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Cirrus DESIGN SR22T User Manual

Cirrus DESIGN SR22T
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2-20 P/N 13772-003
Section 2 Cirrus Design
Limitations SR22T
5. Navigation using the Perspective Integrated Avionics System is
not authorized in the following geographic areas:
a. north of 70°North latitude (northern polar region),
b. south of 70°South latitude (southern polar region),
c. north of the 65°North latitude between longitude 75°W and
120°W (Northern Canada),
d. south of 55°south latitude between longitude 120°E and
165°E (region south of Australia and New Zealand).
6. The MFD checklist display supplements the Pilot Operating
Handbook checklists and is advisory only. Use of the MFD
checklists as the primary set of on-board airplane checklists is
prohibited.
7. The NAVIGATION MAP is intended only to enhance situational
awareness. Use of the NAVIGATION MAP page for pilotage
navigation is prohibited.
8. The TERRAIN PROXIMITY MAP is intended only to enhance
situational awareness. Use of the TERRAIN PROXIMITY
information for primary terrain avoidance is prohibited.
9. LTNG information on the NAVIGATION MAP or WEATHER MAP is
approved only as an aid to hazardous weather avoidance. Use of
the WEATHER MAP for hazardous weather penetration is
prohibited.
10. The SYNTHETIC VISION SYSTEM (SVS) cannot be used for
flight guidance, navigation, traffic avoidance, or terrain avoidance.
Maneuvering the airplane in any phase of flight such as taxi,
takeoff, approach, landing, or roll out shall not be predicated on
SVS imagery. The synthetic vision system is not intended to be
used independently of traditional attitude instrumentation.
Consequently, SVS is disabled when traditional attitude
instrumentation is not available. Otherwise, the traditional attitude
instrumentation will always be visible in the foreground with SVS
features in the background.
11. Use of the TRAFFIC ADVISORY SYSTEM (TAS) to maneuver the
airplane to avoid traffic is prohibited. The TAS is intended for
advisory use only. TAS is intended only to help the pilot to visually
located traffic. It is the responsibility of the pilot to see and
maneuver to avoid traffic.
Revision 1

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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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