What was found
VISUALLY DETECTED LEAKING AREA BETWEEEN TIE BOLTS. CONFIRMED CRACK TUBE WALL ROTOR DRIVE KEY HOLE. NO CRACKS PERMITTED THIS AREA. BENDIX OHM 32-40-05 REV 15 DATE 10-15-96. CHECK SECTION PARA 2B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VISUALLY DETECTED LEAKING AREA BETWEEEN TIE BOLTS. CONFIRMED CRACK TUBE WALL ROTOR DRIVE KEY HOLE. NO CRACKS PERMITTED THIS AREA. BENDIX OHM 32-40-05 REV 15 DATE 10-15-96. CHECK SECTION PARA 2B.