- Registered owner
- Hochstedler Wilford L
- Location
- Parsons, KS
- Owner type
- Individual
- Serial number
- 086
- Year built
- 2019
- Type
- Fixed wing single engine
- Engine
- 4 cycle
- Airworthiness
- Light sport, airplane
- Airworthiness date
- August 11, 2019
- Certificate issued
- September 18, 2024
- Expires
- September 30, 2031
- Mode S code
- A38954
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 N327LJMatched 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 Aeroprakt Mfg SP Z O O A32 aircraft
FAA incident reports
No FAA accident or incident reports matched to N327LJMatched 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 Aeroprakt Mfg SP Z O O A32 aircraft
Service difficulty reports
No reports matched to N327LJGeneral 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 Aeroprakt Mfg SP Z O O A32 aircraft
Reports on N327LJ not matched to an aircraft · 2
They name N327LJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2003FA0000527Elt · inoperativeELT (PN 02195 MODEL 110-406) IS TRIGGERED ON WHENEVER AIRCRAFT IS WASHED, DEICED OR IN HEAVY STANDING RAIN, ELT IS MOUNTED AT FRAME 25, INSIDE THE TAIL CONE FAIRING ABOVE THE DATUM LINE. POSSIBLE WATER ENTRY AREA IS THROUGH THE RUDDER SHAFT AS IT PASSES THROUSDR WUX2002F00000Bracket · mislocatedLEFT THRUST REVERSER STOW HOSE PULLED OUT OF SWAGGED FITTING AT PYLON ATTACH POINT, CAUSING IT TO LEAK. DETERMINED THAT LOWER SUPPORT BRACKET ATTACHED AT THE LOWER 5:30 CLOCK POSITION ON THE T/R IS RIVETED .250 CLOSER TO LIGHTING HOLE (WHERE HOSE PASSES THROU
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.