Cirrus SR22T User Manual

7-28 P/N 13772-005
Section 7 Cirrus Design
Systems Description SR22T
forward from the baggage compartment. Recline position is controlled
through a lever located on either side of the seat.
To fold seat ba ck forward:
1. With no pressure on the seat back, rotate the lever to the recline
position and fold the seat back forward.
Seat Belt and Shoulder Harness
Integrated seat belt and shoulder harness assemblies with inertia
reels are provided for the pilot and each passenger.
The front seats use a 4-point inflatable restraint system. Forward seat
belts are attached to the seat frame. The shoulder harnesses are
attached to inertia reels mounted in the seat back.
The rear seats use a 3-point safety harness consisting of one shoulder
harness and a lap belt. The rear seat belts are attached to fittings on
the cabin floor. The shoulder harnesses are attached to inertia reels
mounted to the baggage compartment rear bulkhead.
Each front and rear seat shoulder harness is attached to the seat belt.
The inertia reels allow complete freedom of movement of the
occupant’s upper torso. In the event of a sudden deceleration, the
reels lock automatically to protect the occupants. It is recommended
that the seat belts be stowed in the latched position when not in use.
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