What was found
ON CLIMBOUT OBSERVED AN N1 RPM SPLIT OF APPROX. 5% #2 ENGINE WAS LOW. COULD NOT MANUALLY INCREASE THRUST ON #2. / R&R HYDRO MECHANICAL UNIT PER MT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON CLIMBOUT OBSERVED AN N1 RPM SPLIT OF APPROX. 5% #2 ENGINE WAS LOW. COULD NOT MANUALLY INCREASE THRUST ON #2. / R&R HYDRO MECHANICAL UNIT PER MT.