What was found
ACFT WAS FOUND WITH A 6MM CRACK FOR RIVET EDGE ON THE LT SKIN AT FRAME 75 BELOW STRINGER 2. MX INSTALL A SMALL PATCH TO THE FUSELAGE SKIN AT FRAME 75, STRINGER 2L IAW EC 5330-02353. PRESSURE CHECKED GOOD AND WAS RELEASED TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ACFT WAS FOUND WITH A 6MM CRACK FOR RIVET EDGE ON THE LT SKIN AT FRAME 75 BELOW STRINGER 2. MX INSTALL A SMALL PATCH TO THE FUSELAGE SKIN AT FRAME 75, STRINGER 2L IAW EC 5330-02353. PRESSURE CHECKED GOOD AND WAS RELEASED TO SERVICE.