What was found
FUSELAGE SKIN HAS 2.5 INCH CRACK THROUGH LAP SEAM RIVETS AT STA 1022 LONG 14L. REPAIRED PER AIRTRAN EA 17-53-01127IR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS 2.5 INCH CRACK THROUGH LAP SEAM RIVETS AT STA 1022 LONG 14L. REPAIRED PER AIRTRAN EA 17-53-01127IR.