What was found
A WALKAROUND INSPECTION FOUND A 3" CRACK IN L/H FUSELAGE SKIN AT STA 727C, STRINGER 25L AND 26L. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-00, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A WALKAROUND INSPECTION FOUND A 3" CRACK IN L/H FUSELAGE SKIN AT STA 727C, STRINGER 25L AND 26L. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-00, FIGURE 201.