As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STA 400 NOSE WHEEL WELL TORQUE BOX PRESSURE PAN (FOR NLG RETRACT ACT) FOUND CRACKED AT INBD LOWER CORNER AND UPPER OUTBD CORNER. REF SRM 53-11-20 FIG 12 SHT 12 ITEM 60. CRACKED PRESSURE PAN (3 PARTS) FABRICATED BY WORKSHOP AND INSTALLED IAW B747 SRM 51-10-01 P69.