This N-number isn't registered right now. Below is its last known registration, canceled Jul 13, 2018.
Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Oct 2015)7 ADs may apply
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 in-flight fuel management due to distraction and self-induced pressure, which resulted in fuel starvation and a total loss of engine power. Contributing to the accident was the pilot’s failure to conduct the descent checklist, which included a task to manage fuel.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR16LA008)
THE PILOT'S FAILURE TO PROPERLY MANAGE THE FUEL SYSTEM TO AVOID RUNNING A TANK DRY AT A LOW ALTITUDE. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA95LA174)
DURING THE LANDING ROLL, THE PILOT HEARD A LOUD BANG ON THE RIGHT SIDE OF THE AIRPLANE. WHEN THE PILOT APPLIED BRAKES AND THE SPEED DISSIPATED, DIRECTIONAL CONTROL WAS LOST. THE AIRPLANE VEERED OF THE RUNWAY AND COLLIDED WITH A RUNWAY LIGHT. DURING AN INSPECTION, IT WAS FOUND THAT THE RIGHT MAIN LANDING GEAR TIRE HAD A WORN SPOT AND WAS FLAT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX88LA291)
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 |
|---|---|---|---|
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (GTSIO-520-C) |
| 2020-16-11 | Reciprocating Cylinder Section | Sep 21, 2020 | Engine (GTSIO-520-C)Only with: Engines originally manufactured, rebuilt, or modified with a cross-flow cylinder assembly replacement on or after November 1, 2014, with cross-flow cylinder assembly P/N 658538, 658540, 658542, 658591, 658595, 658613, 658624, 658539, 658541, 658590, 658594, 658603, 658623, or 658630 installed. |
| 2020-03-16 | Fuselage Main, Structure | Mar 9, 2020 | Airframe (T210K) |
| 2012-10-04 | Wings | Jun 5, 2012 | Airframe (T210K)Certain serial numbers: 210G 21058819–21058936; T210G T210-0198–T210-0307; 210H 21058937–21059061; T210H T210-0308–T210-0392; 210J 21059062–21059199; T210J 21058140; … |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (T210K) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (T210K)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
| 2007-05-15 | Teledyne Continental Motors GTSIO-520 Series Reciprocating Engines | Apr 16, 2007 | Engine (GTSIO-520-C) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.