Hélicoptères Guimbal
SECTION 7
CABRI G2
SYSTEMS DESCRIPTIONS
7-6
Approved under DOA EASA.21J.211
Cooling system
The engine is air-cooled, with an additional oil cooler.
Cooling air enters the upper cowling plenum around the mast and
gearbox. It is forced by a squirrel-cage blower, directly driven by the
engine.
Warm air is exhausted below the engine.
Fuel system
The fuel system comprises :
•
a single, crash-resistant fuel tank,
•
an submersed electric booster pump,
•
the engine-driven pump,
•
a shut-down valve,
•
a gascolator.
FUEL TANK
Filler cap
Electrical
pump
Cutoff
valve
Vent
Engine
pump
Pressure sender
Gascolator
Flow
sender
Drain
P
Drain
S