What was found
DURING ROUTINE INSPECTION, LWR FLOORBEAM CORROSION AT BS 848 FROM RBL 0 - 24 AND CRACKED AT RBL 1. REMOVED CORROSION IAW SRM 51-10-6, STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE AND SUPPORT DOUBLER IAW 51-40-3 & 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, LWR FLOORBEAM CORROSION AT BS 848 FROM RBL 0 - 24 AND CRACKED AT RBL 1. REMOVED CORROSION IAW SRM 51-10-6, STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE AND SUPPORT DOUBLER IAW 51-40-3 & 51-30-2.