What was found
INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 876 BETWEEN S23L AND S24L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, REPAIR 31, 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 876 BETWEEN S23L AND S24L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, REPAIR 31, FIGURE 201.