What was found
THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 598, LONGERON 25R TO 26R. REPAIRED PER SRM 53-04, FIG 12C, AND AREA NUMBER 1 ON ARA 18438A. CHECK-C 8-15-02 STL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN WAS DAMAGED AT STA 586 TO 598, LONGERON 25R TO 26R. REPAIRED PER SRM 53-04, FIG 12C, AND AREA NUMBER 1 ON ARA 18438A. CHECK-C 8-15-02 STL.