Cirrus SR22T User Manual

4-14 P/N 13772-005
Section 4 Cirrus Design
Normal Procedures SR22T
19. Navigation Lights.................................................... AS REQUIRED
20. Landing Light ......................................................... AS REQUIRED
21. Magnetos ....................................................CHECK Left and Right
RPM drop must not exceed 150 RPM for either magneto. RPM
differential must not exceed 75 RPM between magnetos
a. Ignition Switch ................................. R, note RPM, then BOTH
b. Ignition Switch .................................. L, note RPM, then BOTH
22. Engine Parameters ............................................................ CHECK
23. Power Lever ...................................................................1000 RPM
24. Flight Instruments, HSI, and Altimeter ....................CHECK & SET
25. Flight Controls................................................. FREE & CORRECT
26. Trim ............................................................................. SET Takeoff
27. Autopilot .................................................................. DISCONNECT
Amplification
• WARNING •
Do not takeoff with frost, ice, snow, or other contamination on
the fuselage, wing, stabilizers, and control surfaces.
• Caution •
Because this aircraft has a turbocharged system that
maintains 36.0 in.Hg manifold pressure for all takeoffs, the
mixture should be full rich for takeoff, even at high elevation
airports. Leaning for takeoff and during maximum
performance climb may cause excessive cylinder head
temperatures.
During cold weather operations, the engine should be properly
warmed up before takeoff. In most cases this is accomplished when
the oil temperature has reached at least 100°F (38°C). In warm or hot
weather, precautions should be taken to avoid overheating during
prolonged ground engine operation. Additionally, long periods of idling
may cause fouled spark plugs.
Pitot Heat should be turned ON for flight into IMC, flight into visible
moisture, or whenever ambient temperatures are 41° F (5° C) or less.
During the Magneto Check, if there is a doubt concerning operation of
the ignition system, RPM checks at higher engine speeds will usually
confirm whether a deficiency exists. An absence of RPM drop may
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