Cirrus SR22T User Manual

Cirrus Design Section 2
SR22T Limitations
P/N 13772-005 2-21P/N 13772-005 2-21
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. Do not use SAFETAXI or CHARTVIEW functions as the basis for
ground maneuvering. SAFETAXI and CHARTVIEW functions have
not been qualified to be used as an Airport Moving Map Display
(AMMD). SAFETAXI and CHARTVIEW are to be used by the flight
crew to orient themselves on the airport surface to improve pilot
situational awareness during ground operations.
9. The TERRAIN PROXIMITY MAP is intended only to enhance
situational awareness. Use of the TERRAIN PROXIMITY
information for primary terrain avoidance is prohibited.
10. 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.
11. 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.
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