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Cirrus DESIGN SR22T User Manual

Cirrus DESIGN SR22T
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Cirrus Design Section 2
SR22T Limitations
P/N 13772-003 2-5
Airspeed Indicator Markings
The airspeed indicator markings are based upon Section 5 Airspeed
Calibrations using the normal static source. 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 62 - 104 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
73 - 177
73 - 151
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 l ow A r c
up to 17,500 MSL
25,000 feet MSL
177 - 200
151 - 170
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
200
170
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

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Cirrus DESIGN SR22T Specifications

General IconGeneral
ManufacturerCirrus Aircraft
ModelSR22T
Seating Capacity5
EngineContinental TSIO-550-K
Horsepower315 hp
AvionicsCirrus Perspective+ by Garmin
TypeSingle-engine piston aircraft
Maximum Speed213 knots
Cruise Speed183 knots
Service Ceiling25, 000 feet
Maximum Takeoff Weight3, 600 lbs
Wingspan38 feet 4 inches
Length26 ft
Height8 feet 11 inches
Safety FeaturesCirrus Airframe Parachute System (CAPS)
Cabin Width49 inches
Cabin Height50 inches

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