Systems Description
Model G58
Section 7
7-40
and R BAT. Each battery is capable of supplying power to the
entire electrical system if the alternators are inoperative and
the Bus Tie Relay is closed.
Left and Right Alternators - A 100-amp, 28.5-volt, gear-driven
alternator is located on each engine in front of the right forward
cylinder. The alternators are controlled by switches on the
pilot's left subpanel placarded L ALT and R ALT. Each alterna-
tor is capable of supplying power to the entire electrical system
if the opposite alternator is inoperative and the Bus Tie Relay
is closed. Each alternator will generate 100 amps at 2300 RPM
and above. Each alternator is controlled by a solid-state volt-
age regulator which regulates the voltage between 27.5 to
29.0 volts and will automatically turn the alternator off if an
over-voltage condition should occur.
Standby Power for the Standby Attitude Indicator - A sealed
lead acid battery is attached to the back of the standby attitude
indicator. If power is lost to the right bus, (or to the L CB
PANEL BUS powered by the Right Bus) this battery will power
the standby attitude indicator for a minimum of one hour if the
battery is fully charged.
PROTECTIVE DEVICES
The electrical system is protected by current limiters, circuit
breakers, and circuit-breaker-type switches. A row of re-setta-
ble circuit breakers is located below the right subpanel. This
panel contains the majority of the avionics circuit breakers and
thus is referred to as the Avionics Circuit Breaker Panel.
Another group of re-settable circuit breakers is located on the
left side of the cockpit. These are arranged in three rows and
consist primarily of circuit breakers for airplane systems. This
panel is referred to as the Left Circuit Breaker Panel. Circuit-
breaker-type switches are located on the pilot's instrument
sub-panel. A hot battery bus is powered by the Right Battery.
Protection devices for equipment powered by this bus are not
available to the pilot. Current limiters are installed throughout
the system to connect buses together and provide a quick
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Summary of Contents for Baron G58
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Page 66: ...Model G58 2 4 May 2015 Section 2 THIS PAGE INTENTIONALLY LEFT BLANK Limitations ...
Page 138: ...Emergency Procedures Model G58 Section 3 3 30 THIS PAGE INTENTIONALLY LEFT BLANK April 2008 ...
Page 170: ...Model G58 4 4 June 2011 Section 4 Normal Procedures THIS PAGE INTENTIONALLY LEFT BLANK ...
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Page 247: ...Performance Section 5 Model G58 5 23 July 2014 ...
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Page 288: ...Wt and Bal Equip List Model G58 Section 6 6 10 December 2009 ...
Page 289: ...Wt and Bal Equip List Section 6 Model G58 6 11 December 2009 ...
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Page 434: ...Supplements Model G58 Section 9 9 2 THIS PAGE INTENTIONALLY LEFT BLANK November 2005 ...
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