What was found
FUEL TANK PANEL 525AT HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.116" WHICH IS WITHIN LIMITS. APPLIED ALODINE, PRIMED. 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 525AT HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-442. CONFIRMED CRACK FREE. MINIMUM THICKNESS REMAINING IS 0.116" WHICH IS WITHIN LIMITS. APPLIED ALODINE, PRIMED. INSTALLED INNER AND OUTER SEALS.