What was found
CRACK IN FUSELAGE MAIN FRAME FITTING UNDER CABIN FLOOR AT STA 616 RBL 70, INNER CHORD AT BOTTOM 2 RIVETS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE MAIN FRAME FITTING UNDER CABIN FLOOR AT STA 616 RBL 70, INNER CHORD AT BOTTOM 2 RIVETS.