What was found
INSPECTION FOUND A 1.5" CRACK IN R/H FUSELAGE SKIN AFT OF TRAILING EDGE OF FLAP, BS 727E, S18R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01 AND ECRA 5330-03191.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5" CRACK IN R/H FUSELAGE SKIN AFT OF TRAILING EDGE OF FLAP, BS 727E, S18R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01 AND ECRA 5330-03191.