What was found
FOLLOW ON ACTION, ON FUSELAGE SKIN DAMAGE AND STRINGER DAMAGE STA 1417 TO STA 1439 S-38R TO S-38L AFTER ADDITIONAL CUTOUT PERFORMED, FOUND SKIN AT AFT SIDE OF CUTOUT TO BE .063" THICK. OPEN
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOLLOW ON ACTION, ON FUSELAGE SKIN DAMAGE AND STRINGER DAMAGE STA 1417 TO STA 1439 S-38R TO S-38L AFTER ADDITIONAL CUTOUT PERFORMED, FOUND SKIN AT AFT SIDE OF CUTOUT TO BE .063" THICK. OPEN