What was found
CORROSION ON FUSELAGE SKIN BELOW FILLET PANEL RUBSTRIP AREA ON BS 807 BETWEEN LONGERONS 28-29R. SKIN REPAIRED IAW SRM 53-04, FIG 57, 51-30-5, 51-30-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE SKIN BELOW FILLET PANEL RUBSTRIP AREA ON BS 807 BETWEEN LONGERONS 28-29R. SKIN REPAIRED IAW SRM 53-04, FIG 57, 51-30-5, 51-30-1.