What was found
DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FUSELAGE SKIN AT FORWARD EDGE OF THE FORWARD CARGO COMPARTMENT DOOR JAMB HAD TWO CRACKS AND EXCESSIVE CORROSION BLENDOUTS. REPAIRED IAW ABX REA D953-13853-MR.
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 THE FUSELAGE SKIN AT FORWARD EDGE OF THE FORWARD CARGO COMPARTMENT DOOR JAMB HAD TWO CRACKS AND EXCESSIVE CORROSION BLENDOUTS. REPAIRED IAW ABX REA D953-13853-MR.