What was found
FUSELAGE STRUCTURE PRESSURE WEB CORRODED. WEB IS LOCATED AT FS 46 IN THE MAIN LANDING GEAR WHEEL WELL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STRUCTURE PRESSURE WEB CORRODED. WEB IS LOCATED AT FS 46 IN THE MAIN LANDING GEAR WHEEL WELL.