- Registered owner
- Anduril Industries Inc
- Location
- Costa Mesa, CA
- Owner type
- Corporation
- Serial number
- 4046
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Mode S code
- A4C011
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 N405JWMatched 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 ROADRUNNER aircraft
FAA incident reports
No FAA accident or incident reports matched to N405JWMatched 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 ROADRUNNER aircraft
Service difficulty reports
No reports matched to N405JWGeneral 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 ROADRUNNER aircraft
Reports on N405JW not matched to an aircraft · 3
They name N405JW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR UVVR200200002Rib · corrodedRIB HAS CRACK RADIATING THROUGH FASTENERS ATTACHING RIB TO SPAR AND A PIECE IS MISSING APPROX 6 INCHES LONG AND 1/4 INCH WIDE. CORROSION EVIDENT, POSSIBLY DUE TO INSULATION BEING WET. THIS DEFECT CAN ONLY BE SEEN IF LEADING EDGE IS DISASSEMBLED.SDR UVV2002F00001Rib · crackedRIB HAS CRACK RADIATING THROUGH FASTENERS ATTACHING RIB TO SPAR AND A PIECE IS MISSING APPROX 6 INCHES LONG AND .2500 INCHES WIDE, CORROSION EVIDENT, POSSIBLY DUE TO INSULATION BEING WET. THIS DEFECT CAN ONLY BE SEEN IF LEADING EDGE IS DISASSEMBLED.SDR 20000828SH035Hinge · crackedFOUND CRACK IN LOWER THRUST REVERSER OUTBOARD BRACKET AT 1,200-HOUR INSPECTION. INSPECTION REQUIRED DYE PENETRANT INSPECTION. HINGE BRACKET ORIGNAL. (X)
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.