What was found
LOWER FWD FUSELAGE SKIN BETWEEN FRAMES 26 & 27, STRINGERS 41 & 42R DENTED. FOUND WITHIN LIMITS IAW SRM 53-21-11, DIAGRAM 103. HFEC INSPECTED INTERNAL & EXTERNAL AREA IAW NTM 51-10-08, NO CRACK INDICATION NOTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FWD FUSELAGE SKIN BETWEEN FRAMES 26 & 27, STRINGERS 41 & 42R DENTED. FOUND WITHIN LIMITS IAW SRM 53-21-11, DIAGRAM 103. HFEC INSPECTED INTERNAL & EXTERNAL AREA IAW NTM 51-10-08, NO CRACK INDICATION NOTED.