Cirrus SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-5P/N 13772-005 2-5
Airspeed Indicator Markings
The airspeed indicator markings are based on Section 5, Airspeed
Calibration: Normal Static Source Table. When using the alternate
static source, allow for the airspeed calibration variations between the
normal and alternate static sources.
Marking
Value
(KIAS)
Remarks
White Arc 64 - 110 Full Flap Operating Range
Lower limit is the most adverse stall speed in
the landing configuration. Upper limit is the
maximum speed permissible with flaps
extended. Do not use flaps above 17,500 feet
MSL.
Green Arc
up to 17,500 feet MSL
25,000 feet MSL
74 - 176
74 - 150
Normal Operating Range
Lower limit is the maximum weight stall at
most forward C.G. with flaps retracted. Upper
limit is the maximum structural cruising
speed (V
NO
). V
NO
and upper limit of green
arc is reduced linearly from 17,500 feet to
25,000 feet.
Ye l lo w A r c
up to 17,500 MSL
25,000 feet MSL
176 - 205
150 - 175
Caution Range
Operations must be conducted with caution
and only in smooth air. Upper and lower limits
of yellow arc are reduced linearly from
17,500 feet to 25,000 feet.
Red Line
up to 17,500 feet MSL
25,000 feet MSL
205
175
Never Exceed Speed (V
NE
)
Maximum speed for all operations. V
NE
and
red line is reduced linearly from 17,500 feet
to 25,000 feet.
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