Accident · destroyed
Apr 19, 2021 · Tatum, TXThe pilot’s loss of airplane control for undetermined reasons.
- Damage
- Destroyed
- Injuries
- Fatal
- Report
- CEN21FA195
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN21FA195)
This N-number isn't registered right now. Below is its last known registration, canceled Dec 31, 2022.
Safety record in brief:1 NTSB accident (destroyed damage, Apr 2021)4 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.
The pilot’s loss of airplane control for undetermined reasons.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN21FA195)
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 |
|---|---|---|---|
| 2016-17-08 | Elevator Tab Control System | Sep 12, 2016 | Airframe (340A) |
| 2000-01-16 | Cessna Aircraft Company 300 and 400 Series Airplanes | Feb 15, 2000 | Airframe (340A) |
| 98-24-14 | Cessna Aircraft Company Models 340A and 414A Airplanes | Dec 21, 1998 | Airframe (340A)Certain serial numbers: 340A 215–1817; 414A 1–1212. Only with: Equipped with any WYE tube P/N 9910299-25 or P/N 9910299-26 in the engine exhaust system. |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (340A) |
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.
WHILE PERFORMING VISUAL INSPECTION DURING ANNUAL INSPECTION, TECH NOTED STAINING BETWEEN CYLINDER FINS ON INTAKE SIDE OF CYLINDER NR 6 ON RT ENGINE. CYLINDER COMPRESSION CHECK AND BORESCOPE INSPECTION CONFIRMED THAT STAINING WAS DUE TO A CRACK BETWEEN INTAKE VALVE AND SPARK PLUG BOSS. CYLINDER SN…
From FAA Service Difficulty Reports; matched by N-number and serial number.