What was found
INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE ATTACH ANGLE AT STA 1059, LONGERON 15R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE ATTACH ANGLE AT STA 1059, LONGERON 15R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.