Jabiru Aircraft
Pty Ptd
Aircraft Service Manual
Jabiru J230-C
REVISION
0
Dated : Feb 2006
Issued By: RAS
Page: 15 of 171
L:\files\Technical_manuals\J230_J430\J230.J430_Work_files\J230-C_Tech_Rev_1.doc
Print Date: 14/01/2009 4:41:00 PM
2.6
TORQUE VALUES
A chart of recommended torque values is shown in Figure 1-2. These torque values are
recommended for all service procedures contained in this manual, except where other
values are stipulated. They are not to be used for checking tightness of installed parts
during service.
2.7
AIRCRAFT SPECIFICATIONS
Table 1. J230 Specifications
Model
J230-C
Aircraft Maximum Weight
600kg
(1320lb)
Fuel Capacity
135 litres
Fuel Type
AVGAS 100/130.
MOGAS with Octane Rating 95 RON (AKI 90) or
above may be used if AVGAS is not available.
Fuels Containing Alcohols (Ethanol etc) will
damage the fuel tank sealant and
MUST NOT BE USED IN JABIRU AIRCRAFT
Oil Capacity
3.5 litres
Oil Type
Refer Engine Manuals
Engine Model
(Refer To Appendix I For Engine Data)
Jabiru 3300
Propeller Type
Jabiru
2-bladed Wooden
Propeller Diameter
60” dia (1524mm)
Propeller Pitch
Jabiru 53” pitch (1346mm)
Wheel Sizes Standard
500 x 6” rim
Tyres Standard
6” wide, 6 Ply
Tyre Pressures Standard - Mains
228 kpa (45 psi)
Tyre Pressures Standard - Nose
193 kpa (30 psi)
Wheel Alignment (At Gross Weight)
Camber
Toe In
0”
0”
Battery Location
In Engine Compartment