Cirrus SR22T User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-17P/N 13772-005 5-17
Takeoff Climb Gradient
• Note •
Climb Gradient values shown are the gain in altitude for the horizontal
distance traversed expressed as Feet per Nautical Mile.
For operation in air colder than this table provides, use the coldest (left-most)
data shown.
For operation in air warmer than this table provides, use extreme caution.
Conditions:
•Power....................................................................................................Full Throttle
•Mixture.......................................................................................................Full Rich
•Flaps.................................................................................................................50%
•Airspeed.....................................................................................Best Rate of Climb
Weight
LB
Press
Altitude
FT
Climb
Speed
KIAS
CLIMB GRADIENT ~ Feet per Nautical Mile
Temperature ~°C
-20 0 20 40 50 ISA
3600
SL 91 1020 879 752 634 579
782
2000 91 958 823 701 589 537
755
4000 91 898 770 654 547 496
728
6000 91 841 719 608 506 458
702
8000 91 787 671 565 468 422
676
10000 91 735 625 524 431 387
651
2900
SL 94 1303 1148 1002 864 797
1038
2000 94 1251 1097 952 815 750
1016
4000 93 1196 1043 900 765 701
991
6000 93 1137 986 845 713 650
964
8000 92 1077 928 790 660 599
935
10000 92 1015 869 733 607 546
904
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