This N-number isn't registered right now. Below is its last known registration, canceled Aug 1, 2012.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jun 2000)2 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.
Fuel starvation due to the unavailability of fuel to the engine for undetermined reasons and the pilot's misjudgment of distance/altitude on final approach. Contributing factors were the pilot's premature gear extension and the berm.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for DEN00LA101)
the pilot's inadvertent raising the flaps during a go-around attempt. A factor in the accident was the gusty crosswind condition.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for LAX94LA253)
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 |
|---|---|---|---|
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (IO-540 SER)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
| 2004-05-24 | Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and… | Mar 30, 2004 | Engine (IO-540 SER)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos. |
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.
AFTER RUNNING LEFT WING TANK DRY, PILOT SWITCHED TO RIGHT WING TANK. ELECTRIC FUEL PUMP FAILED TO PICK UP FUEL AGAIN. INVESTIGATION REVEALED ELECTRIC PUMP HAD BEEN INSTALLED ON FIREWALL INSTEAD OF IN NOSE WHEELWELL AS PLANS INDICATED.
From FAA Service Difficulty Reports; matched by N-number and serial number.