Cirrus SR22T User Manual

2-28 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
Figure 2-7
(Sheet 5 of 6)
Instrument Panel, center:
DISPLAY
BACKUP
GRAB HERE
Bolster Panel, both sides:
ELT LOCATED BEHIND BULKHEAD
REMOVE CARPET AND ACCESS PANEL
Baggage Compartment, aft edge:
F
I
R
E
E
X
T
I
N
G
U
I
S
H E
R
F
O
R
W
A
R
D
L
E F
T
O
F
P
I
L
O
T
S
E A T
FASTEN SEATBELTS • NO SMOKING
Instrument Panel:
EMERGENCY EXIT
REMOVE EGRESS HAMMER FROM WITHIN
CENTER ARMREST LID. STRIKE CORNER OF
WINDOW. KICK OR PUSH OUT AFTER FRACTURING
Cabin Window, above door latch:
DISTRIBUTED FLOOR LIMIT 130 LBS
BAGGAGE STRAP CAPACITY IS 35 LBS EACH MAXIMUM
SEE AIRPLANE FLIGHT MANUAL FOR BAGGAGE TIE-DOWN
AND WEIGHT AND BALANCE INFORMATION
Baggage Compartment Door, inside:
SR22_FM02_2684
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