What was found
During Hck in ATL, the L/H wing spar revealed corrosion in the lower spar cap at the inbd and outbd attach holes for the flap hinge fitting. A .625 crack was found at the inboard hole. Repaired per EA 96-188409.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
During Hck in ATL, the L/H wing spar revealed corrosion in the lower spar cap at the inbd and outbd attach holes for the flap hinge fitting. A .625 crack was found at the inboard hole. Repaired per EA 96-188409.