- Registered owner
- Anduril Industries Inc
- Location
- Costa Mesa, CA
- Owner type
- Corporation
- Serial number
- 214
- Type
- Fixed wing single engine
- Engine
- 2 cycle
- Certificate issued
- November 21, 2024
- Expires
- November 30, 2031
- Mode S code
- A535F5
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 N435CTMatched 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 N435CTMatched 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 N435CTGeneral 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 N435CT not matched to an aircraft · 4
They name N435CT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR T17A201603224011Fastener · shearedA LOCK FASTENER WAS NOTED MISSING FROM THE RT ENG INLET. UPON FURTHER INSPECTION, ENG FAN BLADE DAMAGED & COMPRESSOR VANE DAMAGE WAS FOUND. ENG IS BEING REMOVED FOR REPAIR.SDR E81R2012091600001Harness · mismanufacturedCOPILOT NOTED QUICK-DONNING CREW MASK HEAD HARNESS ORIENTED UPSIDE DOWN COMPARED TO PILOT'S O2 MASK WHEN TEST FITTED. MASK FUNCTIONS OK, AND HEAD HARNESS COULD BE RE-ORIENTED TO FIT, BUT CONNECTIONS WOULD FACE AWAY FROM MASK BODY INSTEAD OF TOWARDS MASK BODY.SDR T17A2012020800001Electrical Sys · failedON CLIMB OUT, LOST ALL AIRCRAFT "NORMAL" ELECTRICAL POWER. ALL AVIONICS SCREENS, FMS, AND ANNUNCIATOR DISPLAYS WENT BLACK.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.