- Registered owner
- Flywerx LLC
- Location
- Anchor Point, AK
- Owner type
- LLC
- Serial number
- 0001
- Year built
- 2010
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- March 12, 2010
- Certificate issued
- February 23, 2023
- Expires
- February 28, 2030
- Mode S code
- A4B1B2
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 N401PWMatched 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 Underwood Reo L GUARDIAN RAVEN aircraft
FAA incident reports
No FAA accident or incident reports matched to N401PWMatched 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 Underwood Reo L GUARDIAN RAVEN aircraft
Service difficulty reports
No reports matched to N401PWGeneral 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 Underwood Reo L GUARDIAN RAVEN aircraft
Reports on N401PW not matched to an aircraft · 4
They name N401PW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR MHJ2002F00002Cylinder · separatedNR 4 CYLINDER FOUND SEPERATED FROM CRANKCASE, CAUSE UNKNOWN. ENGINE REMOVED FROM AIRCRAFT AND SENT TO OVERHAUL FACILITY.SDR 20010122CW001Torque Tube · crackedCABLE ATTACH ARM FAILED AT WELD. MOST LIKELY CRACKED DURING TOWING OPERATION DUE TO OVERSTEERING TURN LIMITS.SDR 20010221AP001Arm · failedPILOT REPORTED LOSS OF RIGHT RUDDER CONTROL ON FINAL APPROACH AT DAL. RT RUDDER CABLE ARM ON TORQUE TUBE FAILED AT THE WELD. BELIEVE DAMAGE WAS CAUSED BY OVER TURNING NOSE GEAR BY GROUND PERSONNEL.INSTALLED SERVICEABLE TORQUE TUBE,AND RIGGED PER MANUAL.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.