- Registered owner
- Aerosim Academy Inc
- Location
- Sanford, FL
- Owner type
- Corporation
- Serial number
- 1818
- Year built
- 2007
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 18, 2007
- Certificate issued
- December 21, 2016
- Expires
- December 31, 2029
- Mode S code
- A5D7B0
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 26
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1988 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1998 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 1 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 5 |
| 2009 | 1 |
| 2010 | 1 |
| 2012 | 2 |
| 2022 | 1 |
| 2023 | 3 |
| 2024 | 1 |
Airframe · Cirrus Design SR20
AD 2024-24-11Power LeverAD 2022-03-15Fuel Quantity IndicatorAD 2009-05-05Primary Flight DisplaysInformation bulletins that may apply · 19
Advisory, not mandatory.
See all 20 bulletins
NTSB investigations
No NTSB investigations matched to N476DAMatched 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 SR20 aircraft
FAA incident reports
No FAA accident or incident reports matched to N476DAMatched 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 SR20 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2012FA0000720Magneto · malfunctionedMAGNETO MISFIRES DURING MAGNETO CHECK.SDR 2012FA0000721Magneto · malfunctionedRIGHT MAGNETO WOULD NOT FIRE DURING MAGNETO CHECK. ENGINE QUIT RUNNING WHEN RIGHT MAGNETO SELECTED.SDR 2012FA0000706Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL NOT OUTPUT HIGHER THAN 14.3 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. SHOULD BE IN THE 17 - 18 GPH RANGE.SDR 2008FA0000307Oil Cooler · wornTHE OIL COOLER SUPPORT SHOE RUBBER COATING IS FAILING AND EATING INTO THE OIL COOLER .020 TO .040 OF AN INCH. IAW MM IT IS INSTALLED AT ENGINE ASSY AND ADJUSTED AFTER INITIAL TEST RUN. THERE IS NO PUBLISHED IN SERVICE INSTRUCTION FOR IT. IF THIS CONDITION IS
STCs that may be installed · 138
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 SR20
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
Earlier aircraft with this N-number · 1
This aircraft carried N476DA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.