- Registered owner
- Cirrus Associates LLC
- Location
- Colorado Springs, CO
- Owner type
- LLC
- Serial number
- 0053
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 29, 2009
- Certificate issued
- November 10, 2015
- Expires
- November 30, 2028
- Mode S code
- A9CB41
From the FAA registry file of October 22, 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 N730CDMatched 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 N730CDMatched 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 · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MNG2002F00001Rivet · failedRIVETS HOLDING THE ATTACH BRACKET TO THE INTAKE ASSEMBLY, FAILED AND CAME OUT. THE RIVETS HAD NO WHERE TO GO BUT THROUGH THE INTAKE AND THROUGH THE ENGINE. THE MANUFACTURER IS AWARE OF PROBLEM, BUT HAS NOT YET CORRECTED.SDR MNG2002F00000Isolator · failedDURING TROUBLESHOOTING FOR ENGINE VIBRATION IT WAS NOTED THAT THE FRONT ENGINE MOUNTS WERE SAGGING TO THE POINT THAT THE ISOLATOR WAS TOUCHING THE ENGINE MOUNT STRUCTURE. REPLACEMENT OF THE ISOLATORS WAS NEEDED.SDR 2002FA0000524Mount · chafedDURING THE 100 HOUR INSPECTION, A FUEL LINE CLAMP WAS FOUND CHAFING ON THE ENGINE MOUNT. THE CLAMP HAD CHAFED APPROXIMATELY .006 INTO ONE OF THE ENGINE MOUNT TUBES. THE CLAMP FOR THIS LINE APPEARS TO BE TOO LONG, ALLOWING IT TO CONTACT THE MOUNT TUBE. THE E
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.
See all 147 STCs