What was found
(CAN) MAIN ROTOR BLADE SKIN CRACKED AT DOUBLER LIP ON BOTTOM SIDE OF BLADE CHORDWISE. CRACK LENGTH 2 INCHES. RUNS UNDERNEATH SEALANT THAT BOND DOUBLER TO THE BLADE. FOUND DURING 100 HR INSPECTION M/R TORQUE EVENT INSPECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) MAIN ROTOR BLADE SKIN CRACKED AT DOUBLER LIP ON BOTTOM SIDE OF BLADE CHORDWISE. CRACK LENGTH 2 INCHES. RUNS UNDERNEATH SEALANT THAT BOND DOUBLER TO THE BLADE. FOUND DURING 100 HR INSPECTION M/R TORQUE EVENT INSPECTION.