What was found
AT C-CHECK, RT WING T/E ANGLE CRACKED 2 INCHES AT XW 5.000. PERFORMED STOP DRILL IAW SRM 57-2-0 FIG 2, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0, FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, RT WING T/E ANGLE CRACKED 2 INCHES AT XW 5.000. PERFORMED STOP DRILL IAW SRM 57-2-0 FIG 2, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0, FIG 2.