What was found
DURING FUEL LEAK INVESTIGATION, FOUND OWS 28 LT WING FLAP TRACK RIB STIFFENER FITTING CRACKED APPROX 3 INCHES THROUGH THREE LOWER INBD ATTACH HOLES. REPLACED STIFFENER IAW SMP 583-57-60 PG 7 AND SMP 583-51-130 PG 47.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING FUEL LEAK INVESTIGATION, FOUND OWS 28 LT WING FLAP TRACK RIB STIFFENER FITTING CRACKED APPROX 3 INCHES THROUGH THREE LOWER INBD ATTACH HOLES. REPLACED STIFFENER IAW SMP 583-57-60 PG 7 AND SMP 583-51-130 PG 47.