What was found
INSPECTION TYPE:C CRACK IN SECTION 41 FUSELAGE SKIN AT BS 211.8 R/H AT WL 197.5 REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3 USING 0.063" DOULER IAW EO B727-5330-0795-G
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C CRACK IN SECTION 41 FUSELAGE SKIN AT BS 211.8 R/H AT WL 197.5 REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3 USING 0.063" DOULER IAW EO B727-5330-0795-G