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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 2-17
Taxi Power
Maximum continuous engine speed for taxiing is 1000 RPM on flat,
smooth, hard surfaces. Power settings slightly above 1000 RPM are
permissible to start motion, for turf, soft surfaces, and on inclines. Use
minimum power to maintain taxi speed.
Fuel Limits
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity...................................... 94.5 U.S. Gallon (358.0 L)
Total Fuel Each Tank ................................. 47.25 U.S. Gallon (179.0 L)
Total Usable Fuel (all flight conditions)........ 92.0 U.S. Gallon (348.0 L)
Maximum Allowable Fuel Imbalance .............10.0 U.S. Gallon (¼ tank)
The fuel pump must be set to BOOST for takeoff, climb, landing, and
for switching fuel tanks.
Altitude Limits
Maximum Takeoff Altitude ..........................................10,000 Feet MSL
Maximum Operating Altitude ......................................25,000 Feet MSL
The operating rules (FAR Part 91 and FAR Part 135) require the use of
supplemental oxygen at specified altitudes below the maximum
operating altitude.
Environmental Conditions
Do not operate the airplane below an outside air temperature of -40°F
(-40°C).
Maximum Occupancy
Occupancy of this airplane is limited to four persons (the pilot and
three passengers).
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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