What was found
AIR TURNBACK, DURING CLIMB OUT THE NR 1 ENGINE WOULD NOT PRODUCE MORE THAN 86.9% N1 THRUST. R&R HYDRO MECHANICAL UNIT PER MT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AIR TURNBACK, DURING CLIMB OUT THE NR 1 ENGINE WOULD NOT PRODUCE MORE THAN 86.9% N1 THRUST. R&R HYDRO MECHANICAL UNIT PER MT.