What engine?
An example, covering several CAT (TCM) engines:
"10-12.3. (edited)
The preferred, and most effective method, of priming the lubrication system is using a preoiler
tank (pressure pot). “Engine Pre-oiling” instructions are provided in Section 5-2.9.
Engines are assembled with a small amount of oil on mating surfaces. Crankcase oil
galleries, cylinder walls, the oil pump, oil filter, oil cooler, and hoses contain no oil on a
freshly assembled engine. The starter is not capable of filling all the empty passages in the
engine with oil before ignition. The seconds that pass before oil pressure is developed can
take hours off the life of the engine.
There may be times when an engine pre-oiler tank is not readily available. The following
alternate priming methods may be used."
"5-2.9. Engine Pre-oiling
See also “Lubrication System Priming” in Section 10-12.3.
WARNING
Do not exceed the starter duty cycle to rotate the engine during
engine pre-oiling. Persistent engagement of the starter to rotate
the crankshaft will exceed the starter duty cycle and may result
in premature starter failure.
1. Install and torque the spark plugs and ignition lead wires according to the “Ignition
System Maintenance” instructions in Section 6-4.9.
2. Verify lubrication lines, fittings, hoses, screens, and filters are in place prior to preoiling.
3. Obtain a 1-gallon capacity bladder-type pressure pot with an output pressure of 50
psi (not to exceed 60 psi).
4. Connect the pre-oiler supply hose to the engine oil pressure output (fitting). It may
be necessary to disconnect the aircraft oil pressure sensor fitting according to the
aircraft manufacturer's instructions.
5. Remove the rocker covers.
6. Open the pre-oiler valve and monitor the rocker arms for oil flow. Depending upon
oil temperature, it may take several minutes to see an indication of oil flow.
7. Close the pre-oiler valve upon verification of oil flow at the rocker arms.
8. Install the rocker covers with new gaskets according to the “Cylinder Installation”
instructions in the primary ICA (Section 1-1.1). Torque the rocker cover fasteners to
Appendix B specifications.
9. Disconnect the pre-oiler supply hose and cap; connect the aircraft oil pressure sensor
to the engine oil pressure output according to the aircraft manufacturer's
instructions."