What was found
INSPECTION FOUND TWO PARALLEL SEMICIRCULAR CRACKS .25 INCH APART WITH 2 DIAMETERS IN RT FUSELAGE SKIN AT STA 200 SIX INCHES BELOW CUSP LINE. REPAIRED IAW SRM 53-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO PARALLEL SEMICIRCULAR CRACKS .25 INCH APART WITH 2 DIAMETERS IN RT FUSELAGE SKIN AT STA 200 SIX INCHES BELOW CUSP LINE. REPAIRED IAW SRM 53-04.