What was found
DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN AT STA 623 BETWEEN LONGERONS 25L AND 25R. REPAIRED IAW DC-9 SRM 53-04, FIGURE 43.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN AT STA 623 BETWEEN LONGERONS 25L AND 25R. REPAIRED IAW DC-9 SRM 53-04, FIGURE 43.