What was found
FUSELAGE SKIN CRACKED AT STA 938 AND 1FT ABOVE STRINGER 25L.CRACK STARTS FROM SKIN RADIUS AND EXTENDS BEYOND RIVET HOLE, APPROX LOCATION IS 1FT FWD OF WATER SERVICE PANEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT STA 938 AND 1FT ABOVE STRINGER 25L.CRACK STARTS FROM SKIN RADIUS AND EXTENDS BEYOND RIVET HOLE, APPROX LOCATION IS 1FT FWD OF WATER SERVICE PANEL.