Cirrus DESIGN SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-003 2-15
Navigation & Pitot Static
Airspeed Indicator 1 1 1 1
Altimeter 1 1 1 1
Magnetic Compass 1 1 1 1
Pitot System 1 1 1 1
Static System, Normal 1 1 1 1
Attitude Indicator — — 1 1
Clock ——1 1
Gyroscopic Directional Indi-
cation (HSI)
——1 1
Magnetometer — — 1 1
Nav Radio — — 1 1
PFD Airspeed Indication — — 1 1
PFD Altitude Indication — — 1 1
PFD Attitude Indication — — 1 1
PFD Heading Indication — — 1 1
PFD Slip/Skid Indication — — 1 1
Turn Coordinator — — 1 1
Altitude Encoder A/R A/R 1 1 As required per
procedure.
GPS Receiver/Navigator — — A/R A/R As required per
procedure.
Marker Beacon Receiver — — A/R A/R As required per
procedure.
VHF Navigation Radio — — A/R A/R As required per
procedure.
System, Instrument, and/
or Equipment
Kinds of Operation
(Continued)
Remarks, Notes,
and/or
Exceptions
VFR
Day
VFR
Nt.
IFR
Day
IFR
Nt.
Original Issue

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches