This N-number isn't registered right now. Below is its last known registration, canceled Mar 28, 2000.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Feb 1999)1 AD 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 pilot's improper positioning of the fuel selector. Factors to the accident were the transmission wires, the building, and the flood levy wall.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI99LA095)
the pilot's inadequate fuel consumption calculations which led to fuel exhaustion and the pilot's selection of an unsuitable landing area for the forced landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI96LA212)
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 |
|---|---|---|---|
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (C23)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 |
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.
CRACKS IN STABILATOR MAIN SPAR ADJACENT TO FUSELAGE HINGE ATTACHMENT FITTINGS. AIRCRAFT USED FOR FLIGHT TRAINING. CRACKS DUE TO FATIGUE. SUBMITTER RECOMMENDED DETAILED INSPECTION OF THIS AREA AT EACH INSPECTION INTERVAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A ROUTINE 100-HOUR INSPECTION, CRACKS WERE FOUND IN THE RIB AT THE AILERON HINGE DOUBLER.
From FAA Service Difficulty Reports; matched by N-number and serial number.