What was found
FOUND 8 INCH CRACK ON LEADING EDGE OF RT WING ON FIRST RIB CAP OUTBD FUSELAGE. EXTERNAL DOUBLER REPAIR PER SRM 57-30-04 FIG 1. TIME LIMITED REPAIR PERMANENT FLUSH REPAIR NO LATER THAN 6 MONTHS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND 8 INCH CRACK ON LEADING EDGE OF RT WING ON FIRST RIB CAP OUTBD FUSELAGE. EXTERNAL DOUBLER REPAIR PER SRM 57-30-04 FIG 1. TIME LIMITED REPAIR PERMANENT FLUSH REPAIR NO LATER THAN 6 MONTHS.