What was found
INSPECTION FOUND THREE .25 INCH CRACKS FROM TWO RIVETS IN LT FUSELAGE SKIN AT STA 63 TEN INCHES BELOW CUSP LINE. THE CRACKED AREAS WERE CUT OUT, A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THREE .25 INCH CRACKS FROM TWO RIVETS IN LT FUSELAGE SKIN AT STA 63 TEN INCHES BELOW CUSP LINE. THE CRACKED AREAS WERE CUT OUT, A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38.