What was found
MANIFOLD PRESSURE FOLLOWED PROPELLER PITCH ADJUSTMENT, MAXIMUM PRESSURE OK ON TAKEOFF, BUT DID NOT MAINTAIN CONSTANT MP IN-FLIGHT. FOUND DIFFERENTIAL PRESSURE CONTROLLER TO BE INOPERATIVE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MANIFOLD PRESSURE FOLLOWED PROPELLER PITCH ADJUSTMENT, MAXIMUM PRESSURE OK ON TAKEOFF, BUT DID NOT MAINTAIN CONSTANT MP IN-FLIGHT. FOUND DIFFERENTIAL PRESSURE CONTROLLER TO BE INOPERATIVE.