What was found
INSPECTION FOUND FUSELAGE COMPONENT P/N 102291-4 CRACKED BOTH SIDES IN THE 90 DEGREE ANGLE UNDER RIVETS THAT ATTACH TO BULKHEAD. ACTION DRILLED STOP HOLES AND INSTALLED REINFORCEMENT WITH NEW.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE COMPONENT P/N 102291-4 CRACKED BOTH SIDES IN THE 90 DEGREE ANGLE UNDER RIVETS THAT ATTACH TO BULKHEAD. ACTION DRILLED STOP HOLES AND INSTALLED REINFORCEMENT WITH NEW.