What was found
RT INBD FLAP CENTER L/E PANEL IS GOUGED ON LOWER SURFACE INBD SIDE. BLENDED DAMAGED AREA IAW AMM 57-53-00. REMAINING SKIN THICKNESS .073. ORIGINAL IS .080, WITHIN LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT INBD FLAP CENTER L/E PANEL IS GOUGED ON LOWER SURFACE INBD SIDE. BLENDED DAMAGED AREA IAW AMM 57-53-00. REMAINING SKIN THICKNESS .073. ORIGINAL IS .080, WITHIN LIMITS.