What was found
INSPECTION FOUND FUSELAGE SKIN BUCKLED WITH STRESSED RIVETS AT BS 500D + 10, S28R, RBL 10. A REPAIR WAS INSTALLED IAW SRM 53-30-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN BUCKLED WITH STRESSED RIVETS AT BS 500D + 10, S28R, RBL 10. A REPAIR WAS INSTALLED IAW SRM 53-30-12.