Safety record in brief:1 NTSB accident (substantial damage, Feb 1993)4 ADs may apply2 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 COLLISION WITH A ROAD SIGN DURING A FORCED LANDING. CONTRIBUTING TO THE ACCIDENT WAS THE TOTAL LOSS OF ENGINE POWER DUE TO FATIGUE FAILURE OF THE CRANKSHAFT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA93LA077)
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 |
|---|---|---|---|
| 2019-21-08 | Aileron Control System | Nov 22, 2019 | Airframe (N35)Certain serial numbers: F33A CE-290–CE-680; F33C CJ-26–CJ-128; V35B D-9069–D-9961; A36 E-185–E-925 |
| 94-20-04 R2 | Raytheon Aircraft Company Beech Models C35, D35, E35, F35, G35, H35, J35, K35, M35, N35… | Jun 27, 2003 | Airframe (N35)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 (N35)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 (N35) |
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.
UNCOMMANDED PROPELLER OVER SPEED, AND LOSS OF RPM CONTROL ON A NEWLY MANUFACTURED PISTON ENGINE POSSIBLY CAUSED BY ACCESSORY GEAR RETENTION BOLTS OVERTORQUED AT ASSEMBLY. -1.3 HOURS INTO A FLIGHT ON A NEW ENGINE, EXPERIENCED A SUDDEN UNCOMMANDED ENGINE OVERSPEED TO 3,800 RPM. PROP CONTROL WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number.ENGINE OVERSPEED IN FLIGHT, LOSS OF PROP CONTROL, LANDED WITHOUT INCIDENT. INSPECTED ON SITE BY LOYD'S AIRCRAFT AND FOUND LOOSE PROP BOLTS, AND METAL CONTAMINATION IN OIL PRESSURE RELIEF VALVE. METAL CONTAMINATION WAS ALSO FOUND IN THE OIL FILTER. ENGINE WAS REMOVED FROM AIRCRAFT AS DIRECTED BY…
From FAA Service Difficulty Reports; matched by N-number and serial number.