What was found
CLT - .5 INCH CRACK AT NR 4 FORWARD CAP RIB AT LOWER FLANGE RADIUS AND TORQUE ROD CUT OUT. CRACK WAS VISUALLY FOUND BY CLT INSPECTION. REPAIRED NR 4 CAP RIB. FABRICATED NEW RIB, PER SRM 57-02-03 AND SRM 20-30-06. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - .5 INCH CRACK AT NR 4 FORWARD CAP RIB AT LOWER FLANGE RADIUS AND TORQUE ROD CUT OUT. CRACK WAS VISUALLY FOUND BY CLT INSPECTION. REPAIRED NR 4 CAP RIB. FABRICATED NEW RIB, PER SRM 57-02-03 AND SRM 20-30-06. (M)