What was found
CORROSION ON STRG 55 LHS BETWEEN FRAME 75-76, REMAINING THICKNESS OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON STRG 55 LHS BETWEEN FRAME 75-76, REMAINING THICKNESS OUT OF LIMIT. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.