
CM170407AMA
SECTION 2 GENERAL INFORMATION
The DMA MPS49 is an automatically controlled low cost Air Data Test solution for
troubleshooting and certification of aircraft pitot-static systems with RVSM accuracy
requirements. It provides facilities for the simulation of altitude, airspeed and a third
pressure (Pd2), for testing Angle of Attack (AoA) smart probes. All rate values are also
controlled.
The MPS49 instrument is simple and fast to use. The operator interface is easy to
understand by both experts and first time users. All testing and troubleshooting with the
MPS49 is carried out via the touch-screen and an intuitively arranged color-coded keyboard
on the front panel (FIG 2).
The values of pressure, altitude, airspeed, AoA and associated rates are shown on the
color graphical LCD display. Commanded and measured test values are simultaneously
displayed at all times.
The MPS49 is also compatible with the DMA MPSRC remote control (FIG 3), that provides
the same operating interface. The MPS49 is designed to reject any commanded values
which exceed pre-programmed limits. Limiting values are password protected.
Test profiles can be programmed and automatically executed by the MPS49.
The Unit Under Test (UUT) is safely isolated in the event of any power loss.
The MPS49 incorporates two internal pump units for pressure and vacuum supplies. The
pumps only run when required, to save power and ensure a longer operating life.
2.1 MAIN PARTS
The MPS49 main parts are:
•
Power supply.
•
Static, Pitot and AoA lines pneumatic components.
•
Electronic circuits, including microprocessor-based systems for pressure measurement
and control.
•
Internal battery.
•
High Performance Piezoresistive Pressure sensors.
•
Compressor – vacuum membrane type pump units.
•
Keyboard and Color Touch-Screen Display.
The front panel (FIG 1) provides operating controls and displays, pressure fittings and
connectors for external control.
The equipment is packaged within a lightweight HDPE (high density polyethylene) case.
2.2 MAIN TECHNICAL SPECIFICATION
2.2.1 FUNCTION
•
Generation of pressure and vacuum sources using the internal pumps.
•
Generation of static (absolute) pressure or altitude.
•
Generation of total (absolute) pressure or dynamic (differential) pressure or airspeed.
•
Generation of angle of attack as differential pressure (Pd2).
D.Marchiori Copyright
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