Cirrus SR22T User Manual

2 of 10 P/N 13772-148
Section 9 Cirrus Design
Supplements SR22 / SR22T
Section 1 - General
No Change.
Section 2 - Limitations
1. Compliance with the limitations contained in the basic AFM and
approved supplements is mandatory.
2. Foreign operating rules and any references to such rules in the
basic AFM and approved supplements are not applicable in Chile.
3. The aircraft must be equipped and operated in accordance with
the applicable Chilean operating requirements.
4. The use of GPS is not authorized for precision approach and
landing in Chile.
5. Pilot Performed Preventative Maintenance as defined in Section 8,
Handling, Servicing, and Maintenance is not applicable when
operating under Dirección General de Aeronáutica Civil de Chile
Regulations (DGAC).
Original Issue: Oct 04, 2012

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