- Registered owner
- Winged Vision Inc
- Location
- Gaithersburg, MD
- Owner type
- Corporation
- Serial number
- 1257
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 21, 1979
- Certificate issued
- November 29, 2000
- Expires
- November 30, 2028
- Mode S code
- A6D179
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 4
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1979 | 1 |
|---|---|
| 1982 | 1 |
| 2005 | 1 |
| 2022 | 1 |
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Helio HT-295
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemNTSB investigations
No NTSB investigations matched to N5387GMatched 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 Helio HT-295 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVGR2018060500044Cylinder · wornDURING A ROUTINE OIL AND FILTER CHANGE. NOTHING ABNORMAL WAS NOTED DURING THE ENGINE RUN UP, NOR WAS THE ANY ABNORMALITY REPORTED FROM THE PILOT. WHEN THE EXTERNAL REMOTE MOUNTED OIL FILTER WAS CUT OPEN, A LOT OF METAL WAS DISCOVERED IN THE PAPER PLEATS. ITSDR EVGR201304120001Plug · wornOIL ANALYSIS CAME BACK WITH VERY HIGH ALUMINUM METAL CONTENT IN THE OIL. METAL WAS ALSO VISIBLE IN THE DRAINED OIL WITH AN APPEARANCE LIKE METAL-FLAKE PAINT. THE FLAKES WERE SMALL ENOUGH THAT SOME WERE NOT BEING TRAPPED IN THE OIL FILTER EXCEPT SOME AS SLUDGSDR 20050505Tube · crackedWHILE PERFORMING THE 1500 HOUR INSPECTION REQUIRED BY AD 82-16-08, A CRACK WAS FOUND ON THE RT VERTICAL TUBE OF THE CARRY THRU. THE CRACK WAS LOCATED AT THE TOP WELD OF THE TUBE. THE LENGTH OF THE CRACK IS ROUGHLY HALF THE CIRCUMFERENCE OF THE TUBE ON THE FR
STCs that may be installed · 105
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Helio HT-295
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller