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electrical data block located in the mid-right section of the MFD. The
MFD and PFD receive the amp signals via the DAU as derived from
current transducers located in the MCU.
In the event Alternator 1 or Alternator 2 ampere output is less than 2
amps for 20 seconds or more, the MFD will display “Check ALT 1” or
“Check ALT 2” respectively, in a yellow advisory box in the lower right
corner of the MFD.
28 VDC for the digital instrument operation is supplied through the 2-
amp ANNUN / ENGINE INST circuit breaker on the Essential Bus.
June 2007
Information Manual 7-71
Cirrus Design Section 7
SR22 Airplane Description
Ammeter Select Switch
Serials 0002 through 1601, 1603 through 1643 and 1645 through
1662: The AMMETER SELECT switch on the instrument panel is used
to select the desired source of electrical current flow to be indicated on
the ammeter. The switch has three positions: ALT 1, BATT, and ALT 2.
The BATT position indicates BAT 1 current flow only. Selecting one of
the switch positions will cause the amperage output from that device to
be displayed on the ammeter.
Serials 1602, 1644, 1663 and subsequent: Main and Essential Bus
voltages are displayed on the MFD and PFD, therefore, no ammeter
select switch is necessary.
Low-Volts Warning Light
The airplane is equipped with a red LOW VOLTS warning light in the
annunciator panel located on the left side of the instrument panel. A
voltage sensor in the (MCU) monitors voltage on the Essential Bus
and illuminates the warning light when the voltage is less than
approximately 24.5 volts.
• Note •
The LOW VOLTS warning light may come on during extended
low RPM operation with heavy electrical loads. Under these
conditions, the light will go out at higher RPM.
ALT Fail Caution Lights
Two ALT Fail caution lights are installed in the annunciator panel. The
ALT 1 and ALT 2 caution lights in the annunciator panel provide
annunciation of alternator failure or overcurrent conditions at the
respective alternator. The lights are operated by circuits in the MCU
and current sensors on the ALT 1 and ALT 2 output lines. Steady
illumination of either light indicates an alternator failure. Serials 0002
through 1601, 1603 through 1643 and 1645 through 1662: A flashing
ALT light indicates an overcurrent condition.
June 2007
7-72 Information Manual
Section 7 Cirrus Design
Airplane Description SR22
Circuit Breakers and Fuses
Individual electrical circuits connected to the Main, Essential, and
Non-Essential Buses in the airplane are protected by re-settable circuit
breakers mounted in the circuit breaker panel on the left side of the
center console.
Essential Buses
The circuit breaker panel Essential Bus is powered by ALT 2 from the
MCU Essential Distribution Bus through the 20-amp ESSENTIAL
POWER circuit breaker and from BAT 2 through the 20-amp BATTERY
2 circuit breaker. The Essential Bus is also powered by ALT 1 and BAT-
1 through an isolation diode connecting the Main and Essential
Distribution Buses in the MCU. The autopilot and Essential avionics
equipment are powered directly from the Essential Distribution Bus in
the MCU through a 25-amp circuit breaker on the Distribution Bus.
Power from the 15-amp AVIONICS circuit breaker is also controlled
through the AVIONICS master switch on the bolster switch panel.
Main Buses
The circuit breaker panel Main Bus 1 and Main Bus 2 are powered by
ALT 1 and BAT 1 from the MCU Main Distribution Bus through 25-amp
circuit breakers on the Distribution Bus. ALT 2 and BAT 2 are
prevented from powering the Main Buses by the isolation diode
interconnecting the MCU distribution buses. Loads on circuit breaker
panel Main Buses are shed by pulling the individual circuit breakers.
The 15-amp AVIONICS circuit breaker on Main Bus 1 powers all loads
on the Non-Essential Avionics Bus. Power from the 15-amp AVIONICS
circuit breaker is also controlled through the AVIONICS master switch
on the bolster switch panel.
Non-Essential Buses
The circuit breaker panel contains two Non-Essential Buses, the Non-
Essential Equipment Bus and the Avionics Non-Essential Bus. The
Avionics Non-Essential Bus is powered through the 15-amp
AVIONICS circuit breaker on Main Bus 1 and is discussed above. The
Non-Essential Equipment Bus is powered by ALT 1 and BAT 1 from
the MCU Main Distribution Bus through a 25-amp circuit breaker. ALT
2 and BAT 2 are prevented from powering the Non-Essential
Equipment Bus by the isolation diode interconnecting the MCU
June 2007
Information Manual 7-73
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(75)
