Cirrus DESIGN SR22T User Manual

Cirrus Design Section 1
SR22T General
P/N 13772-003 1-11
Engine Power Terminology
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 DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches