The Autopilot system uses the full complement of internal inertial sensors of the EFIS/One or EFIS/Lite to precisely detect aircraft movement in all three axes. Other internal sensors for airspeed and altitude also play a roll in the function and operation of the Autopilot providing the best dynamic performance possible. Compare the BMA Digital Autopilot to the Trutrak DFC-250. You can buy and EFIS/Lite and our Digital AP for less!

Since the Autopilot system software has access to the all sensors and limitation settings of the aircraft, it can act in a intelligent fashion to increase overall safety. For example, the AP system will limit a climb rate such that airspeed is never reduced below Vy. Although not currently implemented, the AP could also warn if a given flight path, say using a gs/loc signal, was not taking you to a runway, or if a given flight path took you too close to terrain. External AP made by other manufactures don't have available to them the wealth of data that is available to the AP system software in the EFIS/One. The Autopilot functionality is easily accessed through a signal button on the EFIS/ One bezel or remote keypad for the EFIS/Lite. Upon pressing the AP button a simple, easy to understand, menu is shown allowing the pilot to select the various features of the autopilot system. That's all there is to it. The AP can be disengaged three different ways: a remotely mounted disengage momentary switch, usually yoke mounted, by pressing the AP button on the bezel and pushing the concentric knob or by removing power from the AP subsystem with an AP master switch.When the BMA Digital Autopilot is not engaged, there will be no drag on the aircraft controls. Most autopilot systems don't completely disengage from the flight controls and can be felt by the pilot in today's modern aircraft that have light control forces and small movement. BMA uses an electro-magnetic clutch which provides both a safety factor and makes our system impossible to detect, by the pilot, when not in use.

FEATURES: Track any selected course using a Course Bug on the EHSI. Track any selected heading using a Heading Bug on the EHSI. Track and fly a GPS flight plan from the EFIS/One built in GPS receiver. Track an external NAV receiver signal for the selected VOR radial (EFIS/Lite requires an UPS Garmin SL30 radio). Track a Localizer and Glideslope signal from an external NAV receiver. Climb at a given rate (feet/min). Fly to and hold at a specific altitude.

The kit includes everything you need. Two servos, interconnect cables from the servos to the servo controller and a single cable from the controller to the EFIS/One or EFIS/Lite. The components can be mounted in any orientation or location. All aircraft sensing data is provided by the EFIS/One or EFIS/Lite.
 

FEATURES: Electronic ADI and Flight Director: Replaces conventional six-pack. Breathtaking high resolution terrain on all models. Smoothest and fastest AHRS made: 420 degrees/sec. HITS - Highway in the sky / Flight Director. NEW processors for better performance. Dazzingly bright sunlight readable displays in 3.8”, 5” and 8” split screen. Electronic HSI and Navigation: Follow WAAS GPS, Virtual VOR, External VOR, Heading Bug. Can display GS/LOC/CDI/ILS/VOR/OBS. Worldwide Jeppesen® Database. Flight planning and optional Digital Autopilot. Magnetic Heading, GPS Lat/Lon, Wind Speed and Direction, and two engine gauges. Terrain View with VFR and IFR Charts. Engine Monitoring System Option: Precision Engine Monitoring with the BMA Engine POD. For aircraft engines, auto conversions, turbines and radials. Graphically monitor EGT/CHT trends. Monitor RPM, MP, Oil Pressure and emperature, volts/Amps, Fuel Pressure and Flow, Fuel quantities, Hydraulic Pressure, ITT, CHT and EGT with trend analysis, Leaning Function, and OAT.
 

FEATURES: Electronic ADI and Flight Director: Replaces conventional six-pack. Breathtaking high resolution terrain on all models. Smoothest and fastest AHRS made: 420 degrees/sec. HITS - Highway in the sky / Flight Director. NEW processors for better performance. Dazzingly bright sunlight readable displays in 3.8”, 5” and 8” split screen. Electronic HSI and Navigation: Follow WAAS GPS, Virtual VOR, External VOR, Heading Bug. Can display GS/LOC/CDI/ILS/VOR/OBS. Worldwide Jeppesen® Database. Flight planning and optional Digital Autopilot. Magnetic Heading, GPS Lat/Lon, Wind Speed and Direction, and two engine gauges. Terrain View with VFR and IFR Charts. Engine Monitoring System Option: Precision Engine Monitoring with the BMA Engine POD. For aircraft engines, auto conversions, turbines and radials. Graphically monitor EGT/CHT trends. Monitor RPM, MP, Oil Pressure and emperature, volts/Amps, Fuel Pressure and Flow, Fuel quantities, Hydraulic Pressure, ITT, CHT and EGT with trend analysis, Leaning Function, and OAT.
 

FEATURES: Electronic ADI and Flight Director: Replaces conventional six-pack. Breathtaking high resolution terrain on all models. Smoothest and fastest AHRS made: 420 degrees/sec. HITS - Highway in the sky / Flight Director. NEW processors for better performance. Dazzingly bright sunlight readable displays in 3.8”, 5” and 8” split screen. Electronic HSI and Navigation: Follow WAAS GPS, Virtual VOR, External VOR, Heading Bug. Can display GS/LOC/CDI/ILS/VOR/OBS. Worldwide Jeppesen® Database. Flight planning and optional Digital Autopilot. Magnetic Heading, GPS Lat/Lon, Wind Speed and Direction, and two engine gauges. Terrain View with VFR and IFR Charts. Engine Monitoring System Option: Precision Engine Monitoring with the BMA Engine POD. For aircraft engines, auto conversions, turbines and radials. Graphically monitor EGT/CHT trends. Monitor RPM, MP, Oil Pressure and emperature, volts/Amps, Fuel Pressure and Flow, Fuel quantities, Hydraulic Pressure, ITT, CHT and EGT with trend analysis, Leaning Function, and OAT.
 

EFIS/One has solid-state instruments for: Airspeed, Altitude and VSI, magnetically slaved all-attitude compass, HSI, solid state AHRS (Attitude Heading Reference System), a 12 channel GPS navigation engine and the highest resolution 3D terrain available. There's also a built in digital autopilot with altitude hold and ILS capture, a full air data computer with fuel burn and fuel totalizing functions, a flight planning system and digital monitoring of up to 32 engine gauges. Select from either US or worldwide database. Using the built in flight recorder and the new Flight Performance Software, monitor all your flights, engine performance and much more.

System Includes: EFIS/One Processor, 10.4" transflective LCD sunlight readable display, all inertial components, 12 Channel GPS receiver and antenna, magnetometer, CD or DVD drive for updates, all interconnect and power cables.

EFIS/One is also available with Dual Display
 

The BMA Engine Pod is standard for the EFIS/One G4 and available as an option for all other BMA EFIS products. The Engine Pod can also give you important EGT, CHT and Trend information critical to in-flight engine tuning. Select EGT mode and you can follow a graphical presentation of the exhaust gas temperature while also displaying the hottest cylinder head temperature. Select CHT mode and follow your cylinder temperatures while displaying the hottest EGT. By selecting the Trend mode for either EGT or CHT, the display will graphically present a 120 second trend for the selected temperature. The BMA Engine Pod is so simple because most sensors are already calibrated for you. That gets you in the air sooner. The Engine Pod is so versatile it can suit just about any installation.

FEATURES: Your Blue Mountain Avionics EFIS unit and Engine Pod can monitor: RPM or N1 speed, Manifold Pressure, Oil Pressure, Oil Temperature, Fuel Flow-2 Channels, Fuel Pressure, EGTs, up to 9 Channels, Nitrogen Pressure, CHTs, up to 9 Channels, Volts and Amps, Main and Emergency Hydraulic Pressure, OAT, 3 Fuel Quantity Indicators, 2 ITT Channels Available.
 

FEATURES: Optional Avionics Master Switching; Ten (10) Avionics Circuits; Six (6) Switched Circuits; Seven (7) Switch Annunciators Included; Pitch and Roll Trim Circuits; Flaps/Speed Brakes Circuit; Coolie Hat Switch Provisions. Audible Alarm Circuit
 

FEATURES: • 25+ years of experience and over 15 TSO’d instrument designs have been incorporated into the MVP-50. • No more scanning a panel full of gauges looking for a possible problem. All your engine instruments are in one location. If any function exceeds its pilot programmed limit, the display will change color and blink, an external warning light will blink and a voice warning will be activated. • The MVP-50 will not go out of date. The USB Port allows you to add pilot-generated checklists, flight plans, general information and voice warnings. Also, program upgrades and new features may be uploaded through this port. • The Bar Graph Engine Analyzer incorporates many NEW advanced diagnostic features to help insure excellent engine health and proper operation. • Automatically finds and displays the first and the last cylinder to reach peak EGT. • Tattletale bars show which cylinders have reached peak EGT and at what temperature. • The digital display shows the exact temperature at which each cylinder is operating rich or lean of peak EGT. • Bars change colors when pilot programmed limits are reached. • In the Digital “ACTUAL” mode, EGTs and CHTs are presented in a digital format. • In the Digital “DIFF” mode the EGT & CHT spread between cylinders is presented. • Any out-of-range temperatures will be displayed in red or yellow. All limits and colors are pilot programmable. • EGT and CHT spread between the hottest and coldest cylinder are automatically calculated and displayed. • Shock cooling is calculated and displayed. • Any time one of several Flight Data Screens are displayed, the primary engine instruments are shown on the right side of the display. • The “Fuel Management” data screen shows Four Fuel Tanks, Fuel Flow, Fuel Used, Fuel Remaining, Time to Empty, Distance to Empty, Ground Speed, Efficiency (MPG), Fuel to Waypoint, Time to Waypoint, and Distance to Waypoint. • Fuel Reserve, Time Reserve and Distance reserve are automatically calculated from Fuel Flow, Fuel Remaining and GPS Data. If you do not have a minimum of 45 minutes of reserve fuel, the display will turn yellow. If you cannot reach your destination with the remaining fuel, the display will turn red. • Standard and pilot-generated Checklists, Flight Plans and General Information Screens provide a Flight Management System tailored to your aircraft and to each flight. • Simple and easy operation puts all the flight data where you need it, when you need it. The MVP-50 allows you to create a weight and balance chart for your aircraft. Both data and graph formats are provided. Any time a CG or weight limit is violated the appropriate display value will turn red. Whether you add or remove fuel, baggage or passengers, the new weight and CG data are immediately displayed. The MVP-50 also will show your reserve weight as each item is added to the aircraft. Some additional MVP-50 Screens: Add Fuel; Warning Controls; USB and Data Recording; General Information; Timers; and Clock and Date.

ADDITIONAL FEATURES AND SPECIFICATIONS:

Hardware Configuration: All of the probes, transducers and extension cables are connected to a small box (4.5" x 3.5" x 2.2") called the EDC (Engine Data Converter). The EDC can be mounted on the inside firewall of the aircraft. The EDC converts all engine data to serial data, which is then provided to the MVP-50 via two wires. This configuration makes installation much easier by reducing the wires to the instrument panel and eliminating the installation of many individual instruments. Available Functions: RPM - Works on Mags or Electronic Ignitions. Fuel Flow - Also operates on engines with return fuel lines. Fuel Left, Fuel Right, Fuel Main, Fuel Aux, Fuel Tip Left, Fuel Tip Right and Fuel Header. Volts, Volts Main, Volts Aux, Volts Emergency and Volts Backup. Amps, Amps Main, Amps Aux, Amps Emergency and Amps Backup. M.P., Oil Press, Fuel Press, Hydraulic Press, Water Press, Cabin Press and Upper Deck Press. Flaps, Rudder, Elevator, G-Meter, C.O., and Angle-of-attack. EGT, CHT, TIT, TIT L., TIT R., Oil T., Carb T., Cabin T., OAT, Cowl T., Water T., Alt T., Heater T., Super Heat, CDT, CDI T., CDO T., Power Reduction Unit T., Shock Cooling, EGT Diff and CHT Diff. H.P., Flt Timer, Up Timer, Down Timer, Tach Timer, Engine Hours, Date, Local Time (12 or 24), Zulu Time, Weight and Balance data, Fuel Used, Fuel Rem, Time to Empty, Distance to Empty, Fuel Reserve, Time Reserve and Distance Reserve. Remarkable Data Recording: .33 second to 6 minute intervals. Stores over 3,330 hours at 30 second intervals! Data is downloaded via USB Memory Stick. The Downloads can then be analyzed using the EGView Software (no conversion required). * New functions can be uploaded through the USB port as they become available. Kits: Complete kits are available for any engine and most aircraft functions. A kit will include pressure transducers, temperature probes, RPM pick-ups, extension cables, flow transducer, shunt and pre-wired connectors. Any special probes can be accommodated through any of the EDC inputs and the MVP-50 configuration screen. Also available for 6 cyl/single engine.
 

Also available the EDM-900-6C, same features as the 4C version.

Call APG-Eastern Avionics for certified versions for primary use in production aircraft.
 

Call APG-Eastern Avionics for certified versions for primary use in production aircraft.
 

The Flight Op MFD is designed to interface with a variety of navigation and communication radios, TCAD traffic and collision alert devices, real-time weather receivers, lightning strike finders and with the 10.4" display, a forward-looking infrared camera. Data from these devices can be displayed on the MFD and EFIS to allow for a variety and mixture of situational awareness displays. Aviation radios can be tuned from our MFD, eliminating the need to divert attention from the display to tune the radio. The MFD can be used to display engine instruments, or a combination of engine instruments and a navigation display. Engine instrumentation can be easily customized to an individual installation by using the system's setup menus. After installation, a series of setup menus can be used to customize the engine instruments to the airplane that the system is installed on. The system is designed to be compatible with single or twin engine, piston or turbine powered airplanes.

The Flight Op MFD navigation display consists of a full-color moving map which is driven by the system’s internal GPS receiver. In addition, it may be desirable to interface the system to panel-mounted GPS receivers. Symbology used for the moving map is similar to that of paper navigation charts so additional training is not required to use it. The navigation display also includes a terrain warning overlay which can to displayed for additional situational awareness or suppressed to de-clutter the display. Situational awareness can be further enhanced by displaying data received from traffic systems, lightning strike finders or real-time weather receivers on the moving map. Flight plans are entered and displayed on the navigation display and direct-to navigation and nearest search keys lower the heads-down time required for flight planning. When flying approach procedures, the MFD displays a full screen approach plate view that shows the aircraft location in both the lateral and vertical planes. Autopilot coupling provides control throughout the approach procedure and the missed approach is automatically selected if needed. The active flight plan, and the predicted time at each waypoint can be continuously displayed or hidden to further de-clutter the navigation display. Frequencies for airports in the flight plan and the destination airport can be obtained at any time by using a COMM hot key and entering the desired airport. The heading bug can be set by pressing the HDG hot key and dialing in the new heading. Software and navigation database updates are accomplished by simply inserting a data card with the update into the card reader in the display unit and powering the unit on.

SPECIFICATIONS:

10.4” Display: System Weight 10.2 lbs; Display Height 11.14 inches; Display Width 8.94 inches; Display Depth 5.69 inches. System Power 70 watts 62 watts 8.4” Display: System Weight 9.2 lbs; Display Height 9.0 inches; Display Width 7.9 inches; Display Depth 4.4 inches; System Power 62 watts. Electrical 10 – 28 VDC; Operating Temperature -20 C to +70 C (fan cooling); Screen Brightness 1500 nits; Solid-state Air Data System Included; Solid-state AHRS Included; Internal GPS Receiver Included; Synthetic Vision Yes; Graphical Traffic in Attitude Yes; Airports in Synthetic Terrain Yes; Graphical Terrain Warning Yes; Graphical Airspace Yes; Engine Monitoring Yes; Highway-in-the-Sky Yes; TCAD Interface Yes / Ryan TCAD, Garmin 330; Real-Time Weather Interface Yes / WSI InFlight; Nav/Com Frequency Search Yes; Nav/Com Tuning from EFIS Yes (Garmin AT SL30, SL40); Autopilot Interface Yes / TruTrak, S-Tec, Century; RS232 Interfaces Seven bi-directional channels; ARINC 429 Interfaces Four receive; two transmit channels.

Supported Interfaces: Nav Radios - Garmin AT SL30; GPS - Garmin AT GX 50/55/60/65; Nav/Com/GPS - Garmin GNS 430/530, Garmin AT GNS80; Weather - WSI InFlight satellite weather receiver; Traffic - Ryan TCAD 9900, Garmin GTXTM330; FLIR Camera - Forward Vision.

The Flight Op 200 MFD consists of the following instrumentation:

An Electronic Horizontal Situational Indicator (HSI) including: Color-coded Airspace; Full-Screen Approach Procedure Display; FLIR Camera Display (optional); Course Pointer; 2 Bearing Pointers; DME Display Course Deviation; Color Moving Map; Graphical Terrain; Graphical Weather including NOTAMS, METARS, SIGMETS, TFRs; Traffic Display; Strikefinder Display; Map De-clutter Functions; Automatic Waypoint Sequencing; Bearing, Distance and ETA to Active Waypoint; Nearest Airport Search; “Direct-To” Navigation; Clock; Timer; Destination Page: Distance and ETA at destination, Predicted fuel remaining in volume and time at destination, Approach and airport radio frequencies.

Engine Indicator and Crew Alert System (EICAS) which displays up to 10 engine instruments.

Tuning of Supported Nav/Com Radios from the EFIS.
 

Op Technologies sets the standard for EFIS technology with advanced features including an optional FLIR camera interface to provide unparalleled situational awareness in day or night or any weather conditions. The EFIS is an integrated display system designed to provide total situational awareness with intuitive displays available in a variety of screen sizes. The EFIS combines a Primary Flight Display and a Multi-function Display in a single screen with easy-to-use menus.

The Flight Op Synthetic Vision includes not only real-time synthetic vision with highway in the sky but the display of airports with runway detail in the attitude indicator. Lowering pilot workload and increasing safety is the first priority and the display gives you the peace of mind of approach guidance down to the runway. For additional situational awareness, even unusable runway and the center line are shown to help you line up the approach. When you're flying in crowded airspace the Flight Op EFIS has you covered. The display units can be interfaced with either a Mode S transponder or the Ryan TCAD to provide you with a real-time display of traffic information in both the attitude indicator and the full-color moving map. Traffic symbols are color-coded to allow you to quickly recognize any traffic at your altitude or on a possible collision course and take action. With the optional FLIR camera, the traffic can even be "visually" identified. The Flight Op EFIS is the obvious choice for your experimental aircraft. The EFIS was designed to allow for installation in a wide variety of aircraft by a builder or professional installer. Intuitive set-up menus walk the installer through a number of configuration options to customize the display to the aircraft it is installed in. The ranges, limits and units on the instrumentation and the aircraft's engine probes are identified during this process. The flexibility of the system allows for installation in a piston or turbine aircraft and the entire process is accomplished in the cockpit without the use of an external keyboard.

SPECIFICATIONS:

10.4” Display: System Weight 10.2 lbs; Display Height 11.14 inches; Display Width 8.94 inches; Display Depth 5.69 inches. System Power 70 watts 62 watts 8.4” Display: System Weight 9.2 lbs; Display Height 9.0 inches; Display Width 7.9 inches; Display Depth 4.4 inches; System Power 62 watts. Electrical 10 – 28 VDC; Operating Temperature -20 C to +70 C (fan cooling); Screen Brightness 1500 nits; Solid-state Air Data System Included; Solid-state AHRS Included; Internal GPS Receiver Included; Synthetic Vision Yes; Graphical Traffic in Attitude Yes; Airports in Synthetic Terrain Yes; Graphical Terrain Warning Yes; Graphical Airspace Yes; Engine Monitoring Yes; Highway-in-the-Sky Yes; TCAD Interface Yes / Ryan TCAD, Garmin 330; Real-Time Weather Interface Yes / WSI InFlight; Nav/Com Frequency Search Yes; Nav/Com Tuning from EFIS Yes (Garmin AT SL30, SL40); Autopilot Interface Yes / TruTrak, S-Tec, Century; RS232 Interfaces Seven bi-directional channels; ARINC 429 Interfaces Four receive; two transmit channels.

Supported Interfaces: Nav Radios - Garmin AT SL30; GPS - Garmin AT GX 50/55/60/65; Nav/Com/GPS - Garmin GNS 430/530, Garmin AT GNS80; Air Data Computer - Op Technologies Flight Op solid-state ADC unit; Attitude Heading and Reference System (AHRS) - Crossbow AHRS500, Crossbow AHRS420; Weather - WSI InFlight satellite weather receiver; Traffic- Ryan TCAD 9900, Garmin GTXTM330; FLIR Camera - Forward Vision.

The Flight Op 200 consists of the following instrumentation:

A Primary Flight Display (PFD) including: Airspeed Indicator; Attitude Indicator; Altitude Indicator; Vertical Speed Indicator; Highway-in-the-sky Guidance; 3-D Real-Time Synthetic Vision; Real-Time Traffic Display; Airports Displayed in Synthetic Vision and Glideslope/Deviation Indicator.

An Electronic Horizontal Situational Indicator (HSI) including: Color-coded Airspace; Approach Procedure Display; Course Pointer; 2 Bearing Pointers; DME Display Course Deviation; Color Moving Map; Graphical Terrain; Graphical Weather including NOTAMS, METARS, SIGMETS, TFRs; Traffic Display; Strikefinder Display; Map De-clutter Functions; Automatic Waypoint Sequencing; Bearing, Distance and ETA to Active Waypoint; Nearest Airport Search; “Direct-To” Navigation; Clock; Timer; Destination Page: Distance and ETA at destination, Predicted fuel remaining in volume and time at destination, Approach and airport radio frequencies.

Engine Indicator and Crew Alert System (EICAS) which displays up to 10 engine instruments.

Tuning of Supported Nav/Com Radios from the EFIS.
 

The OP Integrated is offered in a number of configurations making the system customizable for almost any experimental airplane.

FEATURES to choose from: 3 screen sizes: 8.4” portrait, 10.4” portrait, 10.4” landscape; Single or dual VOR/LOC/GS receivers; Single of dual Communication transceivers; Single of dual WAAS/GPS receivers; Single or dual Attitude and Heading Reference Systems (AHRS) for redundancy; Single or dual Air Data Computers (ADC) for redundancy; Optional Engine Indication and Crew Alerting System (EICAS) with support for single or twin engine, piston or turbine airplanes.

SPECIFICATIONS:

10.4” Display: System Weight 10.2 lbs; Display Height 11.14 inches; Display Width 8.94 inches; Display Depth 5.69 inches. System Power 70 watts 62 watts 8.4” Display: System Weight 9.2 lbs; Display Height 9.0 inches; Display Width 7.9 inches; Display Depth 4.4 inches; System Power 62 watts. Electrical 10 – 28 VDC; Operating Temperature -20 C to +70 C (fan cooling); Screen Brightness 1500 nits; Solid-state Air Data System Included; Solid-state AHRS Included; Internal GPS Receiver Included; Synthetic Vision Yes; Graphical Traffic in Attitude Yes; Airports in Synthetic Terrain Yes; Graphical Terrain Warning Yes; Graphical Airspace Yes; Engine Monitoring Yes; Highway-in-the-Sky Yes; TCAD Interface Yes / Ryan TCAD, Garmin 330; Real-Time Weather Interface Yes / WSI InFlight; Nav/Com Frequency Search Yes; Nav/Com Tuning from EFIS Yes (Garmin AT SL30, SL40); Autopilot Interface Yes / TruTrak, S-Tec, Century; RS232 Interfaces Seven bi-directional channels; ARINC 429 Interfaces Four receive; two transmit channels.

The OP Integrated Flight Deck consists of the following instrumentation:

A Primary Flight Display (PFD) including: Airspeed Indicator; Attitude Indicator; Altitude Indicator; Vertical Speed Indicator; Highway-in-the-sky Guidance; 3-D Real-Time Synthetic Vision; Real-Time Traffic Display; Airports Displayed in Synthetic Vision and Glideslope/Deviation Indicator.

An Electronic Horizontal Situational Indicator (HSI) including: Color-coded Airspace; Approach Procedure Display; Course Pointer; 2 Bearing Pointers; DME Display Course Deviation; Color Moving Map; Graphical Terrain; Graphical Weather including NOTAMS, METARS, SIGMETS, TFRs; Traffic Display; Strikefinder Display; Map De-clutter Functions; Automatic Waypoint Sequencing; Bearing, Distance and ETA to Active Waypoint; Nearest Airport Search; “Direct-To” Navigation; Clock; Timer; Destination Page: Distance and ETA at destination, Predicted fuel remaining in volume and time at destination, Approach and airport radio frequencies.

Engine Indicator and Crew Alert System (EICAS) which displays up to 10 engine instruments.

FEATURES: Connect your Intercom to other TL elektronic instruments using the iFamily® Bus to enable the option of a voice alert, which will warn you of the exceeded limits; download the latest version of the firmware to your Intercom. Designed for all types of aircraft and RDST; enables the connection to all hand-held and other aircraft RDST; incorporates an output for a CD/cassette player to enable recording the communication from the RDST; ISOLATE function via an external button for separating the communication of the pilot and the passengers; EMERGENCY function for re-playing the pre-recorded messages; indication of all selected functions show clearly on the display; possibility of volume control during the transmission (SIDE TONE); possibility of volume control separately for the pilot and the co-pilot; and automatic MUTE function for the AUX (CD/Cassette) while receiving from the RDST. Simple two-button control using the nav-menu and user-programmable external button for quick selection of any function

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts;backlights internal or external: 5V, 12V or 24V;current consumption: 50 to 250 mA @ 14 Volts;operating: -20°C to 70°C (-4°F to 158°F) temperature range;relative humidity: 95% without condensation;load: +/-20 g;vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs);dimensions: 71x67x45 mm (2.795x2.637x1.771 inch);diameter hole: 57 mm (2 1/4’’); source voltage to the Microphone: 8 Volts, 560 ohms; microphone type: Amplified electret or dynamic microphone; output power: 100mW@150 ohm;Aux input: 0.2 to 2Volts@1kHz; Aux output: 1mV@1kHz;voice alarm and check list memory capability: 16MB;communication line with a PC via standard RS-232c.
 

FEATURES: Display immediately the maximum fuel consumption, fuel pressure, etc. by pressing the external button; using your PC, download at any time the history of fuel consumption, fuel pressure, contents of tank, etc.; connect your Fuel Computer to the output of the signalisation unit, which will warn you of the exceeded limits, e.g. the low pressure or the minimum fuel level reached. You can also connect your Fuel Computer with the Intercom or the Voice Module using the iFamily® Bus and gain the option of having a voice alert of the exceeded values, low fuel levels, etc. and you can at any time download the latest version of the firmware to your Fuel Computer. Measures the instant and the average fuel consumption up to 100 l/hour (30 GPH); displays in liters, US gallons or British gallons; remaining flight time, engine hours, overall information on fuel used; fuel tank levels (L, R, L+R) and fuel pressure; calibrate the fuel level sensor in the tank within 15 steps. You may order a high-quality metal flow sensor providing high-precision measurement; choice of the resistive sensor or the capacity fuel level sensor; choice of the resistive sensor or the fuel pressure sensor with the voltage output. Simple two-button control using the nav-menu; history of the measured values with use of the SchecK® method; user-programmable external switch for quick selection of any function.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts;backlights internal or external: 5V, 12V or 24V;current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; resolution: 0.1 Liter/hour (0.26US-Gallon), 0.01 bar (0.14PSI);measurement: +/-1%(not including sensor accuracy);flow rate: According to flow sensor (max. 1000 pulse per second); operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); input for fuel level sensors: active 0 to 5 Volts / passive 0 to 500 ohms; input for fuel pressure sensors: active 0 to 5 Volts / passive 0 to 500 ohms; input for flow sensor: HIGH level detected; communication line with a PC via standard RS-232c; and second communication line with a GPS via standard RS-232c.
 

FEATURES: Display immediately the maximum reached temperature, pressure etc. by pressing the external button; using your PC, download at any time the history of the measured temperature (or pressure) values; connect your Thermometer to the output of the signalisation unit, which will warn you of the exceeded temperature limits; connect your Thermometer with the Intercom, using the iFamily® Bus, and gain the option of having a voice alert of the exceeded values; you can at any time download the latest version of the firmware to your Thermometer. Measures EGT and CHT temperatures using thermocouple sensors of the type K and J; measures the temperature of oil and water ; displays in °C or °F; measures oil pressure using resistive sensors or sensors with the voltage output; high-precision measurement; simple two-button control using the nav-menu; obtain history of the measured values with use of the SchecK® method ;and user-programmable external button for the quick selection of any function.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measurement: +/-1%(not including sensor accuracy); resolution: 1°C (33.8°F), 0.1 bar (1.45PSI); operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); EGT input for thermocouple probe: -40 °C to 1100 °C by environmental temperature 25 °C; CHT input for thermocouple probe: -20 °C to 800 °C by environmental temperature 25 °C; input for pressure sensor: active 0 to 5 Volts / passive 0 to 500 ohms ; input for temperature sensors: PT-100 or VDO silver line with black isolator; choke control via analog modal servo (external power for servo required); and communication line with a PC via standard RS-232c.
 

FEATURES: Display immediately the maximum reached voltage, current, frequency, etc., by pressing the external button; using your PC, download at any time the history of the measured current and voltage from the Volt-Ampere Meter; connect your Volt-Ampere Meter to the output of the signalisation unit, which will warn you of the exceeded current and voltage limits;connect your Volt-Ampere Meter with the Intercom, using the iFamily® Bus, and gain the option of having a voice alert of the exceeded limits; you can at any time download the latest version of the firmware to your Volt-Ampere Meter. This instrument is designed for all types of aircraft power network; measures voltage of up to 60 V or of up to 250 V (60Hz or 400Hz); version ACV; measures current of up to 50 A or higher, according to the type of the shunt; high-precision measurement; simple two-button control using the nav-menu; history of the measured values with use of the SchecK® method; and user-programmable external button for the quick selection of any function.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measuring range: 60 or 250 Volts, 100 Amps; resolution: 1 Volts, 0,1 Amps; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); output voltage of shunt: 100mV max. (1mV @ 1Amps); and communication line with a PC via standard RS-232c.
 

FEATURES: Display immediately the maximum reached rotation speed etc. by pressing the external button; using your PC, download at any time the history of the measured rotation speed from the RPM Meter; connect your RPM Meter to the output of the signalisation unit, which will warn you of the exceeded rotation speed limits; connect your RPM Meter with the Intercom using the iFamily® Bus and gain the option of having a voice alert of the exceeded limits; you can at any time download the latest version of the firmware to your RPM Meter, thereby always having the latest functions we prepare for you; designed for all types of engine ; incorporates the "real time and date" circuit for the reverse analysis of the measured values and detecting the person guilty of exceeding some of the set limits ; rotation speed can be measured without the necessity of installing a sensor, e.g. by connecting to the ignition unit or external sensor ; incorporates inputs for the low and high alternating current and direct-current positive pulses; incorporates two inputs for connecting with the ignition switches for the function of detecting the low rotation speed; high-precision measurement; simple two-button control using the nav-menu; history of the measured values with use of the SchecK® method;and user-programmable external button for the quick selection of any function

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V ; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measurement: +/-1%(not including sensor accuracy); measuring range: 0 to 9999 1/min); resolution: 1 digit; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation ; load: +/-20 g ; vibration: 1 to 200 Hz ; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); inputs for RPM sensors: three wire, pick-up with low or high voltage; two status inputs of magnetos: LOW or HIGH (separate pole of switch reqired); internal speed sensor 0 to 450km/h (240 knots) for calculate flying time (version SAS); starter lock signal: grounded, max. 0.5Amps (external relay required);and communication line with a PC via standard RS-232c.
 

FEATURES:Display immediately the maximum acceleration reached, by pressing the external button; using your PC, download at any time the history of the measured values including symbols, which can be recorded into your log by pressing the button. Connect your 'G' Accelerometer to the output of the signalisation unit, which will warn you of the exceeded acceleration limits. Connect your 'G' Accelerometer with the Intercom using the iFamily® Bus and gain the option of having a voice alert of the exceeded limits. You can, at any time, download the latest version of the firmware to your instrument. You have the otpion of ordering the Accelerometer with an internal air speed sensor which enables monitoring 'g' acceleration and speed at the same time. Incorporates an input for the external button that, when pressed, records a symbol into the log, e.g. before an acrobatic element. Enables the connection of a landing gear switch for the control of recording. Simple two-button control using the nav-menu; history of the measured values with use of the SchecK® method; and user-programmable external button for the quick selection of any function.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measurement: +/-1%(not including sensor accuracy); measuring range: +/- 20g; resolution: 0.1g; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); internal speed sensor 0 to 450km/h (240 knots) for recording control (version SAS); output status signal: grounded, max. 0.5Amps; and communication line with a PC via standard RS-232c.
 

FEATURES: Display immediately the maximum height reached etc., by pressing the external button;using your PC, download at any time the history of the measured height values from the Altimeter; connect your Altimeter to the output of the signalisation unit, which will warn you of the exceeded height limits. Connect your Altimeter with the Intercom using the iFamily® Bus and gain the option of having a voice alert of the exceeded limits. You can at any time download the latest version of the firmware to your Altimeter. Displays in meters and feet; output for mode C transponder; STROBE signal for enabling the data output; high-precision measurement; simple two-button control using the nav-menu; history of the measured values with use of the SchecK® method. User-programmable external button for the quick selection of any function.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measurement: +/-1%(not including sensor accuracy); measuring range: -350m to 9700m (-1150ft to 31.950ft); resolution: 1m (3ft) - operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); encoder: MODE C with Strobe signal; and communication line with a PC via standard RS-232c.
 

FEATURES: Display immediately the maximum climb and descent rate reached, by pressing the external button; using your PC, download at any time the flight history from the Acoustic Vertical Speed Indicator (the climb/descent rate, including symbols and GPS positioning). You can at any time download the latest version of the firmware to your Acoustic Vertical Speed Indicator. This instrument is designed for all types of aircraft; incorporates two pressure sensors for optimising the climb and descent rate; switch for the quick selection of integration or averaging memory;incorporates an input from camera for recording symbols in the log (check point); incorporates an input for a switch enabling the recording of symbols in the log; incorporates an input for the detection of extending or using the engine (in case of motorized gliders); simple two-button control using the nav-menu; history of the measured values with use of the SchecK® method; and user-programmable external button for the quick selection of any function.

SPECIFICTIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measurement: +/-1%(not including sensor accuracy); measuring range: +/- 20 m/s (65.6ft); resolution: 0.05m (0.16ft); operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz - weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); input for sensors: active 0 to 5 Volts / passive 0 to 500 ohms; power for external speaker: 1W; communication line with a PC via standard RS-232c; and second communication line with a GPS via standard RS.
 

FEATURES: Display immediately the maximum values reached, by pressing the external button; using your PC, download at any time the history of the measured values from the Combined Engine Instrument; connect your Combined Engine Instrument to the output of the signalisation unit, which will warn you of the exceeded limits; connect your Combined Engine Instrument with the Intercom using the iFamily® Bus and gain the option of having a voice alert of the exceeded limits. At any time, you can download the latest version of the firmware to your instrument. Incorporates the "real time and date" circuit for the reverse analysis of the measured values and detecting the person guilty of exceeding some of the set limits. Measures EGT and CHT temperatures using the thermocouple sensors of the type K and J; easures the temperature of oil and water; measures the oil pressure using the resistive sensor or the sensor with the voltage output; measures the instant fuel consumption; high-precision measurement;and history of the measured values with use of the SchecK® method.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 200 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measurement: +/-1%(not including sensor accuracy); resolution: 1°C (33.8°F), 0.1 bar (1.45PSI), 0.1 Liter/hour (0.26US-Gallon), 0.1 Volts, RPM 1 digit; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 450 grams (0,99 lbs); dimensions: 85x85x65 mm (3.346x3.346x2.559 inch); diameter hole: 80 mm (3 1/8’’); EGT input for thermocouple probe: -40 °C to 1100 °C by environmental temperature 25 °C; CHT input for thermocouple probe: -20 °C to 800 °C by environmental temperature 25 °C; input for pressure sensor: active 0 to 5 Volts / passive 0 to 500 ohms; input for temperature sensors: PT-100 or VDO silver line with black isolator; input for flow sensor: HIGH level detected;and communication line with a PC via standard RS-232c.
 

FEATURES: Display immediately the minimum distances reached, by pressing the external button; using your PC, download at any time the history of the distances from the surrounding aircraft, including the ALPHA/CHARLIE mode; connect your Anti-collision Instrument to the output of the signalisation unit, which will warn you of approaching other aircraft. Connect your Anti-collision Instrument with the Intercom using the iFamily® Bus and gain the option of having a voice alert of approaching other aircraft. You can at any time download the latest version of the firmware to your instrument. It has two receivers for receiving signal; programmable zoom for monitoring the traffic; simple two-button control using the nav-menu. History of the measured values with use of the SchecK® method and user-programmable external button for the quick selection of any function. Designed for all type of aircraft.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); and communication line with a PC via standard RS-232c.
 

FEATURES: By using your PC, download at any time the history of the flight; connect your Autopilot into the output of the signalisation unit, which will warn you in case of danger that the Autopilot is disconnected. Connect your Autopilot with the Intercom using the iFamily® Bus and gain the option of having a voice alert of the course change, emergency disconnection of the Autopilot etc. You can at any time download the latest version of the firmware to your Autopilot. The instrument has three buttons for enabling or disabling the directions (yaw, pitch, roll), which shall be controlled by the autopilot. Controlling the pitch axis is also enabled by an electric trim on the elevator. Additionally, this unit measures the static pressure for keeping the constant altitude; communicates with the GPS in NMEA or ARNAV format for keeping the trace. Keep a history of the measured values with the use of the SchecK® method.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; backlights internal or external: 5V, 12V or 24V; current consumption: 50 to 350 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measure range of the altitude sensor: -350m to 9700m (-1150ft to 31.950ft); maximum angular speed rate for all directions: 150°/1s; resolution: 1m (3ft) / 1°; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz - weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); diameter hole: 57 mm (2 1/4’’); communication line with a PC via standard RS-232c; and second communication line with a GPS via standard RS-232c.
 

FEATURES:Monitor the operation of the Fatiguemeter with use of the control lamp on the instrument panel; using your PC, download from your Fatiguemeter, at any time, the history of the measured values including symbols. Connect the Fatiguemeter into the output of the signalisation unit, which will warn you of the exceeded limits; connect your Fatiguemeter with the Intercom using the iFamily® Bus and gain the option of having a voice alert of the exceeded values. You can at any time download the latest version of the firmware to your Fatiguemeter. This instrument has been designed for all types of aircraft ideal for installing into the centroplane of the aircraft or into the critical points of the construction. It measures 'g' acceleration and air speed, which is also recorded in the memory of the instrument. It has two types of memory for recording the history of the acceleration values and the matrixes of frequency; incorporates an input for the Marker switch that, when pressed, records a symbol into the log, e.g. before an acrobatic element. Enables the connection of an external speed pressure sensor; high-precision measurement; and maintain a history of the measured values with use of the SchecK® method.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; current consumption: 50 to 250 mA @ 14 Volts; maximal voltage and signal current: 30 Volts, 1 Ampere; measurement: +/-1%(not including sensor accuracy); measuring range: +/- 20g - resolution: 0.1g; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 250 grams (0,55 lbs); dimensions: 71x67x45 mm (2.795x2.637x1.771 inch); internal speed sensor 0 to 450km/h (240 knots) for recording control (version SAS); output status signal: grounded, max. 0.5Amps; and communication line with a PC via standard RS-232c.
 

FEATURES: Transfers the data from your instruments by the TCP/IP protocol directly to your PC; designed for all types of aircraft; meets all standards for the connection to the GSM/GPRS network according to the IEC. Transfers SMS messages to a mobile phone to inform on the battery condition; transfers SMS messages to a mobile phone to inform on the condition of the board systems; transfers SMS messages to a mobile phone to inform on the aircraft temperature; and transfers SMS messages to a mobile phone to inform on the aircraft position etc.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; current consumption: 5 to 1.500 mA @ 14 Volts; frequency: EUROPE 900/1800MHz or USA 1900 MHz; alarm signal active to the aircraft ground; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation ; load: +/-20 g; vibration: 1 to 200 Hz; weight: 200 grams (0,55 lbs); dimensions: 100x60x35 mm (3.937x2.362x1.377 inch). Price includes antenna.
 

FEATURES:Display immediately the maximum 'g' acceleration reached, by pressing the button on the Display unit; display immediately the Air speed by pressing the button on the Display unit; display immediately the time to TBO by pressing the button on the Display unit; display immediately the SMS from the aircraft producer by pressing the button on the Display unit. By using your PC, download at any time the history of the measured 'g' acceleration from the Structural life-monitoring unit; connect the Display unit to the output of the signalisation unit, which will warn you of the exceeded 'g' acceleration limits. Connect your Structural life-monitoring unit with the Intercom or Voice module using the iFamily® Bus and gain the option of having a voice alert of the exceeded limits. The latest version of the firmware is automatically downloaded from the server of TL elektronic.

Other features noteworthy: designed for all types of aircraft; measures the stress in the critical places of the aircraft structure etc.; incorporates aircraft service records - so-called service book; enables the wireless remote control of the aircraft starter or the magnetos, e.g. in case of a theft. In addition, the unit enables wireless downloading of the firmware to the instrument according to requirements, e.g. an aircraft manufacturer or an IT office. You will be informed of the whole aircraft operation, 'g' spectra cumulatively written in the 'two-parametric' form; ability to provide strain-gauge measurements and fatigue evaluation according to the measured stress. High-precision measurement; 100 hour memory with 100 SchecK® drawers and 100 Line.

SPECIFICATIONS: Voltage: 10.0 to 32.0 Volts; current consumption: 5 to 1.500 mA @ 14 Volts; frequency: EUROPE 900/1800MHz or USA 1900 MHz; alarm signal active to the aircraft ground; maximal voltage and signal current for locking relay: 30 Volts, 1 Ampere; measurement: +/-1% - measuring range: +/- 20g; resolution: 0.1g; operating: -20°C to 70°C (-4°F to 158°F) temperature range; relative humidity: 95% without condensation; load: +/-20 g; vibration: 1 to 200 Hz; weight: 450 grams (0,99 lbs); dimensions: 150x100x50 mm (5.905x3.937x1.968 inch); internal speed sensor 0 to 450km/h (240 knots); output status signal: grounded, max. 0.5Amps; and communication line with a PC via standard USB2.0.