What was found
EXTERIOR FUSELAGE SKIN CORRODED AT BS 420+10, BETWEEN STRINGERS 28L TO 28R. REPAIRED THE SKIN IAW SRM IAW EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERIOR FUSELAGE SKIN CORRODED AT BS 420+10, BETWEEN STRINGERS 28L TO 28R. REPAIRED THE SKIN IAW SRM IAW EA.