This N-number isn't registered right now. Below is its last known registration, canceled Jan 20, 2026.
Safety record in brief:1 NTSB accident (substantial damage, Jul 2025)3 ADs may apply2 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 inadequate preflight fuel planning, which resulted in fuel exhaustion and a subsequent total loss of engine power to one of the airplane’s two engines. Contributing to the outcome was the pilot’s loading of the airplane beyond its maximum gross weight.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA25LA266)
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 |
|---|---|---|---|
| 2011-15-11 | Cessna Aircraft Company (Cessna) Models 337, 337A (USAF 02B), 337B, 337C, 337D, 337E… | Sep 6, 2011 | Airframe (T337G)Only with: Airplanes that are or have ever been modified by Flint Aero, Inc. STC SA5090NM. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (T337G) |
| 2010-21-18 | Cessna Aircraft Company (Cessna) Models 336, 337, 337A (USAF 02B), 337B, M337B (USAF… | Nov 3, 2010 | Airframe (T337G)Only with: Airplanes that are or have ever been modified by Aviation Enterprises STC SA02055AT, SA02056AT, SA02307AT, or SA02308AT. |
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.
EXHAUST PIPE TO TURBOCHARGER CLAMP FOR FRONT ENGINE CRACKED AT SPOT-WELD AND SEPARATED ON TAKEOFF. WHEN THIS HAPPENED, THE EXHAUST PIPE DEPARTED THE AIRCRAFT AND THE EXHAUST SCORCHED THE ENGINE COWLING AND FIREWALL. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.LAV SMOKE WARNING.
From FAA Service Difficulty Reports; matched by N-number and serial number.