- Registered owner
- Traynor John Patrick
- Location
- Hayward, CA
- Owner type
- Individual
- Serial number
- 289
- Type
- Fixed wing single engine
- Engine
- 4 cycle
- Airworthiness
- Experimental, operating light-sport, previously under 21.190
- Airworthiness date
- May 16, 2018
- Certificate issued
- November 7, 2024
- Expires
- November 30, 2031
- Mode S code
- A017F3
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included below.
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 N105GXMatched 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 Remos Acft Gmbh Flugzeugbau REMOS GX aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports
No reports matched to N105GXGeneral 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 Remos Acft Gmbh Flugzeugbau REMOS GX aircraft
Reports on N105GX not matched to an aircraft · 2
They name N105GX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR G1X2002F00001Bracket · bentFDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SHIELD SHOULD ALSO BE SDR G1X2002F00000Bracket · bentFDR POTENTIOMETER BRACKET INTERFERING WITH AILERON ACTUATOR AT FULL TRAVEL, BRACKET IS MOUNTED TOO FAR FORWARD DUE TO .1250 SHIM USED BETWEEN AFT SPAR AND THE BRACKET. SHIM SHOULD BE REMOVED AND POTENTIOMETER ADJUSTED FOR NEW POSITION. SHIELD SHOULD ALSO BE
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.