- Registered owner
- Anduril Industries Inc
- Location
- Costa Mesa, CA
- Owner type
- Corporation
- Serial number
- 289
- Type
- Fixed wing single engine
- Engine
- 2 cycle
- Certificate issued
- November 21, 2024
- Expires
- November 30, 2031
- Mode S code
- A50E76
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 N425CTMatched 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 Anduril Industries CP200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N425CTMatched 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 Anduril Industries CP200 aircraft
Service difficulty reports
No reports matched to N425CTGeneral 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 Anduril Industries CP200 aircraft
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 T17A201311074002Actuator · stuckRIGHT ROLL TRIM TAB STUCK IN WING UP POSITION. REPLACED TAB ACTUATOR. FUNCTION TEST NORMAL.SDR 2009F00030Inlet · damagedDURING 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 206 CYCLES AFTER REPAIR DUE TO SAME CONDITION OF SEVERAL MISSING AND CRACKED RIVETS ON THE INNER SKSDR N425CT0003Hydromech Unit · restrictedPARTIAL POWER LOSS FROM RT ENGINE AT FL 390 POWER SURGED DURING APPROACH AND LANDING.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.