What was found
DURING D-CK, FOUND AREA OF CORROSION ON FUSELAGE SKIN BEYOND LIMITS AT STA 697 TO 702 BETWEEN LONGERON 25R AND 26R. INSTALLED REPAIR IAW SRM 53-04, FIG 53.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CK, FOUND AREA OF CORROSION ON FUSELAGE SKIN BEYOND LIMITS AT STA 697 TO 702 BETWEEN LONGERON 25R AND 26R. INSTALLED REPAIR IAW SRM 53-04, FIG 53.