Hélicoptères Guimbal
CABRI G2
Powerplant
Model ..................................................... Textron Lycoming O360-J2A
Type .......................... Four cylinders, horizontally opposed, direct drive,
Displacement .................................................................................. 5,9 L
Power rating (continuous) ............. 108 kW @ 2585 through 2700 RPM
Power rating (5 minutes – Max. 30 kt IAS – AVGAS only) ......................
....................................................... 119 kW @ 2585 through 2700 rpm
Nominal speed ....................................................................... 2650 RPM
Cooling system ............................... Direct drive squirrel-cage blower
Ignition systems
Magneto ...................................................................................... Bendix
Electronic ignition system.......................................... LSE Plasma II HG
Fuel
Maximum fuel capacity .................................................................. 170 L
Unusable fuel .................................................................................. 1.5 L
Approved types
AVGAS 100 LL ...........................................................Unrestricted
AVGAS UL 91 .............................................................Unrestricted
Alternate types
Automotive unleaded gasoline..................... Refer to Limitations
Note1 : All these types are mixable, in any proportion. Limitation apply
as soon as a portion of alternate type is in the tank.
Note 2: To use unleaded fuel during run-in, see oil run-in additive in the
Limitation Section.
1-4
Approved under DOA EASA.21J.211
with STC EASA 10015311, initially EASA.E.S.01001
air cooled, normally-aspirated, carburetor-equipped,
one magneto and one electronic ignition system
Solid-state capacitor discharge ignition system
(See Oil additive for break-in in Limitations section)
SECTION 1
GENERAL
/ STC FAA SE03495NY
(361 cu.in)
(145 hp)
(160 hp)
Variable timing advance
(45 U.S. gal)
(0.4 U.S. gal)
Issue 10
Original issue
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