What was found
CANNOT MAINTAIN MAX CONTINOUS THRUST THROUGH CLIMB-OUT ON NR 1 ENGINE. ENGINE RUNS APPROX 80 DEGREES HOTTER THAN NR 2 OR NR 3. REMOVED AND REPLACED ENGINE PER TASK MANUAL 71-01-17.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CANNOT MAINTAIN MAX CONTINOUS THRUST THROUGH CLIMB-OUT ON NR 1 ENGINE. ENGINE RUNS APPROX 80 DEGREES HOTTER THAN NR 2 OR NR 3. REMOVED AND REPLACED ENGINE PER TASK MANUAL 71-01-17.