Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Oct 1988)3 ADs may apply
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DURING THE LANDING ROLL, THE AIRPLANE BEGAN TO VEER TO THE RIGHT. THE PILOT APPLIED HARD LEFT RUDDER FOR A FEW SECONDS, THEN THE LEFT MAIN TIRE CAME OFF THE RIM. SUBSEQUENTLY, THE LEFT GEAR COLLAPSED AND THE AIRPLANE CAME TO REST PARTLY OFF THE RUNWAY.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX89LA024)
DURING A CROSS COUNTRY FLIGHT, THE ENGINE SUDDENLY QUIT, RESTARTED, THEN QUIT COMPLETELY. A FORCED LANDING WAS MADE IN A DRY WASH WHERE THE AIRCRAFT NOSED OVER DURING THE LANDING ROLL. APPROXIMATELY 4 GALLONS OF FUEL WAS DRAINED FROM THE FUEL SYSTEM. THERE WERE NO MECHANICAL FAILURES OR MALFUNCTIONS FOUND AT THE TIME OF THE ENGINE INSPECTION. THE ENG RAN SATISFACTORILY AT ALL POWER SETTINGS…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX88LA164)
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 |
|---|---|---|---|
| 2009-22-02 | American Champion Aircraft Corp. Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC… | Dec 3, 2009 | Airframe (8GCBC)Only with: Manufactured prior to 1989 and equipped with folding rear seat backs. |
| 2005-24-10 | American Champion Aircraft Corporation Models 7AC, 7ACA, S7AC, 7BCM, 7CCM, S7CCM, 7DC… | Jan 17, 2006 | Airframe (8GCBC)Only with: Models 7ECA, 7GCAA, 7GCBC, 8KCAB, 8GCBC manufactured before August 12, 2005 with less than 250 hours TIS; or any listed model with a flight control cable (or wing retrofit kit cable) purchased from ACAC before August 12, 2005 installed and less than 250 hours TIS since installation. |
| 2000-25-02 R1 | American Champion Aircraft Corporation 7, 8, and 11 Series Airplanes | Jul 13, 2001 | Airframe (8GCBC)Only with: Airplanes equipped with wood wing spars; Group 1 vs Group 2 depends on whether the engine has been modified to greater than 90 horsepower. |
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.