- Registered owner
- Villarreal Roque
- Location
- College Station, TX
- Owner type
- Individual
- Serial number
- 5217
- Year built
- 2001
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- May 14, 2001
- Certificate issued
- July 13, 2015
- Expires
- July 31, 2028
- Mode S code
- A74C19
- Kit
- Stoddard Hamilton GLASTAR
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 N57AJMatched 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 Rekieta James GLASTAR 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 N57AJGeneral 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 Rekieta James GLASTAR aircraft
Reports on N57AJ not matched to an aircraft · 2
They name N57AJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 95ZZZX6192Joint · crackedINSPECTION REVEALED BLEED AIR JOINT WITH A CRACK APPROX 1 INCH BEYOND LIMITS. POSSIBLY CAUSED BY UNINTENTIONAL FORCE APPLIED TO AIR JOINT.SDR 95ZZZX3305Hinge · crackedWHILE CHECKING A DOOR SEAL PROBLEM, THE PAINT WAS FOUND CRACKED ON THE LOWER CABIN DOOR HINGE LEG. IT WAS FOUND TO BE A CRACK THAT EXTENDS APPROXIMATELY 65 PERCENT IN LENGTH OF LOWER PART LEG. REMOVED AND INSTALLED NEW HINGE ASSEMBLY. THE LOWER LEG RECEIVED
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.