Jabiru Aircraft
Pty Ptd
Aircraft Service Manual
Jabiru J230-C
REVISION
0
Dated : Feb 2006
Issued By: RAS
Page: 147 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
14
SECTION 14 – ELECTRICAL SYSTEMS
14.1 ELECTRICAL POWER SUPPLY SYSTEM
Electrical energy for the aircraft is supplied by a 12 volt, direct-current, single-wire,
negative ground electrical system. A 12-volt battery supplies power for starting and
furnishes a reserve source of power in the event of electrical power system failure. An
engine-driven Alternator is the normal source of power during flight and maintains a
battery charge controlled by a voltage regulator.
The following paragraphs provide brief descriptions of the elements of the electrical
system. They should be read in conjunction with the Wiring Diagram in Figures 59 and
60.
14.2 WIRING DIAGRAM
The Wiring Diagram is shown in Figures 59 and 60.
