What was found
INSPECTION FOUND AILERON SPARS CRACKED. LOCATION: INBOARD HINGE BRACKET ATTACH POINT. LT AILERON HAD .75 INCH CRACK. RT AILERON HAD 2.25 INCH CRACK. CAUSE COULD BE RELATED TO TOTAL TIME.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND AILERON SPARS CRACKED. LOCATION: INBOARD HINGE BRACKET ATTACH POINT. LT AILERON HAD .75 INCH CRACK. RT AILERON HAD 2.25 INCH CRACK. CAUSE COULD BE RELATED TO TOTAL TIME.