What was found
FUSELAGE SKIN FOUND CORRODED ON THE AVIONICS SKIN AIR INLET VALVE ATTACH SURFACE, FRAME 21+8, STRINGER 14L. REMOVED AND REPLACED THE SKIN DOUBLER IAW SRM 51-72-11, 51-42-11, AND 51-44-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN FOUND CORRODED ON THE AVIONICS SKIN AIR INLET VALVE ATTACH SURFACE, FRAME 21+8, STRINGER 14L. REMOVED AND REPLACED THE SKIN DOUBLER IAW SRM 51-72-11, 51-42-11, AND 51-44-11.