What was found
EXCESSIVE CORROSION PITTING ON SPLINES OF COUPLING AFTER 6,317 HRS. IMPROPER HEAT TREATMENT COULD HAVE BEEN A FACTOR IN THE MALFUNCTION. OPER CONTROL NR 2010.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXCESSIVE CORROSION PITTING ON SPLINES OF COUPLING AFTER 6,317 HRS. IMPROPER HEAT TREATMENT COULD HAVE BEEN A FACTOR IN THE MALFUNCTION. OPER CONTROL NR 2010.