What was found
RT OTBD FLAP UPPER SURFACE SKIN IS SEPARATED FROM STRUCTURE DUE TO PULLED THRU FASTENERS 60" FROM OTBD END. REPAIRED IAW SRM 57-10-00, FIG 7, VOL I. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT OTBD FLAP UPPER SURFACE SKIN IS SEPARATED FROM STRUCTURE DUE TO PULLED THRU FASTENERS 60" FROM OTBD END. REPAIRED IAW SRM 57-10-00, FIG 7, VOL I. MAJOR REPAIR.