# N425CT: Anduril Industries CP200

- Status: Valid registration
- Airframe: [Anduril Industries CP200](https://openairdocs.org/model/anduril-industries-cp200) (registry code 06102I6)
- Serial number: 289
- Type: Fixed wing single engine
- Engine type: 2 cycle
- Certificate issued: November 21, 2024
- Expires: November 30, 2031
- Mode S code: A50E76
- Registered owner: [Anduril Industries Inc](https://openairdocs.org/faa-owner/ANDURIL%20INDUSTRIES%20INC)
- Location: [Costa Mesa, CA](https://openairdocs.org/faa-place/CA/Costa%20Mesa)
- Owner type: Corporation
- Owner's area on the map: 33.6796° N, 117.9085° W: Placed by OpenAirDocs at the center of ZIP code 92626, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=425CT
- Page: https://openairdocs.org/aircraft/N425CT

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 (Anduril Industries CP200)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N425CT.

## FAA accident and incident reports

None matched to N425CT.

## 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 N425CT not matched to an aircraft (3)

They name N425CT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR T17A201311074002](https://openairdocs.org/sdr/T17A201311074002), Nov 4, 2013: ACTUATOR. STUCK. RIGHT ROLL TRIM TAB STUCK IN WING UP POSITION. REPLACED TAB ACTUATOR. FUNCTION TEST NORMAL.
- [SDR 2009F00030](https://openairdocs.org/sdr/2009F00030), Apr 22, 2009: INLET. DAMAGED. DURING SCHEDULED INSP, IT WAS DISCOVERED THAT 1 INLET RIVET HEAD WAS MISSING FROM THE NR 2 ENGINE INLET INNER SKIN (BARREL). THE INLET WAS INSTALLED 288.1 HOURS
- [SDR N425CT0003](https://openairdocs.org/sdr/N425CT0003), Oct 31, 2007: HYDROMECH UNIT. RESTRICTED. PARTIAL POWER LOSS FROM RT ENGINE AT FL 390 POWER SURGED DURING APPROACH AND LANDING.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Anduril Industries CP200 aircraft: https://openairdocs.org/model/anduril-industries-cp200/aircraft.md

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