What was found
BLADE REMOVED FOR BIM INDICATION. THE SPAR IS CRACKED ON BOTTOM SIDE UNDER NR 9 POCKET, APPROXIMATELY 1 INCH STARTING AT BACK WALL RADIUS, RUNNING CHORDWISE TOWARDS LEADING EDGE. PROBABLE CAUSE: CORROSION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BLADE REMOVED FOR BIM INDICATION. THE SPAR IS CRACKED ON BOTTOM SIDE UNDER NR 9 POCKET, APPROXIMATELY 1 INCH STARTING AT BACK WALL RADIUS, RUNNING CHORDWISE TOWARDS LEADING EDGE. PROBABLE CAUSE: CORROSION.