What was found
DURING CHECK-C MAINT THE FWD CARGO DOOR JAMB HAD CORROSION UNDER THE SCUFF PLATE, AIRCRAFT OUTER SKIN FROM LONGERON 28 TO 26, AND FROM STA 370 TO 427. REMOVED SURFACE CORROSION PER SPM 6-80-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT THE FWD CARGO DOOR JAMB HAD CORROSION UNDER THE SCUFF PLATE, AIRCRAFT OUTER SKIN FROM LONGERON 28 TO 26, AND FROM STA 370 TO 427. REMOVED SURFACE CORROSION PER SPM 6-80-01.