Safety record in brief:2 NTSB accidents (substantial damage at worst, latest May 2005)1 AD may apply
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.
a partial loss of engine power, which resulted from the fuel servo leaking and generating an excessively rich fuel/air mixture. A factor was the owner's failure to comply with a service bulletin.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX05LA173)
WHILE ON CROSSWIND FOLLOWING TAKEOFF THE ENGINE LOST TOTAL POWER AFTER CLIMBING TO 500 FEET AGL. THE PILOT INITIATED A TURN TOWARD A FIELD AND COLLIDED WITH TREES ON THE APPROACH END OF THE FIELD. POST-CRASH EXAMINATION OF THE AIRCRAFT REVEALED THAT THE INDUCTION AIR HOSE HAD COLLAPSED AND WAS DRAWN INTO THE INDUCTION SYSTEM, RESTRICTING THE FLOW OF INDUCTION AIR TO THE ENGINE.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL86LA071)
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 |
|---|---|---|---|
| 2004-25-22 | Great Lakes Aircraft Company, LLC, Models 2T-1A-1 and 2T-1A-2 Airplanes | Jan 28, 2005 | Airframe (2T-1A-2)Only with: Airplanes with a Lycoming IO-360-B1F6, AIO-360-B1G6, or AEIO-360-B1G6 engine installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.