What was found
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, BETWEEN LONGERON 13R AND 14R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, BETWEEN LONGERON 13R AND 14R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 18.