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OIL PRESS
START ENGAGE
March 2010
Cirrus Design Section 3A
SR22 Abnormal Procedures
Information Manual 3A-5
Fuel System
Left Fuel Tank Quantity
L FUEL QTY Advisory
Left fuel quantity is less than or equal to 18 gallons.
1. Left Fuel Quantity Gage..................................................... CHECK
If left fuel quantity indicates less than or equal to 18 gallons:
a. If On-Ground ..............................REFUEL PRIOR TO FLIGHT
b. If In-Flight ........................................... CONTINUE, MONITOR
If left fuel quantity indicates more than 18 gallons:
a. If On-Ground .......................... CORRECT PRIOR TO FLIGHT
b. If In-Flight ........................................... CONTINUE, MONITOR
Right Fuel Tank Quantity
R FUEL QTY Advisory
Right fuel quantity is less than or equal to 18 gallons.
1. Right Fuel Quantity Gage .................................................. CHECK
If right fuel quantity indicates less than or equal to 18 gallons:
a. If On-Ground ..............................REFUEL PRIOR TO FLIGHT
b. If In-Flight ........................................... CONTINUE, MONITOR
If right fuel quantity indicates more than 18 gallons:
a. If On-Ground .......................... CORRECT PRIOR TO FLIGHT
b. If In-Flight ........................................... CONTINUE, MONITOR
L FUEL QTY
R FUEL QTY
March 2010
3A-6 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR22
Fuel System (Cont)
Fuel Filter in Bypass Mode
FUEL FILTER Advisory
The fuel filter is in bypass mode. The fuel filter element must be
replaced.
1. If In-Flight ..................................LAND AS SOON AS PRACTICAL
2. Replace fuel filter element prior to next flight.
Electrical System
Battery 1 Current Sensor
BATT 1 Caution
Battery 1 current is discharging at a rate greater than 4 amps for 30
seconds or more.
1. Land as soon as practical.
FUEL FILTER
BATT 1
March 2010
Cirrus Design Section 3A
SR22 Abnormal Procedures
Information Manual 3A-7
Figure 3A-1
Circuit Breaker Panel
STALL
VANE HEAT
EVS
CAMERA
CABIN AIR
CONTROL
CABIN
FAN
STARTER
AVIONICS
FAN 1
RECOG
LIGHTS
NAV
LIGHTS
STROBE
LIGHTS
PITOT
HEAT
FLAPS
AVIONICS
FAN 2
GPS NAV
GIA 2
COM 2
AHRS 2
FUEL
PUMP
PFD #2
MFD #1
12V DC
OUTLET
YAW
SERVO
ALT1
A/C COND
A/C COMPR
SR22_FM03A_2949A
BAT 2
GPS NAV
GIA 1
COM 1
ADC 1
STDBY
ATTD #1
PFD #1
PITCH
TRIM
ROLL
TRIM
ENGINE
INSTR
ALT2
STALL
WARNING
ESSENTIAL
POWER
AHRS 1
DME / ADF
AUDIO
PANEL
WEATHER
TRAFFIC
AP SERVOS
FUEL QTY
MFD #2
STDBY
ATTD #2
CABIN LIGHTS
/ OXYGEN
KEYPADS
/ AP CTRL
XPONDER
ICE
PROTECTION
AVIONICS
March 2010
3A-8 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR22
Integrated Avionics System
Avionics Switch Off
AVIONICS OFF Caution
The AVIONICS master switch is off.
1. AVIONICS Switch............................................ON, AS REQUIRED
Flight Displays Too Dim
• Note •
Photocell backlighting for the flight displays, bezel, audio
panel, and FMS keyboard is manually controlled through the
dimmer control on the instrument panel bolster. When turned
‘off’ (counter-clockwise), the flight displays automatically
adjust for ambient lighting conditions.
1. INSTRUMENT dimmer knob....................................................OFF
If Flight Displays are not controllable with INSTRUMENT dimmer
knob:
2. CABIN LIGHTS Circuit Breaker .............................................PULL
3. Revert to standby instruments with flashlight for illumination.
PFD Cooling Fan Failure
PFD 1 FAN FAIL Advisory
The cooling fan for the PFD is inoperative.
1. AVIONICS FAN 2 Circuit Breaker........................................CYCLE
If annunciation does not extinguish:
a. Hot cabin temperatures ......LAND AS SOON AS PRACTICAL
b. Cool cabin temperatures .................... CONTINUE, MONITOR
AVIONICS OFF
PFD 1 FAN FAIL
March 2010
Cirrus Design Section 3A
SR22 Abnormal Procedures
Information Manual 3A-9
MFD Cooling Fan Failure
MFD FAN FAIL Advisory
The cooling fan for the MFD is inoperative.
　
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