What was found
INSPECTION FOUND A 2 INCH CRACK AND TWO .5 INCH CRACKS IN LT FUSELAGE SKIN AT STA 58 TWELVE INCHES BELOW CUSP LINE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS INSTALLED 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 2 INCH CRACK AND TWO .5 INCH CRACKS IN LT FUSELAGE SKIN AT STA 58 TWELVE INCHES BELOW CUSP LINE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4.