Lycoming TEO-540-C1A Maintenance Manual page 220

(3) Connect a calibrated oil pressure gauge (0 to 100 psi) (0 to 689 kPa) to the appropriate
engine oil pressure port on the test plate for your governor location. Install a plug in the
propeller circuit and unused engine oil pressure circuit port.
(4) Start and warm-up the engine until the oil temperature is within the correct operating
range (Appendix A of the TEO-540-C1A Engine Installation and Operation Manual.)
NOTICE: The oil pressure must not be more than 5 psi (34 kPa) below the lowest
operating pressure of the operating range when the engine rpm is in the usual
operating range.
(5) With the engine OFF, remove the plug from the propeller circuit port and install a
compression tester (Chapter 72-30) at the propeller circuit fitting on the test plate.
NOTICE: Allow 5 minutes after adjusting the first gauge to 40 psi (276 kPa), for air
pressure to stabilize, before reading the pressure on the second gauge.
(6) Apply shop air to the differential pressure regulator and adjust it to 40 psi (276 kPa) on
the Gauge No. 1 (Figure 102. With the engine at operating temperature, the pressure
reading on the Gauge No. 2 must read 6 to 35 psi (41 to 241 kPa), if the system is
operating correctly.
NO. 1 GAUGE 40 psi (276 kPa)
NO. 2 GAUGE 6 psi to 35 psi (41 to 241 kPa)
(7) Remove the test plate P/N ST-483 and gasket. Discard the gasket.
(8) Install the propeller governor on the engine per the airframe manufacturer's instructions.
72-20
Page 190
Above 35 psi (241 kPa)
Below 6 psi (41 kPa)
Figure 102
Propeller Governor Circuit Testing
TEO-540-C1A Engine Maintenance Manual
TEO-540-C1A Engine Maintenance Manual
ACCEPTABLE
Insufficient front main bearing clearance or
a blockage in the propeller governor circuit
Excessive front main bearing clearance
© 2018 Avco Corporation. All Rights Reserved
November 2018