What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1009 TO 1029, STRINGER 52. THE CORRODED AREA WAS CUT OUT. REPAIR DOUBLERS, FINGER DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1009 TO 1029, STRINGER 52. THE CORRODED AREA WAS CUT OUT. REPAIR DOUBLERS, FINGER DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.