What was found
(4) CRACKS IN MAIN ROTOR BLADE UPPER SKIN AT BLADE STATION 75" APPROX 3" LONG, T/E AT BLADE STATION 78" APPROX .5" AND (2) IN INBD TRIM TAB AT BLADE STATION 152" APPROX .5" EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(4) CRACKS IN MAIN ROTOR BLADE UPPER SKIN AT BLADE STATION 75" APPROX 3" LONG, T/E AT BLADE STATION 78" APPROX .5" AND (2) IN INBD TRIM TAB AT BLADE STATION 152" APPROX .5" EA.