Safety record in brief:1 NTSB accident (substantial damage, Nov 2023)2 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.
Aeroelastic flutter of the rudder control surface during the takeoff initial climb for reasons that could not be determined based on the available evidence, which resulted in the fracture of the rudder trim control rod end in flight.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR24LA038)
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 |
|---|---|---|---|
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (95)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798 |
| 97-14-15 | Raytheon Aircraft Company (Formerly Known as Beech Aircraft Corporation) Models E33… | Sep 2, 1997 | Airframe (95) |
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.
FORWARD RUDDER TRIM TAB CONTROL ROD END BROKE. UN CONTROLLED RUDDER TAB CAUSED SEVERE OSCILLATIONS RESULTING IN WINDSHIELD SEPARATED FROM THE AIRCRAFT.
From FAA Service Difficulty Reports; matched by N-number and serial number.