What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 727E, S24L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 727E, S24L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.