Eurocopter AS 350 83 Flight Manual page 242

COMPLEMENTARY FLIGHT MANUAL
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2 LUBRICATION SYSTEM
The engine includes a self-contained lubrication system with an external
oil cooling system and oil tank.
Oil system monitoring is ensured by oil teR1>erature and pressure
indicators located on the VEMD bottom screen.
In addition, the Warning-Caution-Advisory Panel includes
lights that illuminate to indicate:
-minimtnn oil pressure
-metal particles on the magnetic chip detectors.
KEY TO FIGURE OIL SYSTEM ,8
~ DESCRIPTION ~ DESCRIPTI(Jj
1 Oil tank B Pressure relief valve
2 Oil teR1>erature indicator 9 Pressurizing puR1>
3 Oil cooler 10 Heat exchanger
4 Chip detection light 11 Oil filter
S Non-return valve 12 Bypass valve
6 Scavenge PImPS 13 Clogging indicator
7 Suction filter 14 Dil pressure indicator
15 MininIJm oil pressure light
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