What was found
DURING ENGINE INSPECTION RUN-UP, FOUND NR 1 HYDRAULIC PUMP OPERATING AT 2,200 PSI (SHOULD BE 3,000). REMOVED FAILED PUMP AND INSTALLED REPAIRED UNIT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ENGINE INSPECTION RUN-UP, FOUND NR 1 HYDRAULIC PUMP OPERATING AT 2,200 PSI (SHOULD BE 3,000). REMOVED FAILED PUMP AND INSTALLED REPAIRED UNIT.