Jabiru Aircraft
Pty Ptd
Installation Manual
Jabiru 2200 Aircraft Engine
REVISION
0 1 2
Dated : March 2006
Page:
6
\\Gateway\library\files\engine_manuals\2200_engine_manuals\Hydraulic_Lifters\Working copies\HL_Installation_Manual_2200_Rev_0.doc
Print Date: 3/8/2006 1:56:00 PM
3
Specifications
3.1 General
- Displacement
:
2200
cc
-
Bore
: 97.5
mm
-
Stroke
: 74
mm
- Compression Ratio
:
8 :1
-
Direction
of
Rotation
of Prop Shaft
:
Clockwise – Pilot’s view – Tractor Applications
- Ramp Weight
:
61 kg (134 lbs) Complete including Exhaust,
Carburettor, Starter Motor, Alternator & Ignition
System.
- Ignition
Timing
:
25
o
BTDC
- Firing Order
:
1 – 3 – 2 – 4
- DC Output
:
10 Amps
-
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
3.2 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.
3.2.1
Engine Ratings
•
Takeoff/Max Continuous
85 hp / 3300 RPM
•
Fuel Consumption
21 L/hr @ Takeoff/Max Continuous Rating
•
Oil Consumption
0.1 L/hr (max)
