Safety record in brief:1 NTSB accident (substantial damage, Dec 2019)5 ADs may apply3 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 installation of incorrect mounting hardware to secure the right engine cowl, which resulted in an in-flight separation and impact with the horizontal stabilizer and elevator.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN20LA041)
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 |
|---|---|---|---|
| 2024-15-09 | Gust Lock/ Damper System | Oct 22, 2024 | Airframe (525A)Only with: Tamarack ATLAS winglets installed in accordance with STC No. SA03842NY. |
| 2020-24-06 | Flight Controls | Dec 28, 2020 | Airframe (525A)Only with: With Tamarack active load alleviation system (ATLAS) winglets installed in accordance with STC SA03842NY. |
| 2010-12-01 | Cessna Aircraft Company Model 525A Airplanes | Jul 22, 2010 | Airframe (525A)Certain serial numbers: 525A 0001–0244 |
| 2008-03-10 | Cessna Aircraft Company Models 525, 525A, and 525B Airplanes | Mar 11, 2008 | Airframe (525A)Certain serial numbers: 525 0001–0637; 525A 0001–0347; 525B 0001–0152. Only with: Cockpit mounted pilot relief tube installed. |
| 2005-17-11 | The Cessna Aircraft Company Models 525, 525A, and 525B Airplanes | Oct 7, 2005 | Airframe (525A)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.
THE CREW REPORTS THE OXYGEN MASC CONTINUOUSLY FLOW OF OXYGEN AT 100 % FLOW, ATTEMPTEN TO STOP FLOW WITHOUT SUCCESS MASC WAS DISCONNECTED O2 FLOW STOPPED.MAINTENANCE REPLACED THE MASK WITH OVERHUALED UNIT
From FAA Service Difficulty Reports; matched by N-number and serial number.THE CREW REPORTED HOT AIR OUT OF THE LOWER AIR REGISTERS, THE FREON SYSTEM NOT ABLE TO COMPENSATE FOR THE EXCESSIVE AIR DISCHARGE.TROUBLE SHOT THE SYSTEM AND FOUND THE PRSOV PRESSURE REGULATION SHOT OFF VALVES NOT REGULATING AIR TEMPERATURS.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING CLIMBOUT FROM HOME BASE THE CREW NOTED THE HYDRAULIC PRESSURE ON ANNUNCIATION AND THE LEFT HAND THRUST ATTENUATOR LAMP BLINKING.THE CREW EMERGENCY DEPLOYED THE MAIN LANDING GEAR DUE TO HYDRAULIC LOSS. LANDING WAS NORMAL POST FLIGHT WALK AROUND HYDRAULIC FLUID WAS NOTED DRIPPING IN THE AREA…
From FAA Service Difficulty Reports; matched by N-number and serial number.