What was found
DAMAGE ON FUSELAGE SKIN BELOW RUB STRIPS AREA FROM BS 1117 - 1079 BETWEEN LONGERONS 25-30. . CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. AREAS WITHIN LIMITS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAMAGE ON FUSELAGE SKIN BELOW RUB STRIPS AREA FROM BS 1117 - 1079 BETWEEN LONGERONS 25-30. . CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. AREAS WITHIN LIMITS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14-21.