What was found
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT BS 177.35 AND STRINGER 13L AT THE FRAME FLANGE BEND RADIUS 1.2 INCHES FROM THE OTBD EDGE RADIATING INBD. REPAIRED IAW EO 13-1900-53-065. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT BS 177.35 AND STRINGER 13L AT THE FRAME FLANGE BEND RADIUS 1.2 INCHES FROM THE OTBD EDGE RADIATING INBD. REPAIRED IAW EO 13-1900-53-065. MAJOR REPAIR.