What was found
ELEVEN CORRODED HOLES ON STRESS PANEL 521AT. ELEVEN BUSHINGS FABRICATED LOCALLY IAW WITH RD 8-53-2674 ACCESS PANEL 521AT REPLACED ON SEQ 5042.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ELEVEN CORRODED HOLES ON STRESS PANEL 521AT. ELEVEN BUSHINGS FABRICATED LOCALLY IAW WITH RD 8-53-2674 ACCESS PANEL 521AT REPLACED ON SEQ 5042.