As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON CLIMBING THROUGH 6,000 FT WITH CLIMB POWER SET, THE RIGHT ENGINE SUDDENLY LOST APPROXIMATELY 10% OF N1 POWER. THE OTHER ENGINE INSTRUMENTS CORRELATED WITH THE LOSS OF POWER. PERFORMED HIGH POWER RUNS PER P/W AOG SUPPORT AND PW 545A EMM 71-00-00. OPS CK GOOD