What was found
INSPECTION FOUND A .375 INCH CRACK IN UPPER OUTBOARD FLANGE OF RT WING RIB AT WS 171.5, STRINGER 16. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .375 INCH CRACK IN UPPER OUTBOARD FLANGE OF RT WING RIB AT WS 171.5, STRINGER 16. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-6.