Safety record in brief:1 NTSB accident (substantial damage, May 2000)3 ADs may apply
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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.
improper rigging of the rudder/elevators and differential mechanism assembly by unknown person(s), which resulting in what the pilot describes as inflight flutter of the tail section, which resulted in damage to the aft empennage area.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA00FA146)
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 |
|---|---|---|---|
| 94-20-04 R2 | Raytheon Aircraft Company Beech Models C35, D35, E35, F35, G35, H35, J35, K35, M35, N35… | Jun 27, 2003 | Airframe (F35)Only with: Models S35, V35, V35A, and V35B apply only if the straight tail conversion modification per STC SA2149CE is not incorporated. |
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (F35)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 (F35) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.