What was found
INSPECTION FOUND A .625 INCH CRACK IN LT FUSELAGE SKIN AT STA 69 TWO FEET BELOW CUSP LINE. REPAIRED IAW SRM 53-01, FIGURE 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .625 INCH CRACK IN LT FUSELAGE SKIN AT STA 69 TWO FEET BELOW CUSP LINE. REPAIRED IAW SRM 53-01, FIGURE 4.