What was found
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON FUSELAGE SKIN FORWARD OF E AND E COMPARTMENT ENTRY DOOR BETWEEN LONGERON 28 RIGHT AND 29 RIGHT. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 4, SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON FUSELAGE SKIN FORWARD OF E AND E COMPARTMENT ENTRY DOOR BETWEEN LONGERON 28 RIGHT AND 29 RIGHT. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 4, SHEET 3.