What was found
FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 RT SIDE AT BS 867. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME IS CRACKED AT OVERHEAD BIN RAIL ATTACHMENT BETWEEN STRINGERS 8 AND 9 RT SIDE AT BS 867. REPAIRED FRAME IAW ASA EA AD20062609 400 53 116 DATED 25 FEB 11.