For those of you who are looking for Jabiru 5100 Aircraft Engine Installation Manual and Product Specification, you can download it via the link below. In the manual there is important information you should know in order to maximize the use of Jabiru 5100 and gain all the benefits it has. Within Jabiru 5100 Aircraft Engine Installation Manual there is also an illustration of the Jabiru 5100 Aircraft Engine that allows you to study and recognize shapes and parts of this machine.
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Ratings
RPM – Maximum (Redline):..................................... 3000 RPM
RPM – Maximum Continuous: ................................. 3000 RPM
RPM – Recommended Cruise:................................ 2750 RPM – 3000 RPM
Power Rating: .......................................................... 180 hp / 3000 RPM
Fuel
Fuel Pressure to Carburettor Maximum .................. 20 kPa (3 psi)
Fuel Pressure to Carburettor Minimum ................... 10 kPa (1.5 psi)
Recommended Fuel Grade ..................................... Avgas 100LL & Avgas 100/130
Note: Leaded and Unleaded Automotive Gasoline above 100 Octane RON may be used, however due to the lack of a strong quality control system for automotive fuels Jabiru Aircraft recommend using AVGAS wherever possible.
Oil
Oil Capacity.............................................................. 5.5 Litres
Oil – Minimum Temperature for Take-Off................ 50°C (122°F)
Oil – Maximum Peak Oil Temperature .................... 118°C (244°F)
Oil – Maximum Continuous Oil Temperature .......... 80°C – 100°C (176°F - 212°F)
Oil Pressure – Normal Operations........................... Min 220 kPa (32 psi)
........................... Max 525 kPa (76 psi)
Oil Pressure – Idle ................................................... Min 80 kPa (12 psi)
Oil Pressure – Starting & Warm Up......................... Max 525 kPa (76 psi)
Oil Consumption ...................................................... 0.1 L/hr (max)
Oil Standard............................................................. Aero Oil W Multigrade 15W-50, or equivalent complying with
............................................................ MIL-L-22851C, or
............................................................ Lycoming Spec. 301F, or
............................................................ Teledyne - Continental Spec MHF-24B
Additives
Note: No Oil or fuel additives should be used. Use of oil or fuel additives will void warranty.
Cylinder Head Temperature (CHT)
Maximum Peak Cylinder Head Temperature1 ......... 200ºC (392°F)
Maximum Continuous Temperature ........................ 180ºC (356°F)
Note: Time with CHT at between 180°C and 200°C is not to exceed 5 Minutes
Exhaust Gas Temperature (EGT)
EGT (Mid-Range / Cruise): ...................................... Min 680° - 720°C (1256° - 1328°F)
EGT (Above 70% Power): ....................................... Min 640° - 680°C (1184° - 1256°F)
Note: An EGT gauge is not included as standard equipment on the Jabiru 2200 engine, though a system can be supplied as an option.
Ground Running Limitations
Ground Idle Speed................................................... 900 RPM (set while engine is hot)
Ground Oil Pressure – Idle / Startup........................ Min 80 kPa (11 psi)
........................ Max 525 kPa (76 psi)
Ground Oil Temperature.......................................... Max. 100°C (212°F)
Ground Maximum Cylinder Head Temperature....... 180°C (356°F)
Note: If ground temperature limits are reached, shut the engine down or cool it by pointing the aircraft into wind.
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