What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE AFT FUSELAGE FRAME AT BS 509.5 AND STRINGER 3L IN THE FLANGE BEND RADIUS, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-048.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE AFT FUSELAGE FRAME AT BS 509.5 AND STRINGER 3L IN THE FLANGE BEND RADIUS, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-048.