Cirrus SR22T User Manual

2-10 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
Center of Gravity Limits
Reference Datum ....................................100 inches forward of firewall
Forward....................................................................Refer to Figure 2-1
Aft ............................................................................Refer to Figure 2-1
Figure 2-1
CG Envelope
2000
2200
2400
2600
2800
3000
3200
3400
3600
C.G. - Inches Aft of Datum
Weight - Pounds
12.5% MAC
FS 139.1
2700 lb
9.8% MAC
FS 137.8
2100 lb
31.5% MAC
FS 148.2
2100 lb
21.1% MAC
FS 143.2
3600 lb
31.5% MAC
FS 148.2
3600 lb
Max Zero Fuel
138136 140 142 144 146 148 150
SR22_FM02_3216
FORWARD LIMIT - The forward limit is FS 137.8 (9.8% MAC) at 2100 lb, with straight line taper
to FS 139.1 (12.5% MAC) at 2700 lb, to FS 143.2 (21.1% MAC) at 3600 lb.
AFT LIMIT - The aft limit is FS 148.2 (31.5% MAC) at all weights from 2100 lb to 3600 lb.
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