Table of Contents
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Hélicoptères Guimbal
CABRI G2
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.
Vent
Cutoff
valve
7-6
Approved under DOA EASA.21J.211
Filler cap
FUEL TANK
Gascolator
Electrical
pump
Drain
Drain
SYSTEMS DESCRIPTIONS
Flow
sender
Pressure sender
Original issue
SECTION 7
Engine
pump
P
S
Issue 10
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