What was found
FUSELAGE SKIN ON FORWARD LOWER CORNER OF AFT LAVATORY SERVICE PAN IS SEPARATED FROM TITANIUM HOURGLASS. INSTALLED INTERNAL TITANIUM REPAIR DOUBLER AT THE AFT LAVATORY PAN CUT OUT AREA PER SRM 53-04-00 FIGURE 38 AND EA MD80-53-017519.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN ON FORWARD LOWER CORNER OF AFT LAVATORY SERVICE PAN IS SEPARATED FROM TITANIUM HOURGLASS. INSTALLED INTERNAL TITANIUM REPAIR DOUBLER AT THE AFT LAVATORY PAN CUT OUT AREA PER SRM 53-04-00 FIGURE 38 AND EA MD80-53-017519.