As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE C/O DVI INSPECTION PER SB 747-53A2562 R3 STEP 22, FOUND UPPER INNER SIDE ANGLE 65B07941-544 FOUND CRACKED AT NOSE W/W RT TOP PANEL BS 260 - 340, RBL 30. >NOSE W/W R/H UPPER INNER NEW SIDE ANGLE TOP PANEL STA 260 - STA 340 RBL 30 (05 EA) FASTENER HOLES EDGE MARGIN FOUND ACCEPTABLE AND INSTALLED AS PER EN 3595-26 REV. 0. REPAIR CLASSIFIED AS MAJOR REPAIR WITH FIRST AND SECOND STAGE APPROVAL. NO ADDITIONAL STRUCTURAL WORK REQUIRED.