What was found
LT OTBD FLAP, OTBD HINGE PANEL 526JL, CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT OTBD FLAP, OTBD HINGE PANEL 526JL, CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 10.