Safety record in brief:1 NTSB accident (substantial damage, Mar 1988)3 ADs may apply
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FIFTEEN MINUTES AFTER THE PILOT HAD TAKEN OFF ON A TOW PLANE OPERATION HE RETURNED TO THE LOCAL ARPT. AFTER LANDING HE TURNED DOWNWIND TO TAXI TO THE RAMP. THE WIND RAISED THE TAIL OF THE TAILWHEEL ACFT AND NOSED THE ACFT INVERTED. THE PILOT ESTIMATED THE WIND AT 18 KNOTS GUSTING TO 28.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI88LA085)
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.