Cirrus SR22T User Manual

2-20 P/N 13772-005
Section 2 Cirrus Design
Limitations SR22T
e. IFR non-precision approach approval is limited to published
approaches within the U.S. National Airspace System.
Approaches to airports in other airspace are not approved
unless authorized by the appropriate governing authority.
f. RNAV approaches must be conducted utilizing the GPS
sensor.
g. Except when GFC 700 with system software 0764.09 or later
installed, when conducting missed approach procedures,
autopilot (if installed) coupled operation is prohibited until the
pilot has established a rate of climb that ensures all altitude
requirements of the procedure will be met.
h. The Perspective Integrated Avionics System is compliant with
AC 90-100A. As such, the Cirrus Perspective system is
eligible to fly RNAV 'Q' or 'T' routes, RNAV SID/STAR/ODPs
and eligible to use RNAV substitution or RNAV alternate
means of navigation (US Only). Refer to AC 90-100A for
additional operator requirements and limitations.
i. The Perspective Integrated Avionics System includes
navigation sensors that meet the standards set forth in TSO-
C145a/ETSO-C145 (Sensors) and TSO-C146a/ETSO-C146
(Display Units) for Class 3 systems.
j. The Perspective Integrated Avionics System has been
installed in accordance with AC 20-138A and is approved for
navigation using GPS and SBAS (within the coverage of a
Satellite Based Augmentation System complying with ICAO
annex 10) for IFR enroute, terminal and approach operations.
k. The Perspective Integrated Avionics System complies with the
standards set forth in AC 90-96A and JAA TGL-10 (rev 1) for
BRNAV and PRNAV operations.
l. The navigation databases employed by the Perspective
Integrated Avionics System meet the requirements set forth in
AC 20-153 for database integrity, quality and database
management practices. The data in the navigation databases
are referenced to the WGS-84 reference system.
m. The Perspective Integrated Avionics System complies with the
standards set forth in AMC 20-27 and NPA 2009-04 (AMC 20-
28) for RNAV operations including LNAV/VNAV and LPV
approach operations.
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