Cirrus SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-29P/N 13772-005 2-29
Figure 2-8
(Sheet 6 of 6)
DO NOT JERK HANDLE
ACTIVATION PROCEDURE
CIRRUS AIRFRAME PARACHUTE SYSTEM
IN INJURY OR DEATH
USE OF THIS DEVICE COULD RESULT
140 KIAS
BOTH HANDS, MAXIMUM FORCE, STEADY PULL
MAXIMUM DEMONSTRATED DEPLOYMENT SPEED
MUST BE WORN AT ALL TIMES
SEAT BELT AND SHOULDER HARNESS
USE FOR EXTREME EMERGENCIES ONLY
!
WARNING
3. FUEL MIXTURE.................... CUT-OFF
6. RESTRAINT SYSTEM............SECURE
5. MASTER SWITCH..........................OFF
4. FUEL SELECTOR HANDLE...........OFF
2. ACTIVATION HANDLE....PULL STRAIGHT DOWN
1. THIS COVER............................................REMOVE
CAPS Deployment Handle Cover, above pilot's right shoulder:
SR22_FM02_3567
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