Cirrus SR22T User Manual

2-18 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
Maximum Occupancy
Occupancy of this airplane is limited to “4+1” persons, the pilot and
four passengers. If carrying three rear seat passengers, occupants
must be wearing a seat belt and shoulder harness with their hips and
back firmly against the seatback as show in the following illustration. If
three rear seat passengers cannot meet these requirements,
occupancy is limited to four persons.
Child Restraint System
1. Rear seat configuration for LATCH / ISOFIX compliant child seats
is limited to two seats in the outboard positions.
2. A single non-LATCH / ISOFIX compliant seat may be installed in
the center seat position.
3. Installation of three child seats in the rear seat is prohibited.
Refer to Section 7, Seats for additional information.
Figure 2-2
Rear Passenger Seat Arrangement
SR22_FM02_3491
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