Cirrus SR22T User Manual

Cirrus Design Section 1
SR22T General
P/N 13772-005 1-11P/N 13772-005 1-11
Engine Power Terminology
OAT Outside Air Temperature is the free air static
temperature obtained from inflight temperature
indications or from ground meteorological sources.
It is expressed in either degrees Celsius or degrees
Fahrenheit.
Pressure
Altitude
Pressure Altitude (PA) is the altitude read from the
altimeter when the altimeter’s barometric
adjustment has been set to 29.92 in.Hg (1013 mb)
corrected for position and instrument error. In this
Handbook, altimeter instrument errors are assumed
to be zero.
Standard
Temperature
Standard Temperature is the temperature that would
be found at a given pressure altitude in the standard
atmosphere. It is 15°C (59°F) at sea level pressure
altitude and decreases approximately 2°C (3.6°F)
for each 1000 feet of altitude increase. See ISA
definition.
BHP Brake Horsepower is the power developed by the
engine.
MCP Maximum Continuous Power is the maximum power
that can be used continuously.
MAP Manifold Pressure is the pressure measured in the
engine’s induction system expressed as inches of
mercury (in.Hg).
RPM Revolutions Per Minute is engine rotational speed.
Static RPM Static RPM is RPM attained during a full-throttle
engine runup when the airplane is on the ground
and stationary.
TIT Turbine Inlet Temperature is the temperature
measured in front of the first stage turbine nozzle
valves.
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