Cirrus SR22T User Manual

3A-24 P/N 13772-005
Section 3A Cirrus Design
Abnormal Procedures SR22T
Parking Brake Engaged Annunciation
PAR K BRAKE C au ti on
1. Parking Brake................................................................. RELEASE
2. Monitor CAS for BRAKE TEMP Caution. Stop aircraft and allow
the brakes to cool if necessary.
Amplification
Parking brake is set.
Communications Failure
1. Switches, Controls ............................................................. CHECK
2. Frequency ....................................................................... CHANGE
3. Circuit Breakers........................................................................SET
4. Headset........................................................................... CHANGE
5. Hand Held Microphone ................................................. CONNECT
Amplification
If, after following the checklist procedure, communication is not
restored, proceed with FAR/AIM lost communications procedures.
• Note •
In the event of an audio panel power failure the audio panel
connects COM 1 to the pilot’s headset and speakers. Setting
the audio panel ‘Off’ will also connect COM 1 to the pilot’s
headsets and speakers.
PARK BRAKE
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