Jabiru Aircraft
Pilot Operating Handbook
Model J230-D
JP-FM-09
Revision:
0
12 April 2007
Page 22
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Minimum System Voltage (Bottom of green arc)
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Maximum System Voltage (top of green arc)
Note
The display of these limitations are required for the aircraft’s certification, and it does not
comply with the certification basis if these limits are missing or modified.
3.10
POWER GENERATION SYSTEM LIMITATIONS
When the engine is turning at approximately 2000 RPM and above the alternator produces
sufficient power for all lights to be run continuously. However, below this RPM the alternator
cannot produce this power output and power must be drawn from the battery if all electrical
systems are running. To reduce the load on the alternator, Jabiru Aircraft recommend only using
the Landing Light for takeoff and landing – turning it off during normal cruise operations and
wherever safe while taxiing.
3.11
OTHER LIMITATIONS
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Smoking is prohibited.
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In-cabin noise levels exceed 95db. Hearing protection must be worn.
3.12
PLACARDS
The following placards are required, and are to be located in the proximity indicated.
3.12.1
Cockpit Placards General
Warning Placard
P/No. 5A076A0D
Fitted on the rear Face of the Forward Wing Spar Carry-through Beam
in the Cabin Ceiling.
EMS Warning
P/No. 5A042B0D
Fit to instrument panel above EMS
Engine Limits
P/No. 5A079B0D
Fit to instrument panel.
