What was found
DURING 1000-HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE FRAME # 5A AT FUSELAGE STATION 5,023MM. TWO CRACKS WERE LOCATED AT THE FLANGE RADIUS WHERE THE FRAME MEETS THE OUTER STRUCTURE AT THE UPPER LH AND RH SIDES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 1000-HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE FRAME # 5A AT FUSELAGE STATION 5,023MM. TWO CRACKS WERE LOCATED AT THE FLANGE RADIUS WHERE THE FRAME MEETS THE OUTER STRUCTURE AT THE UPPER LH AND RH SIDES.