What was found
FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER BAE FAX JM/RJ0491-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER BAE FAX JM/RJ0491-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)