What was found
DURING ROUTINE 100 HR INSPECTION A CRACK WAS FOUND RADIATING HORIZONTALLY FROM THE SECOND HOLE FROM THE ONE END AND ACROSS THE CORNER OF THE FIRST HOLE ON THE OPPOSITE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE 100 HR INSPECTION A CRACK WAS FOUND RADIATING HORIZONTALLY FROM THE SECOND HOLE FROM THE ONE END AND ACROSS THE CORNER OF THE FIRST HOLE ON THE OPPOSITE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL. (K)