Cirrus SR22T User Manual

7-46 P/N 13772-005
Section 7 Cirrus Design
Systems Description SR22T
Figure 7-9
Fuel System Controls and Indicating
3
Density Alt 8000 Ft
Oat 31°F -1°C (ISA +0°C)
2
4
1
Fuel System Indication
LEGEND
1. Fuel Flow Gage
2. Fuel Calculations:
·Fuel At Destination (Totalizer)
·Fuel Used (Totalizer)
·Fuel Remaining (Totalizer)
·Time Remaining (Totalizer)
·Fuel Range (Totalizer)
·Nautical Miles Per Gallon (Totalizer)
3. Fuel Quantity Gage (Float Sensor)
4. Fuel Pump Switch
5. Fuel Selector Valve
5
Engine Controls
SR22_FM07_3516
Serials 0311 thru 0314, 0316 thru 0317,
0319 & subs.
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