Safety record in brief:1 NTSB incident (Sep 2024)6 ADs may apply1 service difficulty report
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Individual owners are shown by city and state only.
The flight crew’s failure to properly identify the airport and runway of intended landing, and the lack of verification of their airplane’s position using all available navigation information.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for OPS24LA045)
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 |
|---|---|---|---|
| 2026-03-06 | Vertical Stabilizer Structure; 5415, Nacelle/Pylon, Attach Fittings | Mar 13, 2026 | Airframe (525B) |
| 2024-15-09 | Gust Lock/ Damper System | Oct 22, 2024 | Airframe (525B)Only with: Tamarack ATLAS winglets installed in accordance with STC No. SA03842NY. |
| 2020-24-06 | Flight Controls | Dec 28, 2020 | Airframe (525B)Only with: With Tamarack active load alleviation system (ATLAS) winglets installed in accordance with STC SA03842NY. |
| 2008-03-10 | Cessna Aircraft Company Models 525, 525A, and 525B Airplanes | Mar 11, 2008 | Airframe (525B)Certain serial numbers: 525 0001–0637; 525A 0001–0347; 525B 0001–0152. Only with: Cockpit mounted pilot relief tube installed. |
| 2007-23-16 | Cessna Aircraft Company, Model 525B Airplanes | Dec 19, 2007 | Airframe (525B)Certain serial numbers: 525B 0001–0013 |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-17-11 | The Cessna Aircraft Company Models 525, 525A, and 525B Airplanes | Oct 7, 2005 | Airframe (525B)Certain serial numbers: 525 525-0001–525-0600; 525A 525A-0001–525A-0234; 525B 525B-0001–525B-0035 |
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.
UPON INITIAL DESCENT, FROM A CRUISING ALTITUDE OF 45,000 FT, THE PILOT BEGAN REDUCING ENGINE POWER. THE NR 2 ENGINE ROLLED BACK TO IDLE, THEN SHUTDOWN UNCOMMANDED. THE PILOT ATTEMPTED TO RESTART THE NR 2 ENGINE, BUT WAS UNSUCCESSFUL. THE LANDING WAS UNEVENTFUL. UPON INVESTIGATION OF THE INCIDENT…
From FAA Service Difficulty Reports; matched by N-number and serial number.