As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AUS) RT SIDE NOSE LANDING GEAR TUNNEL WALL CRACKED IN AREA NEAR RT NOSE LANDING GEAR TORQUE TUBE STIFFENER PN 1213801-2. FURTHER INVESTIGATION OF THE STRUCTURE FOUND CRACKS IN THE LT AND RT NOSE GEAR TUNNEL WALLS LOCATED AT THE LOWER END OF THE FORWARD ENGINE SHOCK MOUNT ASSEMBLY CHANNEL. CRACKS WERE ALSO FOUND IN THE STIFFENERS PN 1213195-1 AND PN 1213195-2). AREA HAD BEEN MODIFIED IAW STC NO SA00796AT.