Cirrus SR22T User Manual

Cirrus Design Section 7
SR22T Systems Description
P/N 13772-005 7-29P/N 13772-005 7-29
Front Seat Inflatable Restraints
An inflatable shoulder harness is integral to each front seat harness.
The electronic module assembly, mounted below the cabin floor,
contains a crash sensor, battery, and related circuitry to monitor the
deceleration rate of the airplane. In the event of a crash, the sensor
evaluates the crash pulse and sends a signal to an inflator assembly
mounted to the aft seat frame. This signal releases the gas in the
inflator and rapidly inflates the airbag within the shoulder harness
cover, After airbag deployment, the airbag deflates to enable the pilot/
co-pilot to egress the airplane without obstruction.
The crash sensor’s predetermined deployment threshold does not
allow inadvertent deployment during normal operations, such as hard
landings, strikes on the seat, or random vibration.
• Caution •
No slack may exist between the occupant’s shoulder and
restraint harness shoulder strap.
Stow the seat belts in the latched position when not in use.
To use the restraints:
1. Slip arms behind the harness so that the harness extends over
shoulders.
2. Hold the buckle and firmly insert the link.
3. Grasp the seat belt tabs outboard of the link and buckle and pull to
tighten. Buckle should be centered over hips for maximum comfort
and safety.
4. Restraint harnesses should fit snug against the shoulder with the
lap buckle centered and tightened around the hips.
To release the restraints:
1. Grasp the top of the buckle opposite the link and pull outward. The
link will slip free of buckle.
2. Slip arms from behind the harness.
Child Restraint System
The aircraft is equipped with provisions for installing two LATCH
compliant child seats in the outboard rear seat positions, OR one non-
LATCH compliant seat in the center rear seat position.
Lower anchors for the LATCH compliant seats are located in the
outboard seat positions. The non-LATCH compliant seat must be
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