Safety record in brief:1 NTSB accident (substantial damage, Aug 2004)3 ADs may apply1 service difficulty report
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 failure to maintain clearance from an object (pole) during an aborted landing. The pilot's delayed decision to abort the landing and a pole were factors.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA04CA170)
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 |
|---|---|---|---|
| 2020-21-22 | Fuselage; 55, Stabilizers | Dec 7, 2020 | Airframe (180J) |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (180J) |
| 98-23-02 | Cessna Aircraft Company 180 and 185 Series Airplanes | Dec 22, 1998 | Airframe (180J)Only with: Airglas Engineering Company (AECI) Model LW3600-180 or LW3600-180A fixed penetration wheel skis installed per STC SA213AL. |
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.
ENGINE WAS AT CRUISE POWER. LOUD BANG. SMALLER BANGS. ENGINE RAN, BUT DID NOT PRODUCE APPRECIABLE POWER. FORCED LANDING IN TUNDRA NEAR NOATAK, ALASKA FOLLOWED. NO DAMAGE. FOUND SUPPORT LUGS FOR EXHAUST VALVE ROCKER ARM FAILED ON NR 6 CYLINDER. INTAKE MANIFOLD WAS SEPARATED AT RUBBER COUPLING ON RT…
From FAA Service Difficulty Reports; matched by N-number and serial number.