What was found
FUEL TANK PANEL 624AT HAS CORROSION. REMOVED CORROSION IAW R/D 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.118" WHICH IS WITHIN TOLERANCE. APPLIED ALODINE, PRIMER AND INSTALLED INNER AND OUTER SEALS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUEL TANK PANEL 624AT HAS CORROSION. REMOVED CORROSION IAW R/D 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.118" WHICH IS WITHIN TOLERANCE. APPLIED ALODINE, PRIMER AND INSTALLED INNER AND OUTER SEALS.