Cirrus SR22T User Manual

Cirrus Design Section 7
SR22T Systems Description
P/N 13772-005 7-45P/N 13772-005 7-45
ENGINE page changes to the corresponding color of CAS alert and
the annunciation system issues an audio alert.
FUEL QTY: Fuel quantity.
• A white Advisory message is generated when either fuel tank
goes below 14 gallons.
•An amber Caution message is generated when both fuel tanks
go below 14 gallons.
•A red Warning message is generated when the fuel totalizer
amount goes below 9 gallons, or if the sensed fuel quantity (left
plus right) is below 9 gallons.
FUEL IMBALANCE: Imbalanced between Left and Right
Tanks.
•A white Advisory message is generated when the imbalance
between tanks is greater than 8 gallons.
•An amber Caution message is generated when the imbalance
between tanks is greater than 10 gallons.
•A red Warning message is generated when the imbalance
between tanks is greater than 12 gallons.
• Note •
For specific pilot actions in response to Fuel System
Annunciations, refer to Section 3 - Emergency Procedures,
Fuel System Emergencies, and Section 3A - Abnormal
Procedures, Fuel System.
For additional information on Engine Instrument Markings and
Annunciations, refer to Section 2: Limitations.
For additional information on the System Annunciations And
Alerts, refer to the Perspective Integrated Avionics System
description in this section.
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