This N-number isn't registered right now. Below is its last known registration, canceled Jan 25, 2018.
Safety record in brief:1 NTSB accident (substantial damage, Mar 2001)3 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 premature retraction of the landing gear and the failure of the CFI to properly supervise the flight.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX01LA143)
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 (C35)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 (C35)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 (C35) |
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.
SUPPORT REMOVED FOR SMALL CRACK IN UPPER FLANGE. UPON REMOVAL OF CABIN AIR INLET DUCT FROM FORWARD BULKHEAD, FOUND SUPPORT COMPLETELY SEVERED AT POINT SUPPORT PASSES THROUGH TUNNEL ASSY AND ATTACHES TO KEEL. SAME CONDITIONS FOUND ON RT SIDE ALTHOUGH NOT AS OBVIOUS. ENGINE MOVEMENT CAUSED NUMEROUS…
From FAA Service Difficulty Reports; matched by N-number and serial number.SUPPORT REMOVED FOR SMALL CRACK IN UPPER FLANGE. UPON REMOVAL OF CABIN AIR INLET DUCT FROM FORWARD BULKHEAD, FOUND SUPPORT COMPLETELY SEVERED AT POINT SUPPORT PASSES THROUGH TUNNEL ASSY AND ATTACHES TO KEEL. SAME CONDITIONS FOUND ON RT SIDE ALTHOUGH NOT AS OBVIOUS. ENGINE MOVEMENT CAUSED NUMEROUS…
From FAA Service Difficulty Reports; matched by N-number and serial number.