What was found
PANEL 414AL HAS A CRACK ON 3RD RIB. REPLACED STIFFENER IAW SRM 51-42-05, STEP 4D(3-10).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 414AL HAS A CRACK ON 3RD RIB. REPLACED STIFFENER IAW SRM 51-42-05, STEP 4D(3-10).