PILOT’S OPERATING HANDBOOK
Section 7
Airplane and System
Description
2015-07-20
7-11
Doc. No. POH-20101308
Figure 7-2
Scheme of cylinder head cooling system
7.11.3 Engine Lubrication System
Engine lubrication system is performed with the dry crank case. Engine
lubrication system is equipped with oil pump (1) ensuring oil feeding from
reservoir (4) located on the fire wall through the oil cooler (5) and the oil cleaner
(6) to the lubricated points of engine. The pressure sensor (2) is located behind
the oil pump. The oil reservoir is aerated by the hose (7) which is led under the
airplane. Oil pressure and temperature are indicated on Flymap LD’s display. Oil
is replenished through the lid in the upper part of the oil reservoir.
Figure 7-3
Scheme of engine lubrication system
Summary of Contents for SportStar MAX
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