# N424RA: 2022 Cirrus Design SF50

- Status: Valid registration
- Airframe: [Cirrus Design SF50](https://openairdocs.org/model/cirrus-design-sf50) (registry code 2130010, 7 seats)
- Engine: [Williams FJ33-5A](https://openairdocs.org/engine/williams-fj33-5a) (registry code 66015)
- Data sheets: [TCDS A00018CH](https://openairdocs.org/tcds/A00018CH) (Cirrus Design Corporation), [TCDS E3GL](https://openairdocs.org/tcds/E3GL) (Williams International Company L.L.C.) (OpenAirDocs)
- Serial number: 0376
- Year built: 2022
- Type: Fixed wing single engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: August 12, 2022
- Certificate issued: January 29, 2023
- Expires: January 31, 2030
- Mode S code: A50BF3
- Registered owner: [Dabble Aviation LLC](https://openairdocs.org/faa-owner/DABBLE%20AVIATION%20LLC)
- Location: [Indn Hbr Bch, FL](https://openairdocs.org/faa-place/FL/Indn%20Hbr%20Bch)
- Owner type: LLC
- Owner's area on the map: 28.1760° N, 80.6053° W: Placed by OpenAirDocs at the center of ZIP code 32937, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=424RA
- Page: https://openairdocs.org/aircraft/N424RA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 3 in force

### Matched by airframe (Cirrus Design SF50)

- [AD 2023-04-20](https://openairdocs.org/ad/2023-04-20): Auto Flight System · Cirrus Design SF50. Effective Mar 21, 2023
- [AD 2020-03-50](https://openairdocs.org/ad/2020-03-50): Communications · Cirrus Design SF50. Effective Jun 11, 2020
- [AD 2019-08-51](https://openairdocs.org/ad/2019-08-51): Flight Controls · Cirrus Design SF50. Effective Jun 17, 2019

### Matched by engine (Williams FJ33-5A)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N424RA.

## FAA accident and incident reports

None matched to N424RA.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty 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 UATA2021111142415](https://openairdocs.org/sdr/UATA2021111142415), Nov 11, 2021: SPAR CAP. CRACKED. CRACK FOUND WHILE PERFORMING SID INSPECTIONS VIA X-RAY ON R/H WING BOTTOM FWD WING SPAR STRUCTURE CLOSE TO THE WING ROOT.
- [SDR UATA2021092342412](https://openairdocs.org/sdr/UATA2021092342412), Sep 21, 2021: SKIN. DENTED. DENT 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 
- [SDR UATA2021092342411](https://openairdocs.org/sdr/UATA2021092342411), Sep 21, 2021: SKIN. CRACKED. THE 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.
- [SDR UATA2021092342410](https://openairdocs.org/sdr/UATA2021092342410), Sep 13, 2021: FRAME SPLICE. CHAFED. AIRCRAFT WAS FOUND TO HAVE CHAFE DAMAGE TO THE R/H CARGO DOOR FRAME BEAM NEAR LOWER SPLICE OF CENTER BEAM SEGMENT. BLENDED CHAFED AREAS, REMOVED FACTORY SPLICE 
- [SDR 2010FA0001041](https://openairdocs.org/sdr/2010FA0001041), Sep 13, 2010: TRANSMITTER. INOPERATIVE. TROUBLESHOT INOPERATIVE LT ENGINE FUEL FLOW INDICATION. FOUND ROTATING ELEMENT OF INLINE FUEL FLOW TRANSMITTER LOOSE AND SHIFTED FWD. REMOVED FUEL LINE FROM TRA
- [SDR 2001FA0000329](https://openairdocs.org/sdr/2001FA0000329), Aug 1, 2001: BOLT. BACKED OUT. AN5-4A BOLT IN BOTTOM PIVOT POINT ROD ATTACHMENT BACKED OUT CAUSING LOSS OF ENGINE CONTROL. AN936B516 LOCK WASHER WAS PRESENT.

## STCs that may be installed (OpenAirDocs) (3)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Cirrus Design SF50)

- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA04615CH](https://openairdocs.org/stc/SA04615CH): BasicMed 6-place occupancy restriction. CIRRUS DESIGN CORPORATON
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation

## Related

- Other Cirrus Design SF50 aircraft: https://openairdocs.org/model/cirrus-design-sf50/aircraft.md
- The Williams FJ33-5A engine: https://openairdocs.org/engine/williams-fj33-5a.md

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