Cirrus DESIGN SR22 User Manual

Cirrus Design Section 2
SR22 Limitations
P/N 13772-002 2-9P/N 13772-002 2-9
Fuel
a
Serials w/ Perspective System software load 0764-02 and later: Dynamically changes based
on engine parameters.
b
Serials 3026 thru 3848.
c
Serials 3849 and subs.
Electrical
d
20 second delay.
e
30 second delay.
Instrument
(Range & Units)
Red
Arc/Bar
Yellow
Arc/Bar
Green
Arc/Bar
Yellow
Arc/Bar
Red
Arc/Bar
Minimum
Minimum
Caution
Range
Normal
Range
Maximum
Caution
Range
Maximum
Fuel Flow
a
(0 – 30 U.S. Gal/Hr)
–– –– 0 – 30 –– ––
Fuel Totalizer
(U.S. Gallon)
N < 9
FUEL
QTY
9 – 18 > 18 –– ––
Fuel Quantity Gage
b
(0 – 46 U.S. Gallon)
0 10 – 14 –– –– ––
Fuel Quantity Gage
c
(0 – 46 U.S. Gallon)
0 10 – 14 14 – 46 –– ––
Instrument
(Range & Units)
Red
Arc/Bar
Yellow
Arc/Bar
Green
Arc/Bar
Yellow
Arc/Bar
Red
Arc/Bar
Minimum
Minimum
Caution
Range
Normal
Range
Maximum
Caution
Range
Maximum
Essential Bus Volts
(0 – 36 Volts)
0 – 24.4
ESS BUS
–– 24.5 – 32 –– > 32
ESS BUS
Main Bus 1 Voltage
(0 – 36 Volts)
–– 0 – 24.4
M BUS 1
24.5 – 32 –– > 32
M BUS 1
Main Bus 2 Voltage
(0 – 36 Volts)
–– 0 – 24.4
M BUS 2
24.5 – 32 –– > 32
M BUS 2
Alternator 1 Current
(0 – 100 Amps)
–– –– 2 – 100
0 – 1
d
ALT 1
––
Alternator 2 Current
(0 – 70 Amps)
–– –– 2 – 100
0 – 1
d
ALT 2
––
Battery 1 Current
(-59 to 59 Amps)
–– –– -4 – 59
-59 to -5
e
BATT 1
––
Reissue A

Cirrus DESIGN SR22 Specifications

General

Brand	Cirrus
Model	DESIGN SR22
Category	Aircrafts
Language	English