- Registered owner
- Francis Wayne Ltd
- Location
- Springfield, OH
- Owner type
- Corporation
- Serial number
- 2594
- Year built
- 2007
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 11, 2007
- Certificate issued
- April 9, 2014
- Expires
- April 30, 2030
- Mode S code
- A81A86
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1991 | 1 |
| 1993 | 2 |
| 1996 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 3 |
| 2008 | 4 |
| 2009 | 3 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 2 |
| 2014 | 1 |
| 2016 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 5 |
| 2024 | 1 |
Airframe · Cirrus Design SR22
AD 2024-24-11Power LeverAD 2023-09-09Exhaust Turbine System (Recip)AD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 28
Advisory, not mandatory.
See all 31 bulletins
NTSB investigations
No NTSB investigations matched to N621FWMatched 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 SR22 aircraft
FAA incident reports
No FAA accident or incident reports matched to N621FWMatched 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 SR22 aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2026FA0000283Brake Disc · crackedCRACKED - DURING ANNUAL INSPECTION, THE OPPOSITE BRAKE DISC WAS FOUND BADLY CRACKED, SEE SDR 2026FA000282. ADDITIONAL INSPECTION PERFORMED ON LH BRAKE DISC WITH 10X MAGNIFYING GLASS ON INSIDE 90 DEGREE BEND RADIUS WHERE THE BODY MEETS THE FLANGE. POSSIBLE CRACSDR 2026FA0000282Brake Disc · crackedATTACHMENT FLANGE CRACKED THROUGH 270+ DEGREES OF CIRCUMFERENCE - DURING ANNUAL INSPECTION, RT BRAKE DISC/ROTOR DISCOVERED TO HAVE 5 SIZEABLE HOLES AT 90 BEND FROM BODY TO ATTACHMENT FLANGE. SIGNS OF HEAVY CORROSION IN BEND ALSO PRESENT. CRACKS RUNNING BETWEEN
STCs that may be installed · 147
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cirrus Design SR22
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