Cirrus DESIGN SR22T User Manual

P/N 13772-115 9 of 20
Cirrus Design Section 9
SR22 / SR22T Supplements
Section 6 - Weight & Balance
Refer to Section 6 - Weight and Balance of the basic POH for current
weight and balance data. Use the following table to determine the
Moment/1000 for deicing fluid to complete the Loading Form in the
Weight and Balance Section of the basic POH.
Serials before G3 Wing; Total fluid tank capacity is 2.9 gal. (10.9 L).
Serials with G3 Wing: Total fluid tank capacity is 3.5 gallons (13.2 L).
Deicing fluid weight is 9.2 pounds per gallon.
Loading Data - Serials before G3 Wing
Gallons
Weight
LB
Mom/
1000@
Fluid Tank
(FS181.0)
Gallons
Weight
LB
Mom/
1000@
Fluid Tank
(FS181.0)
0.1 0.9 0.17 2.1 19.3 3.50
0.2 1.8 0.33 2.2 20.2 3.66
0.3 2.8 0.50 2.3 21.2 3.83
0.4 3.7 0.67 2.4 22.1 4.00
0.5 4.6 0.83 2.5 23.0 4.16
0.6 5.5 1.00 2.6 23.9 4.33
0.7 6.4 1.17 2.7 24.8 4.50
0.8 7.4 1.33 2.8 25.8 4.66
0.9 8.3 1.50 2.9* 26.7 4.83
1.0 9.2 1.67
*2.9 gallon (10.9 L) Capacity.
1.1 10.1 1.83
1.2 11.0 2.00
1.3 12.0 2.16
1.4 12.9 2.33
1.5 13.8 2.50
1.6 14.7 2.66
1.7 15.6 2.83
1.8 16.6 3.00
1.9 17.5 3.16
2.0 18.4 3.33
Revision 09: 12-17-10

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches