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Cirrus SR22T User Manual

Cirrus SR22T
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5-14 P/N 13772-005
Section 5 Cirrus Design
Performance Data SR22T
Takeoff Distance
The following factors are to be applied to the computed takeoff distance for
the noted condition:
Headwind - Subtract 10% from computed distance for each 12 knots
headwind.
Tai lw in d - A dd 10 % fo r ea ch 2 k no ts t ai lw in d up t o 1 0 k not s.
Dry Grass Runway - Increase distances by 15% of the ground roll distance.
Sloped Runways - Increase distances by 22% of the ground roll value at Sea
Level, 30% of the ground roll value at 5000 ft, 43% of the ground roll value at
10000 ft for each 1% of upslope; decrease distances by 7% of the ground roll
value at Sea Level, 10% of the ground roll value at 5000 ft, and 14% of the
ground roll value at 10000 ft for each 1% of downslope.
• Caution •
The above corrections for runway slope are required to be included herein
under FAR 23. They should be used with caution since published runway
slope data is usually the net slope from one end of the runway to the other.
Many runways will have portions of their length at greater or lesser slopes
than the published slope, lengthening (or shortening) takeoff ground run
values estimated from the published slope as described above.
If brakes are not held while applying power, distances apply from the point
where full throttle and mixture setting is complete.
For operation in outside air temperatures colder than the Takeoff Distance
table provides, use the coldest data shown.
For operation in outside air temperatures warmer than the Takeoff Distance
table provides, use extreme caution.
Aircraft with optional Air Conditioning System: Add 100 feet to ground roll
distance and 150 feet to distance over 50' obstacle if Air Conditioner is ON
during takeoff.
Conditions:
•Winds................................................................................................................Zero
•Runway.........................................................................................Dry, Level, Paved
•Flaps.................................................................................................................50%
•Air Conditioner..................................................................................................OFF
•Power:
•Throttle.....................................................................................................Full Open
•Mixture............................................................................................Set per Placard
Set prior to brake release for short field takeoff.
Original Issue

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Cirrus SR22T Specifications

General IconGeneral
ManufacturerCirrus Aircraft
EngineContinental TSIO-550-K
Horsepower315 hp
Max Takeoff Weight3, 600 lbs
Service Ceiling25, 000 ft
Cabin Width49 in
Cabin Height50 in
Seating Capacity4
AvionicsCirrus Perspective+ by Garmin
CategorySingle-engine piston aircraft
PropellerHartzell 3-blade composite
Wingspan38 ft 4 in
Length26 ft
Height8 ft 11 in
Maximum Cruise Speed213 KTAS
Fuel Capacity92 gallons
Stall Speed64 knots
Safety FeaturesCirrus Airframe Parachute System (CAPS)
Cruise Speed183 knots

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