What was found
AT HMV, CORROSION WAS FOUND ON FLOORBEAM BL0 TO RT FUSELAGE SKIN STA 324. REMOVED CORR AND CK LIMITS PER SRM 53-10-8 FIG 101. DRILLED REPAIR SPLICE ANGLES PER SRM 53-10-8 AND INSTALLED PER SAME.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT HMV, CORROSION WAS FOUND ON FLOORBEAM BL0 TO RT FUSELAGE SKIN STA 324. REMOVED CORR AND CK LIMITS PER SRM 53-10-8 FIG 101. DRILLED REPAIR SPLICE ANGLES PER SRM 53-10-8 AND INSTALLED PER SAME.