What was found
CRACKS ON AFT FACE SLAT PANEL NR 2, BS XRS=240.000 APPROXIMATELY RT WING. CRACKS WERE REMOVED, FILLER AND DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED, IAW SRM 57-09 FIG 10-13 AND 51-10-3, PAR 21 AND 14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS ON AFT FACE SLAT PANEL NR 2, BS XRS=240.000 APPROXIMATELY RT WING. CRACKS WERE REMOVED, FILLER AND DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED, IAW SRM 57-09 FIG 10-13 AND 51-10-3, PAR 21 AND 14.