The pilot's inadequate preflight inspection, which resulted in a loose battery charger becoming entangled in the rudder pedals during a spin recovery, and a subsequent overstress of the glider. Factors included the loose battery charger, and the non-standard battery charging procedure.
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (0)
No Service Difficulty Reports found for this airframe since 1995.