What was found
STRINGER 24S CLIP IS CORRODED AT FR 584.5. REMOVED STRINGER CLIP IAW SRM 51-42-05-02-01. INSTALLED NEW CLIP PER Q400 SRM 51-42-05-02-01. APPLIED ALUMINIZED PAINT IAW Q400 SRM 51-21-15-02-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER 24S CLIP IS CORRODED AT FR 584.5. REMOVED STRINGER CLIP IAW SRM 51-42-05-02-01. INSTALLED NEW CLIP PER Q400 SRM 51-42-05-02-01. APPLIED ALUMINIZED PAINT IAW Q400 SRM 51-21-15-02-01.