As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 24S IS CORRODED BETWEEN STA 529.5 AND 547.0. ACFT IS DOWN FOR C-CHECK. REMOVED CORROSION IAW 51-21-00-00-02. PERFORMED HFEC FOR CRACK IAW NDTM PT 1, 51-00-06-910-801, NO CRACKS NOTED. PERFORMED UT THICKNESS IAW NDTM PT 1, 51-00-04-910-801. MINIMUM REMAINING THICKNESS .064" FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4282. ALODINED, PRIMED AND APPLIED TOP COAT IAW RD 8/4-53-4282.