This N-number isn't registered right now. Below is its last known registration, canceled Jan 10, 2018.
Safety record in brief:1 NTSB accident (substantial damage, Jul 2011)2 ADs may apply5 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The pilot’s improper fuel management, which resulted in a total loss of engine power due to fuel starvation.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA11LA405)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (U206G) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
DURING A 100HR INSPECTION, DISCOVERED BLOWBY BETWEEN FINS ON THE INTAKE SIDE OF THE CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO BE CRACKED BETWEEN THE INTAKE VALVE SEAT AND THE SPARK PLUG HOLE. THIS IS THE 6TH CYLINDER THIS YEAR WITH ALMOST IDENTICAL CRACKS.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A 100 HR INSP, DISCOVERED BLOWBY BETWEEN FINS ON THE INTAKE SIDE OF THE CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO BE CRACKED BETWEEN THE INTAKE VALVE SEAT AND THE SPARK PLUG HOLE. THIS IS THE 5TH CYLINDER THIS YEAR WITH ALMOST IDENTICAL CRACKS.
From FAA Service Difficulty Reports; matched by N-number and serial number.LOW COMPRESSION NR2 CYLINDER ON 100 HR INSPECTION. FOUND BLOW-BY COMING AROUND FINS IN THE HEAD. CYLINDER WAS CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. ALL PREVIOUS COMPRESSION CHECKS WERE IN THE 70/60 RANGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.LOW COMPRESSION NR2 CYLINDER ON 100HR INSPECTION. FOUND BLOWBY COMING AROUND FINS IN THE HEAD. CYLINDER WAS CRACKED BETWEEN SPARK PLUG HOLE AND INTAKE VALVE. ALL PREVIOUS COMPRESSION CHECKS WERE IN THE 70/60 RANGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A 100 HR INSP, FOUND NOSE GEAR HAD FORE AND AFT MOVEMENT WHERE THERE SHOULD BE NONE. REMOVED AFT DRAG LINK BOLT TO INVESTIGATE AND FOUND IT TO BE WORN AND DEFORMED AS IF GETTING READY TO SHEAR. THIS IS THE THIRD OR FOURTH FOUND. THE OTHER ACFT THAT WERE FOUND HAD SHEARED THE BOLT AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.