As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER CLIP, STRINGER 26S AT FRAME X-18.25 BUBBLING PAINT/PROBABLE CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. PART FOUND OUT OF LIMITS IAW SRM 53-20-15-00-01. NO DAMAGE ALLOWED. REMOVED STRINGER CLIP IAW SRM 51-42-05-02-01. MATCH DRILLED NEW PART IAW SRM 51-40-07-02-01. INSTALLED NEW STRINGER CLIP IAW SRM 51-42-05-02-01. APPLIED TOP COAT AND CPC IAW SRM 51-25-15-02-01 AND AMM 51-25-01-390-801.