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Jabiru Aircraft
Pty Ltd
Instruction & Maintenance Manual
Jabiru 2200 Aircraft Engine
Hydraulic Valve Lifter Models
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REVISION
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Dated : June 2010
Issued By: DPS
Page: 12 of 116
L:\files\Manuals_For_Products\Engine_Manuals\Transition\JEM2204-9_I&M_unsigned.docx
Battery independent
-
Ignition Timing
:
25
o
BTDC
-
Firing Order
:
1
– 3 – 2 – 4
-
DC Output
:
10 Amps up to engine S/No. 22A-2661
17 Amps engine S/No. 22A-2661 and 22C-001 onwards
-
Fuel Consumption
@ 75% Power
:
13 l/hr (3.5 US gal/hr)
-
Fuel
:
AVGAS 100/130. MOGAS with RON Octane
Rating 95 or above may be used if AVGAS is
not available.
-
Oil
:
Aero Oil W Multigrade 15W-50, or equivalent
Lubricant complying with MIL-L-22851C, or
Lycoming Spec. 301F, or Teledyne
–
Continental Spec MHF-24B
-
Oil Capacity
:
2.3 L (2.2 quarts)
-
Spark Plugs
:
NGK D9EA
– Automotive
Electrode Gap: 0.55 - 0.6mm (0.022" - 0.024")
-
Generator
:
Jabiru, permanently excited single phase
AC generator with rectifier/regulator
-
Carburettor
:
BING constant depression Type 94/40
-
Air Intake Filter
:
folder paper cartridge type
-
Fuel Filtration
:
0.1 mm (100 Micron) maximum particle size.
-
Fuel Pump
:
Camshaft driven diaphragm type
-
Starting System
:
Electric 12 V / 1.5 kW
-
Oil Filter
:
RYCO Z 386 or equivalent
3.3
Performance
Static sea level ratings under the following conditions:-
International Standard Atmospheric conditions at sea level.
Aircraft service equipment drives unloaded. (Vacuum Pump not fitted)
Full rich fuel/air mixture.
Maximum cylinder head temperature.
Standard Jabiru air filter and cold air.
Standard exhaust muffler.
3.3.1
Engine Ratings
Table 1
– Engine Ratings
Model:
2200C, 2200B
All Other 2200 Models
Maximum Power
60 kW (80 hp) @ 3300 RPM - ISO
STD Conditions
63 kW (85 hp) @ 3300 RPM -
ISO STD Conditions
Note: These apply only to engines meeting the configurations detailed within this manual.
Fuel Consumption
21 L/hr @ Takeoff/Max Continuous Rating
Oil Consumption
0.1 L/hr (max)