What was found
CORROSION ON STRG 59 BETWEEN FRAME 55/58-59, REMAINING THICKNESS OUT OF LIMIT. CONNECTING SECTION REPAIRED 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 59 BETWEEN FRAME 55/58-59, REMAINING THICKNESS OUT OF LIMIT. CONNECTING SECTION REPAIRED IAW SRM 53-10-14/FIG 201.