What was found
CORROSION ON TRANSITION PANEL AT STRINGER 38R, BETWEEN FRAMES 50 AND 52A. REPLACED TRANSISTION PANEL IAW SRM 51-42-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON TRANSITION PANEL AT STRINGER 38R, BETWEEN FRAMES 50 AND 52A. REPLACED TRANSISTION PANEL IAW SRM 51-42-11.