EasyManuals Logo

Cirrus DESIGN SR22T User Manual

Cirrus DESIGN SR22T
512 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #235 background imageLoading...
Page #235 background image
Cirrus Design Section 7
SR22T Airplane and Systems Description
P/N 13772-003 7-33
Tachometer
Engine speed (RPM) is shown in the upper mid-left corner of the
ENGINE page as both a simulated tachometer and as a digital value.
The tachometer pointer sweeps a scale range from 0 to 3000 RPM in
100 RPM increments. The digital RPM value is displayed in
increments of 10 RPM in white numerals below the gage.
The tachometer receives a speed signal from a magnetic pickup
sensor on the right hand magneto from the Engine Indicating System
via the Engine Airframe Unit.
Exhaust Gas Temperature (EGT)
Exhaust gas temperatures for all six cylinders are displayed in the
Engine Temperature block of the ENGINE page as vertical bars. The
EGT graph is marked from 1000°F to 1800°F in 100°F increments.
The digital EGT value of the cylinder is displayed above the bar in
white numerals. A sensor in the exhaust pipe of each cylinder
measures exhaust gas temperature and provides a voltage signal to
the Engine Airframe Unit which processes and transmits the data to
the Engine Indicating System.
Cylinder Head Temperature (CHT)
Cylinder head temperatures for all six cylinders are displayed in the
Engine Temperature block of the ENGINE page as vertical bars. The
CHT graph is marked from 100°F to 500°F in 100°F increments. The
digital CHT value of the cylinder is displayed above the bar in white
numerals.
A sensor in each cylinder head measures cylinder head temperature
and provides a voltage signal to the Engine Airframe Unit which
processes and transmits the data to the Engine Indicating System.
Turbine Inlet Temperature (TIT)
Turbine inlet temperature for the LH and RH turbochargers is displayed
in the Engine Temperature block of the ENGINE page as vertical bars.
The TIT graph is marked from 1000°F to 1800°F in 100°F increments.
The digital TIT value of the turbine inlet is displayed above the bar in
white numerals.
A sensor in each turbocharger measures turbine inlet temperature and
provides a voltage signal to the Engine Airframe Unit which processes
and transmits the data to the Engine Indicating System. The TIT gage
is used as the primary source to lean fuel mixture.
Original Issue

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Cirrus DESIGN SR22T and is the answer not in the manual?

Cirrus DESIGN SR22T Specifications

General IconGeneral
ManufacturerCirrus Aircraft
ModelSR22T
Seating Capacity5
EngineContinental TSIO-550-K
Horsepower315 hp
AvionicsCirrus Perspective+ by Garmin
TypeSingle-engine piston aircraft
Maximum Speed213 knots
Cruise Speed183 knots
Service Ceiling25, 000 feet
Maximum Takeoff Weight3, 600 lbs
Wingspan38 feet 4 inches
Length26 ft
Height8 feet 11 inches
Safety FeaturesCirrus Airframe Parachute System (CAPS)
Cabin Width49 inches
Cabin Height50 inches

Related product manuals