Cirrus SR22T User Manual

P/N 13772-143 1 of 6
Cirrus Design Section 9
SR22 / SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
14 Code of Federal Regulations (CFR) Part 135
Commercial Operation of Small Aircraft
Electrical Loading Shedding Procedure
This supplement provides the necessary guidance for load shed in the
event of a primary electrical generating source failure in accordance
with 14 CFR Section 135.163(f).
When the aircraft is being operated under the provisions 14 CFR 135,
this Supplement is applicable and must be inserted in the
Supplements Section of the Pilot's Operating Handbook. Information
in this Supplement adds to, supersedes, or deletes information in the
basic handbook.
• Note •
This POH Supplement Change, dated Revision 02: 01-06-10,
supersedes and replaces the Revision 01 release of this POH
Supplement dated 03-26-09.
Revision 02: 01-06-10

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