Cirrus SR22T User Manual

P/N 13772-005 5-1
Cirrus Design Section 5
SR22T Performance Data
Introduction ........................................................................................ 3
Associated Conditions Affecting Performance................................ 3
Demonstrated Operating Temperature........................................... 3
Airspeed Calibration: Normal Static Source....................................... 4
Airspeed Calibration: Alternate Static Source.................................... 5
Altitude Correction
Normal Static Source: Primary Flight Display .................................... 6
Altitude Correction
Normal Static Source: Standby Altimeter........................................... 7
Altitude Correction
Alternate Static Source: Primary Flight Display ................................. 8
Altitude Correction
Alternate Static Source: Standby Altimeter........................................ 9
Temperature Conversion ................................................................. 10
Outside Air Temperature for ISA Condition ..................................... 11
Stall Speeds..................................................................................... 12
Wind Components ........................................................................... 13
Takeoff Distance .............................................................................. 14
Takeoff Distance: 3600 LB............................................................... 15
Takeoff Distance: 2900 LB............................................................... 16
Takeoff Climb Gradient .................................................................... 17
Takeoff Rate of Climb ...................................................................... 18
Enroute Climb Gradient ................................................................... 19
Enroute Rate of Climb...................................................................... 20
Time, Fuel & Distance to Climb: Full Power Climb .......................... 21
Time, Fuel & Distance to Climb: Cruise Climb................................. 22
Cruise Performance ......................................................................... 23
Range / Endurance: Full Power Climb.............................................25
Range / Endurance: Cruise Climb ................................................... 28
Balked Landing Climb Gradient ....................................................... 31
Balked Landing Rate of Climb ......................................................... 32
Landing Distance ............................................................................. 33
Landing Distance ............................................................................. 34
Original Issue
Section 5: Performance Data
Table of Contents

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