These UMA new manufacture NON TSO'd electric ammeters offer accuracy, rugged construction, and contemporary styling. They are available in different  measurement ranges with a 270° sweep and are suitable for installation in 2-1/4" panel hole diameters. Made in U. S. A. and furnished with shunt.

The STRATOMASTER VEGA range instruments/indicators from MGL AVIONICS includes different 2 1/4" (57mm) microprocessor based color display instruments operating over a wide supply voltage range of 8 to 30V DC with with built in reverse and over voltage protection. They are non certified and only suitable for installation in experimental and sport  (LSA) aircraft. Using a high resolution color graphics display, these instruments/indicators provide excellent daylight readability with built in backlighting making them easy to read at night time. They include a rotary control plus 2 independent keys for easy menu navigation and to access specific instrument features. Sensors are also offered to enhance their functionality. The MGL AVIONICS STRATOMASTER VEGA Series instruments/Indicators include: Artificial Horizon & Magnetic Compass Display, Altimeter/VSI, ASI, ASI/VSI, Engine Monitoring System (EMS), Fuel Computer, Information Display, Manifold Pressure, Température, RPM, Hobbs, Universal Engine/Rotor RPM, Hobbs, 4-Channel Thermocouple (EGT/CHT), 4 Channel Universal Analog Input (Pressure/Temperature/Voltage/Current) and NAVCOM Control head for MGL N16 NAV/COMM or V16 COMM VHF.

The 730/830 Engine Monitoring Systems (EDM) from JP INSTRUMENTS revolutionize engine monitoring by the compact size integration of a full color graphical LCD display with the extremely popular EDM 700/800 series functionally. Both 730 and 830 EDMs feature: colourful graphics, larger data display for easy reading, parameters in full colour, annunciation of exceedances, less page swapping, more data per page. The units are "Plug and Play" compatible with existing EDM-700/800 units. Oil pressure has also been added to the entire EDM series line.  Both 730 and 830 are FAA approved for use as secondary engine monitors. However they CANNOT BE USED as a replacement for primary gauges which have to be maintained. Different options and accessories are also available at additional cost.

HONEYWELL BENDIX KING® manufactures a range of TSO'd VOR/LOC/Glidescope indicators. These navigation instruments include VOR/LOC left-right needles, To-From indicator, VOR/LOC warning flag, glideslope deviation needle, glideslope warning flag and 30Hz OBS resolver. Depending on the model, the feature rectilinear instead of pendulum type meter movements for more precise indicator readings, 14/28 volt internal lighting, metal bezel with glass lens and course datum synchro for autopilot use.

These indicators are commonly used with BENDIX KING® remote mounted VOR/LOC converters such as KN-72 or KN-77, remote mounted Glideslope Receivers such as KN-73 or KN-75, KNS-80, KNS-81 nav systems and KX-155/KX-165 NAV/COMM transceivers.

The KI203 model features an internal VOR/ LOC converter and it is compatible with the BENDIX KING® KX155 transceiver. It has a rectilinear meter movement. Compatible with the BENDIX KING KX155 NAV/COMM transceiver.

The KI 204 VOR/LOC/Glideslope Indicator features a built-in VOR/LOC converter and scallop rejection filter, rectilinear needle movement and an optically coated glass lens. Requires input from external glideslope receiver. Compatible with the BENDIX KING® KX 155 or KX 155A NAV/COMMs. Requires input from external glideslope receiver.

The KI 206 VOR/LOC/Glideslope Indicator is rectilinear and internally lighted. It is used with the KNS 80/81 units, KX 165  transceiver and the KNR 634 VOR/LOC/GS/MB receiver. It is available with course datum synchro.

The KI208 model features a built-in VOR/ LOC converter and it is compatible with the BENDIX KING® KX 155 or KX 155A NAV/COMMs. It has a  pivoted needle action and a plastic lens.

The KI209 model features an internal VOR/ LOC converter and it is compatible with the BENDIX KING® KX155 transceiver. It features a pivot needle action.  The KI209 model includes GPS interface capability.

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.

TSO'd Electronic Fuel Quantity gauges from UMA INSTRUMENTS (indicated by the letter "T" in the PN) are offered in 1-1/4 in. and 2-1/4 in. sizes for installation in respective panel hole diameters and mounted with (4) 6-32 screws. Smaller 1-1/4 in. instruments can be cluster mounted as close as 11/2” centers utilizing panel space without compromising readability. They can be powered from 14 or 28 volts. Signals are acquired from remote mounted sensors, processed and displayed on black analog dials with white easy to read markings indicating empty to full fuel level. Each gauge uses rugged aircore meter movement for vibration resistance and repeatability. Available in different versions based on their sender type and range. UMA sensors are sold separately.

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").

Scale Ranges:

-M scale in meters per second (-10, 10)

-FT scale in feet per minute (-2000, 2000)

-KTS scale in knots (-20, 20)

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.

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.

TSO'd Electronic Fuel Quantity gauges from UMA INSTRUMENTS (indicated by the letter "T" in the PN) are offered in 1-1/4 in. and 2-1/4 in. sizes for installation in respective panel hole diameters and mounted with (4) 6-32 screws. Smaller 1-1/4 in. instruments can be cluster mounted as close as 11/2” centers utilizing panel space without compromising readability. They can be powered from 14 or 28 volts. Signals are acquired from remote mounted sensors, processed and displayed on black analog dials with white easy to read markings indicating empty to full fuel level. Each gauge uses rugged aircore meter movement for vibration resistance and repeatability. Available in different versions based on their sender type and range. UMA sensors are sold separately.

The LXNAV G–Meter  (accelerometer) is a standalone unit, designed to measure, indicate and log g–forces. The unit is offered in 57 mm or 80 mm diameters for installation into the aircraft instrument panel. It comes in two versions, standard and with flight recorder (FR).

The LXNAV G–Meter has an integrated high precision digital pressure sensor and inertial system. The sensors are sampled more than 100 times per second. Real Time Data is displayed on a QVGA 320x240 pixel 2.5″ high brightness color display. To adjust values and settings the LXNAV g–meter has three push buttons with fixed functions. The top button is ESC (CANCEL), the middle is to switch between modes and the lower button is the ENTER (OK) button.

The unit's inertial platform integrates a  ±8g accelerometer. Device is showing current g–load in navbox/needle and it’s min-max values in bar. Last flight min/max load navboxes are persistent till next flight. Min/Max limits with Warning zones can be defined.

Real Time Data is displayed on a QVGA 320×240 pixel 2.5-inch high brightness color display.

The Logbook menu displays the list of flights. If the RTC time is set properly the take-off and landing time shown will be correct. Each flight item consists of the maximum positive g–load, the maximum negative g–load from the flight and the maximum IAS. This function is available only with “FR” version.

Product Features:

• An extremely bright 2.5″ QVGA color display readable in all sunlight conditions with the ability to adjust the backlight.

• Three push buttons are used for input.

• RS232 input/output.

• Micro SD card

• 320x240 pixels color screen for additional information such as minimum and maximum g–force

• Built in RTC (Real time clock)

• Logbook

• 100Hz sampling rate for very fast response.

• Power supply cable included

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).

KANARDIA INDU Series round Airspeed Indicators 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) IAS units 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"). As an option they can be ordered with an Outside Air Temperature (OAT) digital sensor at additional cost. When static pressure (altitude) is present on the CAN bus, OAT sensor enables also the TAS  as well.

Scale Ranges:

-KMH Scale in kilometers per hour (0-280)

-KTS Scale in knots (0-140)

-MPH Scale in miles per hour (0-150)

NOTES:

A high speed sensor option is also available at additional cost (up to 460 km/h, 250 kts, 285 mph)

Arc colors need to be specified  at the time of order.

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.

SWIFT AIRCRAFT manufactures Swift two-seater low wing composite aircraft with striking elliptical wings and double curvature surfaces. Comfortable, safe and environmentally sound they are designed and manufactured entirely in the UK, and available globally,

The company also manufactures Swift aircraft gauges specializing in precision-engineered gauges, including Exhaust Gas Temperature (EGT) and Cylinder Head Temperature (CHT) gauges, commonly used in aviation.

 Automatic flight control systems (AFCS) are aircraft autopilot systems with many integrated features initially found only on high-performance aircraft but nowadays installed on modern aircraft of any size. Their capabilities vary from system to system with some AFCS offering advanced features beyond ordinary autopilot systems regarding programmability, the level of integration of navigational aids, the integration of flight director and autothrottle systems, and combining of the command elements of these various systems into a single integrated flight control human interface.

LEONARDO HELICOPTERS provides aircraft manufacturers with solutions ranging from single axis or secondary flight control computers and electronics to complete integration of flight control systems. The flight control system architecture spans from simplest architecture, lowest complexity up to full authority fly-bywire architecture, offering the following advantages:

• Compatibility with various actuation technologies (Hydraulics, Mechanical, Electro-Mechanical)

• Eased certification process (EASA Form 1 already achieved)

• Reduced integration cost and schedule risk (building blocks)

The Flight Control Systems (FCS), used to control the control surfaces of the aircraft, are based on:

• Flight Control Computer (FCC)

• APSW (Autopilot).

• Building blocks of dual, dual-duplex, triplex and quadruplex FCS architecture. 

Apart from new, LEONARDO older FCS are also offered in NEW SURPLUS or USED conditions (Serviceable or Overhauled). For additional information please consult the supplied documentation or contact us.

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 offred with or without internal lighting and is designed to work with a 12V system. Dimension: 3-3/8"X 6.46/164mm.

HONEYWELL BENDIX KING® KNI-582 Radio Magnetic Indicator (RMI) provides bearing information to either ADF or VOR stations by means of two pointers each of which is read against compass card. The KNI-582 RMI requires inputs from ADF, HSI and NAV receivers and combines three data points on one indicator. The current aircraft heading from an HSI is shown on the card. The magnetic headings to VOR and NDB stations are shown by the twin needles. By combining all this information visually, less interpretation is required thus enhancing overall situational awareness, something especially helpful when the workload is high.

Product Features:

Dual pointer RMI

Accepts AC SIN/COS, DC SIN/COS, Serial, and VOR Composite inputs

Compatible with NAV Receivers such as KN-53, KNS-80, KNS-81, KX-155/165, KX-170B/175B, KNR-615, KNR-630, KNR-634, KNR-665, KNR-665A

Compatible with ADF receivers such as KR-85 (w/ KI-227 -01/04), KR-87, KDF-800/805/8000

Compatible with Compass Systems and NAV indicators such as KCS-305, KCS-55/55A, and KPI-550

Models available with 5 or 28 volt lighting 

Models available with black or gray bezel

TACAN compatible and night vision goggle versions available

TSO'd

Specifications:

Altitude: To 50,000 feet

Operating Temperature: -20 to +55°C

Weight: 3.0 lbs. (1.4 kg)

Power Requirements: 28V 4A / 26VAC 6VA

TSO Compliance: Env. Cat. RTCA DO-160A A1D1/A/SKP/XXXXXSABAAA; TSO C6c (compass); TSO C41c Class A (ADF); TSO C40a (VOR)

Compass Heading Input: Operates from any slaved magnetic compass with ARINC X,Y,Z outputs.

G-Meters (Accelerometers) by FALCON GAUGES measure G forces acting on the airframe during turbulent or aerobatic maneuvers. One pointer providess a continuous reading, the other two indicate maximum positive and negative loads. FALCON G-Meter models are mechanical and offer precision, accuracy, and durability. They are also easy to operate. No wiring necessary. The units come with the locking knob set to the locked position.  Do not press the reset button until after moving the locking knob to the unlocked position.

FALCON GM510-2 G-Meter is a standalone 57 mm (2 1/4") unit which fits a standard 2 1/4" instrument cutout.

Product Features and Specifications:

Product Features:

• G-Meter, -5 to +10 g

• Operation Temperature: -55º to +60°C

• Dimensions: 61 mm (2 1/4") x 61 mm x 108 mm (3.5")

• Complies with Standard : MIL-A-5885C

Note: FALCON GM510-2 G-Meter is currently not available. Availability in NEW condition depends on existing stocks and is limited.

ROTAX® aircraft  engines form part of the product portfolio  of BRP-Powertrain GmbH & Co. KG which develops and manufactures engines for snowmobiles, watercrafts, boats, roadsters, all-terrain and side-by-side vehicles, motorcycles, carts, and aircrafts.

BRP-ROTAX® product range includes certified and non certified internal combustion engines, parts and accessories for light and ultralight aircraft.

Fuel pressure gauges are used in BRP-ROTAX® aircraft engines and offered as certified or non certified parts from their respective manufacturers. Non certified parts can be used in ultralights or other aircraft not requiring certification of parts for their installation.

Aircraft engine  parts are subject to changes from time to time. Some parts may be no longer available or replaced by others with different part numbers. Listed BRP-ROTAX® engine parts do not imply their current availability or suitability for your engine application. Always consult the most recent Illustrated Part Catalogs (IPCs) or other documentation available from the manufacturer for the correct part number before ordering.

Fuel pressure gauges are no longer offered as ROTAX Part Numbers. These part numbers are provided for reference only. For these gauges please refer to our product presentation on AVIASPORT Fuel Pressure Gauges or contact us.