What was found
SEVERAL HOLES IN FUSELAGE SKIN ARE ELONGATED WHERE SERVICE DOOR OR THRESHOLD ATTACHES TO SKIN STRINGER 16R, FRAMES 20 - 22. REAMED DISCREPANT HOLES TO REMOVE DAMAGE AND PREP FOR INSTALLATION OF FREEZ PLUG BUSHING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SEVERAL HOLES IN FUSELAGE SKIN ARE ELONGATED WHERE SERVICE DOOR OR THRESHOLD ATTACHES TO SKIN STRINGER 16R, FRAMES 20 - 22. REAMED DISCREPANT HOLES TO REMOVE DAMAGE AND PREP FOR INSTALLATION OF FREEZ PLUG BUSHING.