Original Issue; Engine Power Terminology - Cirrus DESIGN SR22T Pilot Operating Handbook

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Cirrus Design

P/N 13772-003

Original Issue

Pressure Altitude (PA) is the altitude read from the

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

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

Brake Horsepower is the power developed by the

Maximum Continuous Power is the maximum power

that can be used continuously.

Manifold Pressure is the pressure measured in the

engine's induction system expressed as inches of

mercury (in.Hg).

Revolutions Per Minute is engine rotational speed.

Static RPM is RPM attained during a full-throttle

engine runup when the airplane is on the ground

and stationary.

Turbine Inlet Temperature is the temperature

measured in front of the first stage turbine nozzle

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