What was found
(CAN) MAIN ROTOR BLADE UPPER AND LOWER SKINS DEBONDED FROM TRAILING EDGE EXTRUSION FOR 66 INCHES FROM THE TIP INBOARD
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) MAIN ROTOR BLADE UPPER AND LOWER SKINS DEBONDED FROM TRAILING EDGE EXTRUSION FOR 66 INCHES FROM THE TIP INBOARD