As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 24S SPLICE IS CORRODED ON BOTH SIDES OF FRAME 116. SPLICE FOUND TO BE OUT OF LIMITS REF SRM 53-20-03-00-01. REMOVED SPLICE REF SRM 51-42-05-02-01. MATCH DRILLED NEW SPLICE REF 51-40-07-02-01. INSTALLED STRINGER SPLICE REF 51-42-05-02-01. APPLIED PRIMER, ALUMINIZED TOP COAT, AND EXTERIOR TOP COAT REF SRM 51-25-10-02-01, 51-25-15-02-01 AND 51-25-05-02-01.