Safety record in brief:1 NTSB accident (substantial damage, Sep 1996)1 AD 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.
fatigue failure of the propeller blade. Factors relating to the accident were: corrosion pit(s) on the propeller blade, and inadequate maintenance/inspection of the propeller.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL96LA131)
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 (A23)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 |
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.
WITH AIRCRAFT AT CRUISE, 2,500 RPM., ONE BLADE FAILED AT 14.6250 INCHES FORM CENTER OF HUB. IT WAS A CLEAN BREAK WITH NO SIGN OF NICK OR SCRATCH ANYWHERE ON THE BLADE. ENGINE VIBRATION BROKE ALL 4 ENGINE MOUNTS. ENGINE DROPPED INTO BOTTOM OF COWLING AND SHUT-DOWN. PILOT DEAD STICKED AIRCRAFT TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.