As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK AT FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL). FWD SUPPORT ANGLES (2EA) OF UPPER ACUMULATOR AT NOSE HYDRAULICS COMPARTMENT INTERNAL STRUCTURE (INSIDE ACCESS PANEL 121AL) WERE REPLACED PER SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01 .