What was found
DURING LINE CHECK, FOUND A 6 INCH CRACK IN THE FUSELAGE SKIN AT APPROXIMATELY FS 320, RIGHT SIDE AFT OF FORWARD LAV SERVICE PANEL. REPAIRED PER SRM 53-30-3 FIG 3A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING LINE CHECK, FOUND A 6 INCH CRACK IN THE FUSELAGE SKIN AT APPROXIMATELY FS 320, RIGHT SIDE AFT OF FORWARD LAV SERVICE PANEL. REPAIRED PER SRM 53-30-3 FIG 3A.