMATION WILL BE 
- [SDR JYDR20161128318](https://openairdocs.org/sdr/JYDR20161128318), Nov 28, 2016: BLADE. UNBONDED. TAIL ROTOR BLADE CAUSED VIBRATION ON AIRCRAFT. UPON DISASSEMBLY AT REPAIR STATION, A LARGE AMOUNT OF WATER WAS FOUND IN THE FAIRING. THE WATER WAS ALLOWED ENTRY
- [SDR JYDR20150611153](https://openairdocs.org/sdr/JYDR20150611153), Jun 11, 2015: RING GEAR. LOOSE. MAIN GEAR BOX WAS RECEIVED FOR OVERHAUL. DURING DISASSEMBLY IT WAS FOUND THAT 1EA NUT, MS14182P06 HAD BACKED OFF OF 1EA BOLT MS14181-06010P THAT HOLDS THE SECON
- [SDR JYDR2014030600439](https://openairdocs.org/sdr/JYDR2014030600439), Mar 6, 2014: BEARING. SPALLED. MAIN GEAR BOX WAS REMOVED FROM ACFT, DUE TO MAKING METAL AFTER A CHIP LIGHT DURING FLIGHT. DISASSEMBLY OF MGB AT REPAIR STATION REVEALED THAT LT (NR 1) 2ND STAG
- [SDR 2006FA0001135](https://openairdocs.org/sdr/2006FA0001135), Oct 6, 2006: BEARING. CRACKED. (REF NR:MDR06-090) MAIN GEARBOX PN 6435-20400065, SN A6-011 WAS REMOVED DUE TO FINDINGS OF FERROUS METAL IN THE OIL SCREEN AND FILTER. UPON DISASSEMBLY AND TEAR

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Gteex Revolution R-40 aircraft: https://openairdocs.org/model/gteex-revolution-r-40/aircraft.md

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