This N-number isn't registered right now. Below is its last known registration, canceled Dec 10, 2013.
Safety record in brief:1 NTSB accident (substantial damage, Jan 2004)3 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 loss of directional control as a result of reduced braking performance due to a snow-covered runway. Also causal was the pilot's decision to land with a quartering tailwind. The snowbank was a contributing factor.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI04LA058)
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 (310R) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
| 98-04-28 | Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414… | Mar 13, 1998 | Airframe (310R) |
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.
DURING AN OPS NR 1 INSP, FOUND THE LT MLG PUSH/PULL ROD LOOSE AT ROD END. DURING GEAR RETRACTION TO GAIN ACCESS TO PART FOR REPLACEMEN, TOTAL FAILURE OF THE ROD END OCCURRED CAUSING LOSS OF MOVEMENT OF THE LEFT MAIN GEAR ASSY TO THE UP OR DOWNLOCK POSITION. SUBMITTER RECOMMENDS CLOSE INSP OF THIS…
From FAA Service Difficulty Reports; matched by N-number and serial number.