Cirrus SR22T User Manual

38 of 52 P/N 13772-151
Section 9 Cirrus Design
Supplements SR22T
Landing Distance with Ice Accumulation
• Note •
The following factors are to be applied to the computed landing distance for the noted
condition:
•Normal landings will be completed with the flaps set to 50%.
•Sloped Runway - Increase table distances by 27% of the ground roll distance for each
1% of downslope. Decrease table distances by 9% of the ground roll distance for
each 1% of upslope.
• Note •
The above corrections for runway slope are required to be included herein for
certification. They should be used with caution since published runway slope data is
usually the net slope from one end of the runway to the other. Many runways will have
portions of their length at greater or lesser slopes than the published slope, lengthening
(or shortening) landing ground run values estimated from the published slope as
described above.
•For operation in outside air temperatures colder than this table provides, use coldest
data shown.
•For operation in outside air temperatures warmer than this table provides, use
extreme caution.
Conditions:
•Winds................................................................................................................Zero
•Runway.........................................................................................Dry, Level, Paved
Original Issue: 02-01-13

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