What was found
(LEFT WING) #2 SLAT COVE PANEL 524GB CRACKED / REMOVED #2 SLAT CORE PANEL 524GB PER SOPM 56556C 12OCT17 FABRICATED #2 SLAT CORE PANEL 524GB IAW SRM 51-40-05-0G-0 & DWG #114A8121. INSTALLED NEW PANEL IAW SOPM 20-50-01.55920U 04NOV17
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LEFT WING) #2 SLAT COVE PANEL 524GB CRACKED / REMOVED #2 SLAT CORE PANEL 524GB PER SOPM 56556C 12OCT17 FABRICATED #2 SLAT CORE PANEL 524GB IAW SRM 51-40-05-0G-0 & DWG #114A8121. INSTALLED NEW PANEL IAW SOPM 20-50-01.55920U 04NOV17