Cirrus DESIGN SR22T User Manual

2-10 P/N 13772-003
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
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 142.3 (19.2% MAC at 3400 lb.
AFT LIMIT - The aft limit is FS 148.1 (31.5% MAC) at all weights from 2100 lb to 3400 lb.
2000
2200
2400
2600
2800
3000
3200
3400
3600
136 138 140 142 144 146 148 150
C.G. - Inches Aft of Datum
Weight - Pounds
12 . 5 % M A C
FS 139.1
2700 lb
9.8% M A C
FS 137.8
2100 lb
19 . 2 % M A C
FS 142.3
3400 lb
31.5% M A C
FS 148.1
3400 lb
31.5% M AC
FS 148.1
2100 lb
Original Issue

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