What was found
LWR FUSELAGE SKIN HAS GOUGE FROM PANEL FASTENER 1 IN. RT OF STR 44 AND 2 IN. AFT OF FR34. BLENDED AREA IAW SRM 51-73-00. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-11, DIAGRAM 105, SHEET 1. T
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LWR FUSELAGE SKIN HAS GOUGE FROM PANEL FASTENER 1 IN. RT OF STR 44 AND 2 IN. AFT OF FR34. BLENDED AREA IAW SRM 51-73-00. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-11, DIAGRAM 105, SHEET 1. T