What was found
DURING CLIMB ENGINE 1 WOULD NOT ACHIEVE COMMAND POWER SETTING AFTER INITIAL THRUST REDUCTION FROM TAKEOFF POWER ENGINE 1N HUNG BELOW 70% WHILE N2 INCREASED TO LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CLIMB ENGINE 1 WOULD NOT ACHIEVE COMMAND POWER SETTING AFTER INITIAL THRUST REDUCTION FROM TAKEOFF POWER ENGINE 1N HUNG BELOW 70% WHILE N2 INCREASED TO LIMITS.