Cirrus SR22T User Manual

Cirrus Design Section 7
SR22T Systems Description
P/N 13772-005 7-43P/N 13772-005 7-43
Fuel Indicating
Fuel quantity is measured by float-type quantity sensors installed in
each fuel tank and displayed on the Fuel Quantity Gage.
• Caution •
When the fuel tanks are 1/4 full or less, prolonged
uncoordinated flight such as slips or skids can uncover the
fuel tank outlets. Therefore, if operating with one fuel tank dry
or if operating on LEFT or RIGHT tank when 1/4 full or less, do
not allow the airplane to remain in uncoordinated flight for
periods in excess of 30 seconds.
• Note •
A “Red X” through any electronic display field indicates that
the display field is not receiving valid data and should be
considered inoperative.
Fuel Quantity Gage
A dual reading fuel quantity gage is displayed on the Engine Strip
along the left edge of the MFD and in the Fuel Qty block of the
ENGINE page. In the case of an electronic display failure (backup
mode), all essential fuel information is displayed on the Engine Strip
along the left edge of the PFD. The LEFT pointer indicates left tank
fuel quantity and sweeps a vertical bar scale marked from 0 to 46 U.S.
gallons in 5-gallon increments. The RIGHT pointer sweeps an identical
scale for the right tank. Each scale is marked with a yellow band from
0 to 14 U.S. gallons and a green band from 14 to 46 U.S. gallons. The
indicators are calibrated to read 0 gallons when no usable fuel
remains.
Fuel quantity is measured by a float type quantity sensors installed in
the fuel tanks. Fluid quantity information is sent to the Engine Airframe
Unit, processed, and transmitted to the simulated Fuel Quantity Gage
and CAS window for display.
Fuel Flow
Fuel Flow is shown in the upper mid right corner of the ENGINE page
as both a simulated gage and as a digital value. The gage pointer
sweeps a scale range from 0 to 45 Gallons Per Hour (GPH). The fuel
flow value is displayed in white numerals below the gage. Fuel flow is
measured by a transducer on the right side of the engine in the fuel
line between the engine driven fuel pump and distribution block. The
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