Cirrus SR22T User Manual

Cirrus Design Section 3A
SR22T Abnormal Procedures
P/N 13772-005 3A-11P/N 13772-005 3A-11
Fuel Imbalance
FUEL IMBALANCE Caution
1. Fuel Quantity Gages.......................................................... CHECK
2. Fuel Pump ......................................................................... BOOST
If HIGH BOOST already in use for vapor suppression, pump
should be left in this position for tank switch.
3. Fuel Selector.......................................... SELECT FULLEST TANK
4. Fuel Pump ............................................................. AS REQUIRED
After switching tanks, message will remain until sensed
imbalance is less than 10 gallons.
Amplification
Fuel level imbalance (between left and right) is greater than 10
gallons.
FUEL IMBALANCE Advisory
1. Fuel Quantity Gages.......................................................... CHECK
2. Fuel Pump ......................................................................... BOOST
If HIGH BOOST already in use for vapor suppression, pump
should be left in this position for tank switch.
3. Fuel Selector.......................................... SELECT FULLEST TANK
4. Fuel Pump ............................................................. AS REQUIRED
After switching tanks, message will remain until sensed
imbalance is less than 8 gallons.
Amplification
Fuel level imbalance (between left and right) is greater than 8 gallons.
FUEL IMBALANCE
FUEL IMBALANCE
Original Issue

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots