What was found
DURING THE INSPECTION PROCESS, IT WAS FOUND LOWER FUSELAGE FRAME 500B WIRE PENETRATION AREA WITH A CRACK BETWEEN S-20R AND S-21R, THE AREA IS AFFECTED BY STC DUE TO THIS SITUATION, A REPAIR IS INSTALLED UNDER EO4763 INSTRUCTIONS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING THE INSPECTION PROCESS, IT WAS FOUND LOWER FUSELAGE FRAME 500B WIRE PENETRATION AREA WITH A CRACK BETWEEN S-20R AND S-21R, THE AREA IS AFFECTED BY STC DUE TO THIS SITUATION, A REPAIR IS INSTALLED UNDER EO4763 INSTRUCTIONS.