We’re still collecting data for this aircraft. Routes appear once we’ve seen it fly enough times.
FATIGUE FAILURE OF THE FORWARD SPAR FUSELAGE ATTACHMENT ASSEMBLY FOR THE RIGHT WING. A FACTOR RELATED TO THE ACCIDENT WAS: THE LACK OF A DIRECTED INSPECTION PROCEDURE THAT COULD HAVE BEEN PROVIDED WITH THE ISSUANCE OF AN AIRWORTHINESS DIRECTIVE.
Piper PA-25