Cirrus SR22T User Manual

P/N 13772-148 9 of 10
Cirrus Design Section 9
SR22 / SR22T Supplements
Section 3 - Emergency Procedures
No Change.
Section 3A - Abnormal Procedures
No Change.
Section 4 - Normal Procedures
Noise Characteristics/Abatement
Serials 22T-0001 and subsequent: The certificated noise levels for the
aircraft established in accordance with ICAO Annex 16, Volume I are:
Section 5 - Performance Data
No Change.
Section 6 – Weight and Balance
No Change.
Section 7 – Airplane and Systems Description
No Change.
Section 8 – Handling, Service, & Maintenance
No Change.
Section 9 – Supplements
This supplement is required for aircraft operation under Dirección
General de Aeronáutica Civil de Chile (DGAC) Requirements.
Section 10 – Safety Information
No Change.
Configuration Actual Maximum Allowable
Hartzell 3-blade Propeller
PHC-J3Y1F-1N/N7605(B)
81.30 dB(A) 85.00 dB(A)
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