AutoGyro MTOsport, Руководство по обслуживанию

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Manufacturer
Maintenance Manual
AutoGyro
MTOsport
MMM-MT-C_14-11-19 Part C
– System Description Section (Ch. 21 – 90)
Page 13 of 22
CHAPTER 34 - NAVIGATION
34-10-00 Flight Environment Data
Total pressure is picked up by a pitot tube located in the nose section of the fuselage. The tube is
connected to the integrated cockpit instruments by a plastic line. Static pressure is measured across
two ports, one on either side of the fuselage. In older versions, static pressure is measured through
the open ports of the instrumentation, right behind the cockpit panel.
OAT data can be derived from rotor bearing temperature which is measured by a battery powered
(earlier version) or by the on-board supply system (current version) powered temperature at the rotor
34-20-00 Attitude and Direction
As part of minimum equipment, a magnetic compass is installed in the forward station or instrument
panel
in pilot’s sight. As an option, a vertical compass may be installed in the instrument panel.
34-70-00 ATC Transponder
An ATC Transponder may be installed as an option. Possible installation positions in the instrument
panel are described in
CHAPTER 31 .
Please refer to the manufacturer’s documentation for reference.
CHAPTER 35 - N/A
CHAPTER 36 - PNEUMATIC
Aircraft trim, rotor brake and activation of the pre-rotator is controlled by a pneumatic system,
consisting of an electrically driven air compressor with filter/dryer, a pressure gauge in the cockpit, a
pressure compensation vessel, solenoid valves, air lines, pneumatic actuators, and the respective
cockpit controls.
The pneumatic system controls the following function:

rotor brake ON, effects i.e. rotor disc flat / flight control stick forward position (brake mode)

adjustable longitudinal trim, effects i.e. rotor disc/stick pulled aft (flight mode)

engagement of the pre-rotator, i.e. activation of the clutch and upper engagement
(only in flight mode or in brake mode with overdrive/override button)
The aforementioned functions are described in more detail in the dedicated chapters.
A schematic drawing of the pneumatic system is provided in Part D - Diagrams and Charts of this
manual.
36-11-00 Generation / Compressor
The electrically driven compressor and filter/dryer is located behind the instrument panel. The wiring
diagram is provided in
Part D - Diagrams and Charts of this manual.
36-21-00 Distribution
Air distribution comprises of hoses, valves (solenoids), (cockpit) controls and switches, (pressure)
sensors and a pressure compensation vessel. The main pneumatic switching logic is combined in the
pneumatic control which is installed behind the instrument panel. See
Part D - Diagrams and Charts
for schematics.
Note that the pneumatics actuators (cylinders) are not described in this ATA Chapter, but assigned to
their mechanical main function.
Example: the brake/trim cylinder is described in 67-05-00 Pitch Trim System / Rotor Brake .