What was found
INSPECTION FOUND THREE 1 INCH CRACKS AT FASTENER HOLES IN FUSELAGE SKIN AT STA Y= 1104, X= 30. THE CRACKS WERE STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THREE 1 INCH CRACKS AT FASTENER HOLES IN FUSELAGE SKIN AT STA Y= 1104, X= 30. THE CRACKS WERE STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.