What was found
AFTER ROTATION NR 2 ENGINE FAILURE RETURNED TO CLE. NR 2 ENGINE FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED PER MM 73-11-01/72-60, PERFORMED POWER ASSURANCE RUN MM 71-09-266 PARTS CHG COMPLETE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER ROTATION NR 2 ENGINE FAILURE RETURNED TO CLE. NR 2 ENGINE FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED PER MM 73-11-01/72-60, PERFORMED POWER ASSURANCE RUN MM 71-09-266 PARTS CHG COMPLETE.