Cirrus SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-25P/N 13772-005 2-25
Figure 2-4
Placards (Sheet 2 of 6)
NO PUSH
Wing, adjacent to fluid filler cap:
OPEN
TO
PUSH
USE ONLY AL-5 (DTD-406B) FLUID
4.0 US GALLONS (15.1 LITERS)
TOTAL USABLE CAPACITY
TKS ICE PROTECTION FLUID
EXTERNAL
POWER
28 V DC
Left fuselage, on external power supply door:
Serials w/ Ice Protection.
Elevator and Rudder, both sides:
SR22_FM02_3568
Doors, above and below latch:
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