Advanced Cockpit Instrumentation Trainer

quick overview :

Features:

The system combines Cockpit analog flight instrumentation, primary flight instrumentation, systems instrumentation and engine instrumentation.

Trainer use the latest in GPS and Digital ADAHRS (Air Data and Attitude Heading and Reference Systems.

Air Data and Attitude Heading and Reference Systems- provide highly accurate and reliable referencing of position, rate, vector and acceleration data.

Three degrees of freedom instrument panel permits full demonstration of attitude and directional gyro functions.

Functional engine monitoring system be connected to engine sensors.

All analog instruments operate manually

Primary flight display be mounted on a panel that can simulate roll, pitch, and yaw movements controlled by a mechanism operated by a control yoke.

Components:

Smart PFD-MFD Screen

Engine Data Modules

Analog instruments

Attitude Gyro and Indicator

Directional Gyro / Heading Indicator

Airspeed Indicator

Altimeter

Vertical Speed Indicator

Turn and Slip Indicator

Fuel Temp/Press Indicator

Oil Temp/Press Indicators

Fuel Level Indicator

MAP

RPM

Vacuum Gauge

Sensors:

Oil Temperature Sensor

Carburetor Air Temp Sensor

Manifold Pressure Sensor

Fuel Level Sensor

Oil Pressure Sensor

Fuel Pressure Sensor

Engine RPM Sensor

Fuel Flow Sensor

Ammeter Shunt

CHT Thermocouples (Qty 4)

EGT Thermocouples (Qty 4)

OAT Sensor

Pitot Tube

Static Port

Inductive sensor

Throttle Lever

Propeller Lever

Pitot-Static System:

Pressure Pump to Create Pitot Pressure

Vacuum Pump to Create Static Pressure

Pitot Tube (not operate)

Fuselage Static Port (not operate)

Alternate Static Port (not operate)

Static Source Selector Switch (not operate)

Two Test Ports for Pitot-Static Test Set

Power

Main Power

PDF

Tachometer

Turn Slip

Vacuum Pump

Contacts:

Pitot Heater

L/G

Taxi Light

Auxiliary Flight Control:

Aileron Trim

Elevator Trim

Flap Position

Electronic Simulation of Sensors:

Oil Temperature Manifold Pressure

Engine RPM

Oil Pressure

Fuel Level

Fuel Press

Sender Selector Panel

Fuel System

Oil System

Vacuum Control Panel

Static System İnstrument

MAP

Fuel Flow

Smart PFD-MFD Screen

NOT: Smart PFD-MFD Screen brand/model and some technical specs can be change due to market availability. (Dynon-Bendix-Garmin or similar)

Screen is very bright and high-resolution driven by advanced graphics processors create highly visible and readable display.

Display is 1280 x 800 pixel, 1200+ nit TFT active-matrix capacitive multi- touch LCD screen.

High-Definition Touch Screen

Display Connectors Specification

There are 37-Pin DIN Connector for the main wiring harness.

There are four (4) RS-232 connector ports for connection to compatible equipment.

All serial ports have configurable baud rates and data formats for use as general-purpose inputs and output.

There is minimum three (2) USB Connectors.

There is an Ethernet Connector to be used to synchronize data between displays.

Displays operate between 10- and 30-volts DC.

Display show “engine instrument data”

Display show “flight instrument data”

Screen Dimensions

7.64″ Wide

5.59″ High

3.13″ Deep

Users should be able to interact via the two knobs, two buttons integrated into the knobs, and eight buttons along the bottom of the display’s bezel and via touch gestures on the display screen itself.

Display have a robust GPS moving map.

Display backlighting is controlled by its ambient light sensor to actively adjust the brightness based on the current lighting conditions or user should be able to adjust the brightness by buttons.

The default layout of screen shows below

PFD

MAP

ENGINE

Screen switch into 100% window or 50%/50% split windows.

There is Count-Up/Count-Down timer in the display.

PFD Page Layout have at least the following:

Airspeed Indicator

Ground Speed (GS)

True Airspeed (TAS)

Airspeed Bug

Airspeed Trend Rate

Attitude Indicator

Flight Path Marker

Altimeter

Setting Barometer (BARO)

Altitude Bug

Altitude Trend Rate

Barometer Setting, and Density Altitude.

Vertical Speed Indicator

Vertical Speed (VS) BUG.

Heading Indicator/Directional Gyro

Heading (HDG) BUG

Slip Ball

Angle of Attack Indicator

OAT (Outside air temperature)

Winds Aloft magnitude and vector

Artificial Horizon/Synthetic Vision

Menu Page have at least the following:

Six Pack

G-meter

Terrain Alert

Airport Flags

HSI SRC

Bugs

There is a Six-Pack presentation options on the PFD.

Main Menu bar are at the bottom of the screen and should include following functions:

NRST – Nearest:

FPL – Flight Plan

INFO

MENU

Message (NO MSG / MESSAGE / CAUTION / WARNING)

KNOPs functions have at least the following:

Adjust Bug (HDG, ALT, etc.) or BARO value

Change Map scale

Activate and/or move cursor

Flight Data Modules have at least the following:

All sensors should be solid state.

Accelerometers, which measure forces in all three directions

Rotational rate sensors, which sense rotation about all three axes

Pressure transducers for measuring air data

Magnetometers on all three axes for measuring magnetic heading.

Engine Data Modules have at least the following:

These modules support popular four and six-cylinder engine installations and should measure a variety of engine and environmental parameters, such as:

RPM

Manifold pressure

Oil temperature

Oil pressure

Exhaust gas temperature (EGT)

Cylinder head temperature (CHT)

Fuel levels for multiple tanks

Voltage

Current

Fuel pressure

Fuel flow

Carburetor air temperature

Coolant pressure and temperature

Flap and trim potentiometers

External contacts