What was found
DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON UPPER ACCESS PANEL 422AB STIFFENER FRAME CRACKED. REPLACED STIFFENER IAW SHORTS CMM 20-40-11, 20-42-06, 20-27-11 & 20-27-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON UPPER ACCESS PANEL 422AB STIFFENER FRAME CRACKED. REPLACED STIFFENER IAW SHORTS CMM 20-40-11, 20-42-06, 20-27-11 & 20-27-11.