What was found
BS 380 CRACKED AT I/B RIVET BETWEEN STRINGERS 8 & 9R AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE OF CABIN. ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE FRAME IAW EC/RA 5311-02172, EA5310-04716 REV. I .
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BS 380 CRACKED AT I/B RIVET BETWEEN STRINGERS 8 & 9R AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE OF CABIN. ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE FRAME IAW EC/RA 5311-02172, EA5310-04716 REV. I .