- Registered owner
- Dabble Aviation LLC
- Location
- Indn Hbr Bch, FL
- Owner type
- LLC
- Serial number
- 0376
- Year built
- 2022
- Type
- Fixed wing single engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- August 12, 2022
- Certificate issued
- January 29, 2023
- Expires
- January 31, 2030
- Mode S code
- A50BF3
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2019 | 1 |
|---|---|
| 2020 | 1 |
| 2023 | 1 |
Airframe · Cirrus Design SF50
AD 2023-04-20Auto Flight SystemAD 2020-03-50CommunicationsEmergency ADAD 2019-08-51Flight ControlsEmergency ADInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N424RAMatched 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 Cirrus Design SF50 aircraft
FAA incident reports
No FAA accident or incident reports matched to N424RAMatched 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 Cirrus Design SF50 aircraft
Service difficulty reports
No reports matched to N424RAGeneral 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 Cirrus Design SF50 aircraft
Reports on N424RA not matched to an aircraft · 6
They name N424RA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR UATA2021111142415Spar Cap · crackedCRACK FOUND WHILE PERFORMING SID INSPECTIONS VIA X-RAY ON R/H WING BOTTOM FWD WING SPAR STRUCTURE CLOSE TO THE WING ROOT.SDR UATA2021092342412Skin · dentedDENT FOUND IN THE LOWER SKIN OF THE R/H HORIZONTAL STABILIZER. UPON REMOVAL OF ALL THE DAMAGED MATERIAL, THE HOLE WAS 0.65" IN DIAMETER. REPAIRED BY APPLYING A FLUSH PATCH PER CASA 212 SRM.SDR UATA2021092342411Skin · crackedTHE TRAILING EDGE OF THE L/H INBOARD FLAP COVE SKIN WAS FOUND TO BE CRACKED ALONG THE RIVET LINE. AFTER DAMAGED MATERIAL WAS REMOVED, THE HOLE WAS ABOUT 8.5"X2.5" THIS AREA WAS FLUSH PATCHED PER CASA 212 SRM.
STCs that may be installed · 3
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.