Cirrus SR22T User Manual

Cirrus Design Section 3
SR22T Emergency Procedures
P/N 13772-005 3-11P/N 13772-005 3-11
Above 18,000 Feet
The manifold pressure should be maintained at or above 15 in.Hg
(bottom of the green arc on the manifold pressure gage) when the
aircraft is operating above 18,000 feet. If the manifold pressure is
reduced below 15 in.Hg and the Power Lever positioned close to or at
idle, the engine may cease combustion. Upon advancing the Power
Lever, if the wind milling engine does not immediately regain power,
the following procedure should be used:
1. Electric Fuel Pump.................................................... LOW BOOST
2. Power Lever ......................................................................½ OPEN
3. Mixture Control ....FULL RICH, then LEAN until engine starts then
slowly advance to FULL RICH
4. Power Lever ........................................................... AS REQUIRED
5. Mixture ................................................................... AS REQUIRED
6. Electric Fuel Pump................................................. AS REQUIRED
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