Cirrus SR22T User Manual

36 of 52 P/N 13772-151
Section 9 Cirrus Design
Supplements SR22T
Balked Landing Climb Gradient with Ice Accumulation
• Note •
Balked Landing Climb Gradients 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 coldest data shown.
Conditions:
•Power....................................................................................................Full Throttle
•Mixture............................................................................................Set per Placard
•Flaps........................................................................................................50% (DN)
•Climb Airspeed...............................................................................................V
REF
Weight
LB
Press
Alt
FT
Climb
Speed,
V
REF
KIAS
CLIMB GRADIENT ~ Feet/Nautical Mile
Temperature ~°C
-20 -10 0 5 ISA
3600
SL
88 796 726 660 628
2000
88 740 673 610 579
4000
88 686 622 562 533
6000
88 635 574 517 489
8000
88 586 529 474 448 479
10000
88 540 486 434 408 459
2900
SL
88 1087 999 915 874
2000
88 1015 931 851 813
4000
88 947 867 791 755
6000
88 883 807 735 700
8000
88 822 750 681 648 687
10000
88 764 696 630 599 662
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