Cirrus SR22T User Manual

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Cirrus Design Section 9
SR22 / SR22T Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
SR22 / SR22T Airplanes Registered in
European Union
1. This supplement is required for operation of Cirrus Design SR22
serial numbers 0002 and subsequent and SR22T serial numbers
0001 and subsequent when registered in the European Union.
This supplement must be attached to the applicable SR22 and
SR22T EASA/FAA-approved Airplane Flight Manuals.
2. The information contained within this supplement is to be used in
conjunction with the basic AFM and supplements. The information
contained herein supplements or supersedes that in the basic
manual and approved supplements only in those areas indicated.
3. Compliance with the limitations contained in the basic manual and
approved supplements is mandatory.
4. Foreign operating rules and any references to such rules in the
basic manual and approved supplements are not applicable in the
European Union. The aircraft must be equipped and operated in
accordance with applicable operating requirements.
5. A Kinds of Operating Equipment List (KOEL) may not necessarily
apply in the European Union.
• Note •
This POH Supplement Change, dated Revision 01: 07-07-
2010, supersedes and replaces the Original Issue of this POH
Supplement dated 04-12-06.
Revision 01: 07-07-2010

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