As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 26S CORRODED FR 156 TO 176. BLENDED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .062", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3879. ALODINED, PRIMED IAW SRM 51-21-10-02-01, 51-25-10-02-01.