What was found
THE FUSELAGE SKIN WAS DAMAGED AT STA 596 TO 605, LONGERON 26R AREA. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3. 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 596 TO 605, LONGERON 26R AREA. SPLICED IN NEW SECTION OF SKIN PER SRM 53-04, FIG 12C, AND ARA 18438A, REPAIR AREA NUMBER 3. CHECK-C 8-15-02 STL.