What was found
CRACKED INNER SKIN ON SLAT PANEL 2, XOS 222. DAMAGE REMOVED IAW SRM 57-09, FIG 108. DOUBLER AND FILLER WERE FABRICATED IAW SRM 57-09, FIG 10B. REPAIR TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14/21 AND SRM 57-09, FIG 10B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED INNER SKIN ON SLAT PANEL 2, XOS 222. DAMAGE REMOVED IAW SRM 57-09, FIG 108. DOUBLER AND FILLER WERE FABRICATED IAW SRM 57-09, FIG 10B. REPAIR TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14/21 AND SRM 57-09, FIG 10B.