What was found
NACELLE PANEL 414AR AFT STIFFENER IS CRACKED. REMOVED STIFFENER AND INSTALLED NEW IAW SRM 51-42-05-02-01. TREATED AND PAINTED IAW SRM 51-25-05-02-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NACELLE PANEL 414AR AFT STIFFENER IS CRACKED. REMOVED STIFFENER AND INSTALLED NEW IAW SRM 51-42-05-02-01. TREATED AND PAINTED IAW SRM 51-25-05-02-01.