Cirrus SR22T User Manual

3-18 P/N 13772-005
Section 3 Cirrus Design
Emergency Procedures SR22T
Forced Landing
Emergency Landing Without Engine Power
1. Best Glide Speed ........................................................ ESTABLISH
2. Radio............................................. Tra nsm it (12 1.5 MHz ) MAYDAY
giving location and intentions
3. Tran sponder ........................................................... SQUAWK 7700
4. If off airport, ELT ........................................................... ACTIVATE
5. Power Lever ............................................................................IDLE
6. Mixture ............................................................................. CUTOFF
7. Fuel Selector............................................................................OFF
8. Ignition Switch..........................................................................OFF
9. Fuel Pump................................................................................OFF
10. Flaps (when landing is assured) ............................................100%
11. Master Switches.......................................................................OFF
12. Seat Belt(s) ................................................................... SECURED
Amplification
If all attempts to restart the engine fail and a forced landing is
imminent, select a suitable field and prepare for the landing. As forced
landings on unprepared surfaces are not recommended, CAPS
activation may be the safest option. Refer to Section 10, Cirrus
Airframe Parachute System (CAPS) for CAPS deployment scenarios
and landing considerations.
When determined that a forced landing is the safest option, a suitable
field should be chosen as early as possible so that maximum time will
be available to plan and execute the forced landing. While gliding, be
aware that use of flaps will reduce glide distance. Flaps should not be
selected until landing is assured. Land on the main gear and hold the
nose wheel off the ground as long as possible.
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