What was found
INSPECTION FOUND A 1.5 INCH CRACK IN LT WING RIB. THE CRACK WAS LOCATED AT LOWER FLANGE WHERE IT MOUNTS TO SECOND FROM FORWARD END HEAVY STRINGER, WS 656.50, ACCESS CUTOUT 7217. THE RIB WAS REPAIRED IAW SRM 57-10-5, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN LT WING RIB. THE CRACK WAS LOCATED AT LOWER FLANGE WHERE IT MOUNTS TO SECOND FROM FORWARD END HEAVY STRINGER, WS 656.50, ACCESS CUTOUT 7217. THE RIB WAS REPAIRED IAW SRM 57-10-5, FIGURE 1.