MGL AVIONICS XTreme full featured instrument series include an Electronic Flight Instrument System (XTreme-EFIS) with navigation/autopilot capabilities and anEngine Monitoring System (XTreme-EMS). Their light weight, small size and high level of functionality makes them an excellent choice for use in non-certified aircraft. Both instruments fit a standard 3 1/8” (80mm) instrument panel hole. All information is displayed in an easy to read format on a high resolution wide viewing angle 4.3” sunlight readable color display. The XTreme-EFIS includes all the functions of the XTreme-EMS version. It a compact, multifunction electronic flight information system intended as a main flight instrument in smaller aircraft or as a backup/secondary flight instrument in larger aircraft. It integrates all the necessary functionality to replace several flight and engine monitoring instruments.The XTreme-EMS is a compact universal engine monitor replacing several engine monitoring instruments. All engine sensors are connected to a RDAC (Remote data acquisition unit) normally mounted behind the aircraft firewall. A simple CAN communication link is then necessary to connect the XTreme-EMS to the RDAC.
MGL AVIONICS XTreme full featured instrument series include an Electronic Flight Instrument System (XTreme-EFIS) with navigation/autopilot capabilities and anEngine Monitoring System (XTreme-EMS). Their light weight, small size and high level of functionality makes them an excellent choice for use in non-certified aircraft. Both instruments fit a standard 3 1/8” (80mm) instrument panel hole. All information is displayed in an easy to read format on a high resolution wide viewing angle 4.3” sunlight readable color display. The XTreme-EFIS includes all the functions of the XTreme-EMS version. It a compact, multifunction electronic flight information system intended as a main flight instrument in smaller aircraft or as a backup/secondary flight instrument in larger aircraft. It integrates all the necessary functionality to replace several flight and engine monitoring instruments.The XTreme-EMS is a compact universal engine monitor replacing several engine monitoring instruments. All engine sensors are connected to a RDAC (Remote data acquisition unit) normally mounted behind the aircraft firewall. A simple CAN communication link is then necessary to connect the XTreme-EMS to the RDAC. XTREME EFIS The XTREME EFIS is a full featured Electronic Flight Information System and Engine Monitor all wrapped up into a compact instrument that fits a standard 3 1/8" instrument hole. The XTreme has a high resolution, wide viewing angle 4.3" sunlight readable (600nits brightness) display. It includes a GPS receiver that is used to provide ground speed and range information, as well as a backup/control for the AHRS. If you do not select the SP-4 attitude sensor, you can still have a GPS-derived bank angle display. XTreme can be used as a Primary EFIS, Backup EFIS, Engine Monitor or EFIS/Engine Monitor. Basic GPS navigation (waypoints, routes, CDI (no moving map)), and Internal Autopilot capabilities are also included (just add servos and connection module). XTREME EFIS Features: Alarms on most displays Programmable maintenance timer for scheduled routine engine maintenance Programmable airframe timer for scheduled airframe maintenance. Records maximum and minimum values of most displayed values Built in black box recorder – records all flight data, engine, attitude and GPS data to SD card. Data can be exported to Google Earth, Microsoft Excel, etc. Includes a 1000 entry automatic flight log (Records start date&time, flight time, pilot number, Hobbs time, maintenance time, max altitude, airspeed and VSI reached during the flight) User configurable start up (Splash) screen Unlimited configurable checklists Unlimited configurable graphic information displays Automatic or manual local magnetic variation Dual menu system for quick item selection and user setups Sunrise/Sunset calculator Firmware upgrades via SD Card 3 year limited warranty (MGL Avionics US) XTREME EFIS Specifications: Powerful ARM processor 4.3” high resolution 480x272, sunlight readable, wide viewing angle, 600 nits TFT LCD display LED backlight (brightness can be adjusted for low light flying conditions) Fits standard 3 1/8” aircraft instrument panel hole SD Card interface for data recording, user splash screens, checklists, graphic information pages, firmware upgrades etc 1/8” NPT female fittings for Altitude and Airspeed pitot tube connections 1x RS232 communication port 1x MGL Avionics Airtalk communication port 1x MGL Avionics RDAC communications port 1x CAN communication port Rotary control plus 5 independent buttons for easy menu navigation and user input External alarm switch output for an external indicator lamp etc Built in 50 Channel GPS receiver with over 1 million effective correlators with high immunity to jamming Time To First Fix (TTFF) of less than 1 second External active GPS antenna connection Support for an internal or an external GPS receiver Built in RTC (Real Time Clock) Wide input supply voltage range of 8 to 30V DC Built in voltage reversal and over voltage protection for harsh electrical environments Light weight design XTreme can be configured as a PFD (with AHRS sensors added), and/or an engine monitor (with RDAC added). See below respective EFIS and Engine Monitor functions and accessories required. EFIS Functions: Attitude display. Note (1) Magnetic heading indication. Note (2) Heading bug Precision altimeter from –1000ft up to a maximum of 30 000ft (-304m to 9144m). Altitude can be displayed in ft or m Altitude bug Airspeed indicator (16mph to 250mph), 1mph resolution. Airspeed can be displayed in mph, km/h or kts Digital VSI indicator (+/-20 ft/min to +/-10 000 ft/min) and analog VSI indicator (+-2000 ft/min range). VSI can be displayed in ft/min or m/s. Serial Altitude encoder output via a RS232 port Density altimeter OAT (Outside Air Temperature) display using an external OAT probe Supply Voltage display Stopwatch timer Automatic flight timer RTC (Real Time Clock) Glide and climb ratio indicator Barometer (actual local pressure) TAS (True airspeed) display G-Force indication. Note (1) Wind speed and wind direction indication. Note (2) Turn Indicator. Note (1) Slip/Skid indicator. Note (1) GPS flight path (GPS calculated bank and pitch angles). Note (8) Waypoint navigation Nearest waypoint display 1 or 2 axis AutoPilot (Notes 1 & 11) Engine Monitoring Function: 1x Engine RPM 1x Rotor RPM. Note (5) 1x Manifold pressure. Note (6) 1x Oil pressure input 1x Oil temperature input 2x Auxiliary analog channels (Pressure/Temperature/Current) 12 Channel EGT/CHT display 1x Fuel Flow Note (7) 2x Fuel Level Programmable maintenance timer for scheduled routine engine maintenance Engine display screens are automatically configured to optimize screen space depending on what parameters are been displayed Settable Hobbs meter (password protected) Fuel range / endurance based on TAS or GPS ground speed Supply Voltage display Current monitor to measure charge/discharge currents. Note (4) Engine leaning feature Notes: (1) Requires optional MGL Avionics AHRS sensor unit (SP4/SP5/SP7) (2) Requires optional MGL Avionics compass sensor unit (SP2/SP6) (3) Requires optional MGL Avionics RDAC unit (4) Requires optional MGL Avionics current monitor sensor (5) Requires RDAC with Rotor RPM input (RDAC-XF) (6) Requires RDAC with Manifold Pressure sender (RDAC-XFM) (7)Two Fuel Flow displays if RDAC with two Fuel Flow inputs (8) Valid ONLY in coordinated flight (9) Requires Vertical Power VP-X Generation 2 unit (10) Requires CO Guardian Aero-452 CO monitor unit (11) Requires MGL servomotor(s) XTREME EMS The XTreme EMS is based on a 4.3" sunlight readable, wide viewing angle, high resolution LCD display. It integrates an SD card reader (for software updates and for engine data recorder), 5 function buttons, a rotary control. It can be connected to standard MGL Avionics RDAC (engine monitor) boxes (required). The XTreme EMS is designed to fit a standard 3 1/8" round instrument hole. The body is located off-center allowing the unit to replace instruments on the right side of a standard 6-pack configuration or any other location that currently occupies two instruments. Due to the light weight and very low mounting depth no complicated mounting brackets or trays are needed. Power use is low and operation from much less than 12V to around 28V is fully supported XTREME EMS Hardware Features: Powerful ARM processor 4.3” high resolution 480x272, sunlight readable, wide viewing angle, 600 nits TFT LCD display LED backlight (brightness can be adjusted for low light flying conditions) Fits standard 3 1/8” aircraft instrument panel hole SD Card interface for data recording, user splash screens, checklists, graphic information pages, firmware upgrades etc 1x RS232 communication port 1x MGL Avionics Airtalk communication port 1x MGL Avionics RDAC communications port Rotary control plus 5 independent buttons for easy menu navigation and user input External alarm switch output for an external indicator lamp etc Built in 50 Channel GPS receiver with over 1 million effective correlators with high immunity to jamming Built in RTC (Real Time Clock) Wide input supply voltage range of 8 to 30V DC Built in voltage reversal and over voltage protection for harsh electrical environments Light weight design XTREME EMS Engine Monitor Features: 1x Engine RPM 1x Rotor RPM (Note 3) 1x Manifold pressure (Note 4) 1x Oil pressure input 1x Oil temperature input 2x Auxiliary analog channels (Pressure/Temperature/Current) 12 Channel EGT/CHT display 2x Fuel Flow 2x Fuel Level Programmable maintenance timer for scheduled routine engine maintenance Engine display screens are automatically configured to optimize screen space depending on what parameters are been displayed Settable Hobbs meter (password protected) Fuel range / endurance Supply Voltage display Current monitor to measure charge/discharge currents. (Note 2) Engine leaning feature
MGL-XTREME-EFIS
Data sheet
Certification/Approval
Certificate of Conformance
Taric
8803300010 Other parts of aeroplanes or helicopters for use in civil aircraft
KANARDIA INDU Series round altimeters are part of INDU diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters. They feature colour LCD display, one or two pointers with possibility to personalise scales (in feet or meters) and LCD displays. They are offered as standalone (master) altimeters with internal pressure sensors or as slave instruments. The slave version requires some PFD like KANARDIA NESIS, EMSIS, AETOS or HORIS to be present on the CAN bus. KANARDIA INDU Series round altimeters are available for two standard panel hole diameters of 57 mm (2.25") with one pointer and 80 mm (3.15") with two pointers. They can also be ordered with integrated backup battery at additional cost. The backup battery can also handle and additional indicator, typically an airspeed indicator.
OMRON A16 series pushbutton 16-dia. cylindrical body switches are detachable switches. The same contacts can be used for both standard loads and microloads. Their miniature design of 28.5 mm makes these switches the smallest class in the industry. Easy-to-wire terminal arrangement. Certified for EN 60947-5-1. These switches are offered in lighted and non lighted versions, different colors, display shapes, with LED or incandescent lamps and different socket units. Please consult the attached documentation for ordering.
UMA 2-1/4" electric tachometers with their high resolution and easy to read displays were designed to offer aviation styling and performance for all types of aircraft. The analog model has a 270° sweep which provides great resolution in both the 3500 and 7000 ranges. The digital model has a bright LED display. Separate power source required. Installation is simple and instructions are included. They can replace mechanical tachometers in Lycoming/Continental engines.
Current: 80 milliamps Size: 2.25" round x 2.75"deep.
The PAI-700 TSO'd Vertical Card Compass is manufactured exclusively by Precision Aviation, Inc. This non-liquid (dry) type compass is magnet driven thus it is subject to lead and lag, however, these tendencies are greatly reduced due to the absence of pendulosity. It is inherently stable due to the use of eddy current damping which is a natural phenomenon built into the basic design and as such has no overshoot. The PAI-700 has been designed to replace the float/liquid type compasses eliminating leaking fluid or backward azimuth readings. Available for Southern and Northern Hemisphere and different supply systems (5V, 14V and 28V). Precision Avionics Inc. also manufactures different compass brackets for overhead or glare shield mounting.
The Precision PAI-700 Vertical Card Compass consists of a 2" vertical rotating dial which is compared with a fixed miniature airplane (lubber line) to present the magnetic heading of the aircraft at all times. Heading information is more natural because the heading is read at the12 o'clock position and off the nose of the miniature aircraft. The compass card rotates and presents all quadrants in their true relation to line of flight. Requires no power (except for lighting) to operate. Installed in many current production aircraft & helicopters. Size: 2-7/8"H x 2-3/8"W x 2-1/8"D. Wt. 0.6 lb. After installing compass must be compensated using standard compensation procedures. Also used in sailplanes.
Note: Compass deviation card is included. A mount, sold separately, is required for installation with the unit.
DAVTRON M301 Series Outside Air Temperature (OAT) digital indicators are FAA-PMA approved and come complete with digital probe, in Fahrenheit or Celsius models and different versions. They require minimum panel space. Other features include: light weight, automatic dimming, miniature remote probe, sunlight readable display and a laser engraved faceplate. A 3-pin connector is installed on probe as an option for an additional charge.
UMA NON TSO'd mechanical manifold pressure gauges (MPGs) are offered in two series, the conventional 2-1/4" manifold lightweight gauges with a slim design and a single diaphragm and the newer 3-1/8" and 2-1/4" gauges which incorporate a dual diaphragm design improving the longevity and reliability of the instrument. Standard markings are black and white while optional color markings can be ordered. Cases are from cast aluminum or Valox 420 plastic depending on model selected.
UMA Non FAA Approved standard 2-1/4" and 3-1/8" altimeters are high quality, simple type (single pointer) with 2 revolution dial, designed to meet the needs of the low cost non-IFR users. Both altimeters utilize a knob adjustable barometric in. Hg scale, viewed through a Kollsman Window.
KANARDIA INDU Series round Vertical Speed Indicators (Variometers) are part of INDU diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters. They feature an LCD display with possibility to personalise the displays and scales. They are offered as standalone (master) VSIs with internal pressure sensors or as slave instruments. The slave version requires a master altimeter or some PFD like KANARDIA NESIS, EMSIS, AETOS or HORIS to be present on the CAN bus. KANARDIA INDU Series round altimeters are available for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15").
SCINTEX complete kit with digital gauge and dual flow meters enabling monitoring of the engine's supply and return lines. It comes with 2 fittings for each flow meter (to be specified at the time of ordering) and clamps. For installation wiring between the flow meters and the display unit is required (not included). This kit is intended for use in vehicles, machinery, generators and boats / marine and other engine applications. The flow meters are precision cut from steel and aluminum and they are highly accurate, repeatable and suitable for use with diesel, biodiesel, unleaded petrol and other fuels. The display unit is a 1.8”, high resolution, sunlight readable, wide viewing angle, LCD colour display with a completely sealed and waterproof display front panel. The gauge enclosure is a common 52mm round size to fit many existing cutouts. Key features include highly accurate with good repeatability displays consumption in Litres per Hour or other units, fuel remaining in up to 2 tanks, connection capabilities to a NMEA enabled RS232 GPS receiver, one or two fuel flow senders and fuel level senders and a single fuel pressure sender and display. It can be powered by 12V - 36V power supplies. Please refer to the additional information and specifications provided or contact us.
Amphenol MS MIL-C-5015 Circular Plug Connectors are designed to meet the demanding performance requirements of military standards. These cable mount circular plug connectors have proven electrical capability for equipment applications where durability is important. The Amphenol plugs have threaded couplings and single key/keyway shell polarization for an accurate and reliable connection. The solid shells of these MS Series circular MIL-C-5015 connectors are made from high grade aluminium alloy. The shells are electrically zinc plated with an olive drab chromate finish which ensures a high resistance to corrosion. The inserts of these military circular connectors are made from resilient synthetic rubber which offers a high dielectric strength and resistance to vibration.
The MS3106A-10SL-3S plug can be used with Turn Coordinator TC02E-3-2 or Turn & Bank Indicator TB02E-2-1.
RS FLIGHT SYSTEMS develops and manufactures avionics for general aviation and flight test equipment. RS FLIGHT SYSTEMS range of avionics includes Engine Management Units for Rotax 912 iS / 915 iS engines, engine panels, automatic propeller speed control unit (SCU), and SCU front panel, iS Data Recorder for Rotax iS engines (912iS / 915iS / 916iS), control panels, portable test bench for independent drive of BRP Rotax iS engines, real-time wind indication system, Fly by wire control sticks, CANaerospace based flight test instrumentation and more.
The RS FLIGHT SYSTEMS 2nd generation ROTAX® 912iS/915iS Engine Management Units (EMU) include 2 cockpit mounted engine monitoring, data logging & propeller control devices, EMU 912iS evo & EMU 9xiS. Both feature the same hardware, software and functionality but differ in dimensions and weight. They integrate seamlessly into the Rotax 912iS/915iS engine wiring harness, providing indications of all available engine parameters, engine status, ECU faults and additional sensor inputs. Suitable for 14 V and 28 V aircraft electrical systems with minimum installation effort. Configurable for use with different unit systems. Additional features: sunlight-readable backlit display, dual optically isolated CANaerospace data bus interfaces for retained redundancy, continuous monitoring and health checking of both ECU display buses, georeferenced data recording of all parameters at 10 Hz over up to 2,000 hours, simple data transfer & software update via an integrated memory card slot, sophisticated visualization & processing tool for recorded data, Google Earth file export of recorded data inc. GNSS and engine data. Wiring Harness Kit (incl. power supply wires) is also available (sold separately). A separate module (sold separately) provides connection to 912/914 carburetor Rotax engines.
For more information on RS FLIGHT SYSTEMS products please consult the Product Description section and the supplied documentation.
UMA line of precision electronic pressure senders feature precision, solid state sensors and circuitry to give unequalled performance and are designed for rugged use in just about any environment. They are offered in TSO'd and Non TSO'd models and gauge, differential and absolute types. UMA TSO'd electronic pressure senders are the most economical TSO’d units on the market. They are compatible with avgas, jet fuel, engine oil and many other fluids. Because they have internal voltage regulation, they are compatible with indicating instruments that do not have precision output voltages. Units for fuel and oil pressure are certified under TSO C47. Units for manifold pressure are under TSO C45a. For additional information please refer to the attached documentation.
HONEYWELL BENDIX KING® KA 51B is a slave meter used in the KCS 55A compass system. Displays slaving error between the KMT 112 flux valve and KI 525A pictorial navigation indicator by means of small meter movement.
The SIRS "Navigator" magnetic compass delivers extremely accurate readings due to its fully integrated, 4 magnet correction facility. It has the same features as the "Pegasus", but is mounted with a fully adjustable bracket that allows attachment to a variety of positions including the glare-shield or the windshield. This allows the compass to be located away from magnetic influences. Available in different versions for Northern or Southern hemisphere, unlighted or lighted 12/28V and has a 3-year warranty. Size: 203/8" H x 2-1/4" W. Product accessories such as installation kit, GS1 glareshield mount, SIRS MF1 short foot bracket and SIRS compass correction key are also available and sold separately.
WULTRAD INC. is a manufacturer of non-certified flight and engine instruments under FALCON GAUGE brand for experimental and homebuilt aircraft. Although their products are Non-TSO, they are made to TSO or MIL specifications for quality.
FALCON GAUGE Electrical Attitude Gyro is intended for use in experimental aircraft only. It provides a continuous visual display of the aircraft attitude with respect to the earth for maneuvering around the longitudinal (pitch), and lateral (roll) axes, and yaw. A precision AC brushless motor is featured in the electrical attitude gyro. The Power failure drops into view whenever the power is insufficient for operation of the gyro. Electrical gyro can be caged by pulling the "Pull to Cage" knob. It is offεred with or without internal lighting and is designed to work with a 12V system. Dimension: 3-3/8"X 6.46/164mm.
The FAA TSO'd RCA26AK (14V) and 26BK (28V) series of electric attitude indicators (artificial horizons) by KELLY MFG (RC ALLEN) are known for their dependability and ruggedness. They incorporate tremendous advances in presentation, precision, and reliability.With a proven track record for dependability and ruggedness, the attractive new extended color schemes and ultra-precise spherical presentation (eliminating old parallax problems) they set a new standard for safety.These gyros provide a more accurate IFR reference for the beginning instrument pilot or a Cat II captain. A new three phase motor/inverter is designed into the gyro enabling it to operate at lower temperatures which extends to useful life. The instruments employ a new, high precision air erection system which provide erection torque for maintaining a proper vertical alignment reference. The erection air is supplied by a turbine pump which is integrally coupled with the gyro motor. Through maximum utilization of unitized construction the design is free of resonant frequencies below 100 HZ and thus cannot respond to low frequency disturbances which can cause dither and premature wear out of the unit. The display portion of the instruments has a directly coupled roll movement, and a pitch movement mechanism identical to that of the field proven vacuum gyros produced by R.C.Allen since 1966. A "pull to cage" spring type force limited mechanism assures immediate alignment and stability whenever power has been applied to the gyro, a feature non-existent on vacuum driven gyros. These artificial horizons have a hybrid inverter which converts the aircraft DC power to the required voltage and frequency for motor operation. All units have a pull cage knob and a power failure flag that drops into view whenever the supply voltage is lost or when the voltage has dropped below a level of acceptable for proper operation of the gyro. Slip indicator can be added to satisfy FAA AC91-75 upon request. Available in 14V or 28V voltage versions with fixed or movable pointer, lighted or unlighted, power failure flag, panel tilt and optional inclinometer. Mating connector MS3116E8-4S and panel screws are now included with each new instrument at no extra charge.
RAY ALLEN (RAC) R2S Rocker Switch provides a very positive snap action in 2 directions and returns to a center off position. It was designed specifically for Ray Allen trim systems. It is wired to connect both power leads to ground when the rocker is released. This eliminates motor coasting and allows very precise trimming. The RS2 switch is rated at 1amp. The faceplate measures 1.75" (44mm) x 1.0" (25mm) x 1.47" (37mm) deep. Self adhesive labels are not included. Sold separately.
The RAY ALLEN (RAC) RP4 LED position indicator is designed to be installed in the cockpit providing an indication of the servo output shaft position. This indicator supercedes and it is a direct replacement for previous RAC RP3. The RP4 indicator uses ten LED lights to show the position of a actuator output shaft (or position sensor arm). There are also two amber colored LED's, one on each end of the indicator scale, to act as a reference for the green indicator light, especially in dark conditions. The 10 LEDs are the brightest available for superior visibility in sunlight, but can be dimmed for night flight. It can be installed horizontally or vertically.
The RAC RP4 position indicator is panel mounted using a faceplate and two countersunk, 2-56 x 7/16" screws (two spare finishing screws are included). The distance between the screw holes is identical to the older Ray Allen RP3 LED indicator. Although the faceplate dimensions are identical between the RP3 and RP4 indicators, the panel cutout size is slightly different between the RP3 and RP4. If you are replacing and older unit with a new RP4, you will only need to increase the size of your panel hole. The RP4 faceplate will cover the older RP3 panel hole.The RP4 faceplate measures 1.75"(45 mm) X .75"(19 mm) and it is 1.6"(41 mm) in depth. It is now the standard position indicator included in Ray Allen trim systems, or can be purchased separately for special applications such as a cowl or wing flap indicator.
The RP4 includes a RP4-L1 label (featuring Elev1, Elev2, Ail, Rudder, Flaps). A RP4-L2 label (featuring Cowl Flaps, < >, on/off) is also available and is sold separately.
NOTE: Labels can only be ordered together with . In ordering these high quality labels please be advised that rocker switches and needle indicators require a large label, LED indicators use a small label. Can be only included in orders of respective RP4 position indicator(s) (not separately).
MGL AVIONICS XTreme full featured instrument series include an Electronic Flight Instrument System (XTreme-EFIS) with navigation/autopilot capabilities and anEngine Monitoring System (XTreme-EMS). Their light weight, small size and high level of functionality makes them an excellent choice for use in non-certified aircraft. Both instruments fit a standard 3 1/8” (80mm) instrument panel hole. All information is displayed in an easy to read format on a high resolution wide viewing angle 4.3” sunlight readable color display. The XTreme-EFIS includes all the functions of the XTreme-EMS version. It a compact, multifunction electronic flight information system intended as a main flight instrument in smaller aircraft or as a backup/secondary flight instrument in larger aircraft. It integrates all the necessary functionality to replace several flight and engine monitoring instruments.The XTreme-EMS is a compact universal engine monitor replacing several engine monitoring instruments. All engine sensors are connected to a RDAC (Remote data acquisition unit) normally mounted behind the aircraft firewall. A simple CAN communication link is then necessary to connect the XTreme-EMS to the RDAC.