Cirrus SR22T User Manual

Cirrus Design Section 5
SR22T Performance Data
P/N 13772-005 5-31P/N 13772-005 5-31
Balked Landing 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......................................................................................................100% (DN)
•Climb Airspeed.................................................................................................V
REF
Weight
LB
Press Alt
FT
Climb
Speed
(V
REF
)
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile
Temperature ~°C
-20 0 20 40 50 ISA
3600
SL 79 1111 921 751 596 524
792
2000 79 1015 835 674 528 459
744
4000 79 924 754 602 463 398 699
6000 79 838 678 534 402 341
655
8000 79 758 606 470 346 287
613
10000 79 682 539 410 293 237 573
2900
SL 79 1519 1274 1057 861 771
1109
2000 79 1394 1164 959 775 689
1049
4000 79 1277 1061 868 694 612 991
6000 79 1168 965 783 618 541
936
8000 79 1066 874 703 547 474
883
10000 79 970 790 628 481 412 832
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