What was found
FUSELAGE SKIN UNDER LEFT STATIC PORT PLATE WAS CORRODED. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN UNDER LEFT STATIC PORT PLATE WAS CORRODED. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 3.