What was found
WORN PREVIOUS REPAIR FILLER ON FUSELAGE SKIN BETWEEN BS 1287-1309 AND LONGERONS 18R-19R. FILLER WAS REPLACED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21 AND 53-04-2, FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WORN PREVIOUS REPAIR FILLER ON FUSELAGE SKIN BETWEEN BS 1287-1309 AND LONGERONS 18R-19R. FILLER WAS REPLACED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21 AND 53-04-2, FIG 2.