What was found
THE FUSELAGE SKIN WAS DAMAGED AT STA 576 TO 579, ABOVE LONGERON 26R, 3.75 INCHES BY 3.75 INCHES AND 0.056 IN DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 2. 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 576 TO 579, ABOVE LONGERON 26R, 3.75 INCHES BY 3.75 INCHES AND 0.056 IN DEEP. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 2. CHECK-C 8-15-02 STL.