What was found
DURING SERVICE CHECK, FOUND A 4" FUSELAGE SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS807+3 STRINGER 18L. THE CRACK WAS REPAIRED IAW SRM 53-30-3, FIGURE 48, DETAIL XI.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SERVICE CHECK, FOUND A 4" FUSELAGE SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS807+3 STRINGER 18L. THE CRACK WAS REPAIRED IAW SRM 53-30-3, FIGURE 48, DETAIL XI.