What was found
NR 2 ENGINE WOULD NOT DEVELOP CLIMB THRUST OUT OF 10,000 FEET, RETURNED TO DEPARTURE. R & R THE NR 2 ENGINE HYDRO MECHANICAL UNIT IAW MT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE WOULD NOT DEVELOP CLIMB THRUST OUT OF 10,000 FEET, RETURNED TO DEPARTURE. R & R THE NR 2 ENGINE HYDRO MECHANICAL UNIT IAW MT.