What was found
OBSERVED A CRACK ON THE FORWARD SIDE OF VERTICAL LEG AT FUSELAGE STATION JUST BELOW RADIUS & ABOVE STRINGER 6L. REPAIRED CHORD IAW SRM 53-80-08 REPAIR 9 & EA 253171 & 253080.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
OBSERVED A CRACK ON THE FORWARD SIDE OF VERTICAL LEG AT FUSELAGE STATION JUST BELOW RADIUS & ABOVE STRINGER 6L. REPAIRED CHORD IAW SRM 53-80-08 REPAIR 9 & EA 253171 & 253080.