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Jabiru Aircraft
Pty Ptd
Installation Manual
Jabiru 2200 Aircraft Engine
REVISION
0 1 2
Dated : March 2006
Page:
7
\\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
4
Operating Limitations
4.1 RPM
Continuous
:
3300 RPM / Full Throttle
Recommended Cruise:
2750 RPM – 3100 RPM
4.2 Engine
Cooling
Maximum Cylinder Head Temperatures measured under exhaust spark plug.
Maximum Peak Temperature
200ºC (392
°
F)
Continuous Operation
180ºC (356
°
F)
4.3 Fuel
4.3.1 Specifications
•
Avgas 100LL & Avgas 100/130
•
Leaded and Unleaded Automotive Gasoline above 95 Octane RON
4.4
Pressure to Carburettor (above ambient)
•
Maximum
20 kPa (3 psi)
•
Minimum
5 kPa (0.75 psi)
WARNING – When using auto fuels, ensure all components of the fuel delivery system
are cooled to prevent fuel vaporization.
4.5 Oil
4.5.1 Specifications
Aero Oil W Multigrade 15W-50,
or equivalent Lubricant complying with
MIL-L-22851C,
or
Lycoming Spec. 301F, or
Teledyne - Continental Spec MHF-24B
4.5.2
Oil Temperature
•
Minimum for Take-off Power
50
°
C (122
°
F)
•
Maximum
118
°
C (244
°
F)
•
Continuous
80
°
C – 100
°
C (176
°
F - 212
°
F)