As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HNL - IN C-CHECK, RIGHT PYLON TO FUSELAGE TOP ATTACH ANGLE HAS A CRACK APPROX 1.5 INCHES LONG BELOW AFT PRESSURE BULKHEAD TEE CAP. REPLACED PYLON ANGLE. REPLACED FASTENERS IN VERTICAL LEG THROUGH FUSELAGE PER SRM 54-04. INSTALLED HORIZONTAL LEG FASTENERS PER SRM 54-04 PAINTED. LEAK CHECK OK. (M)