What was found
DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS, APPROX 2 INCHES INSIDE ACCESS PANEL 311UL OF NR 2 ENGINE INTAKE (LEFT SIDE OF S DUCT LOOKING UP AND AFT). REPAIRED PER SRM 54-12-00 FIG 803.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS, APPROX 2 INCHES INSIDE ACCESS PANEL 311UL OF NR 2 ENGINE INTAKE (LEFT SIDE OF S DUCT LOOKING UP AND AFT). REPAIRED PER SRM 54-12-00 FIG 803.