ORLI
Č
AN M-8 EAGLE
PILOT'S OPERATING
REVISION NO. 05
DATE OF ISSUE: MAY 02,
GENERAL INFORMATION
PAGE
OF
20
25
1.
POWERPLANT
Rotax 912 ULS 2 engine is providing excellent dynamic and flight characteristics. Rotax 912 ULS 2
engine is four- stroke, four-cylinder engine of “boxer” configuration, having air-cooled cylinders with
water-cooled heads, an integrated reduction gearbox, and two carburetors with dual electronic ignition.
For more information, see the ROTAX engine operating manual supplied.
SWEPT VOLUME:
82,5 in
3
(1352 cm
3
)
TAKE-OFF
POWER, MAX.:
73.5 kW / 5800 rpm
CRUISING
POWER, MAX.:
69.0 kW / 5500 rpm
DRY WEIGHT:
128,5 lb (58,3 kg)
FUEL (FUEL
GRADE, OCTANE
INDEX):
automotive pump fuel
min. RON 95 / min. AKI 91
OIL (TYPE):
Only oil with RON 424 classification. At the selection of suitable
lubricants refer to the additional information in the Service Information
SI-912-016, latest edition.
OIL CAPACITY:
0,793 U.S. gal (3 l) without oil cooler and lines
REDUCTION GEAR
(GEAR RATIO):
2.43 : 1
FUEL TANK
VOLUME:
26,41 U.S. gal (100 l)
WARNING!
NEITHER OF THE ENGINES MENTIONED ABOVE IS CERTIFIED AS AN AIRCRAFT
ENGINE. EVEN WITH UTMOST ATTENTION DURING ENGINE MANUFACTURE,
ENGINE FAILURE MAY OCCUR AT ANY TIME DURING FLIGHT AND THE PILOT
BEARS FULL RESPONSIBILITY FOR THE CONSEQUENCES. ACCORDING TO LIGHT
SPORTS AND ULTRALIGHT REGULATIONS, THE PILOT MUST ALWAYS SELECT
BEARING AND ALTITUDE ALLOWING HIM/HER TO GLIDE DOWN AND LAND SAFELY
AT SUITABLE LOCATION.
Summary of Contents for M-8 EAGLE 2022
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