- Registered owner
- Schwartz Bernard M
- Location
- Las Vegas, NV
- Owner type
- Individual
- Serial number
- 2311
- Year built
- 2010
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- June 10, 2010
- Certificate issued
- August 26, 2022
- Expires
- August 31, 2029
- Mode S code
- A97B39
- Kit
- Glasair Aviation LLC SUPER II-RG
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 N71RPMatched 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 Pinkston Randy T SUPER IIS RG 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.
Reports on N71RP not matched to an aircraft · 1
They name N71RP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports
No reports matched to N71RPGeneral 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 Pinkston Randy T SUPER IIS RG aircraft
Reports on N71RP not matched to an aircraft · 2
They name N71RP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2000ZZZX410Clamp · crackedAEROQUIP VEE BAND CLAMP CRACKED STRAP BENEATH 'TEE' BOLT. CLAMP SECURED 12TH STAGE DUCT BLANKING PLATE. CRACK ALLOWED CLAMP TO FLEX THEN FAIL. CLAMP AND PLATE EXITED EXHAUST THROUGH BYPASS SECTION. DAMAGE TO BYPASS CASE OUTBOARD OF 12TH STAGE.SDR 2000ZZZX416Ffr · failedIN-FLIGHT, ENGINE ACCELERATION/DECELERATION FL 45,000. RIGHT ENGINE COMPRESSOR STALLED AND FLAMED OUT DURING ACCELERATION. REMOVED AND REPLACED FFR PER GULFSTREAM CMP 732032.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.