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.

The vertical speed indicator is a precision instrument which provides an accurate indication of rate of change of altitude. UNITED INSTRUMENTS TSO'd (TSO-C8b) 7000 Series vertical speed indicators (VSI) offer several configurations and have been selected as standard equipment by aircraft manufacturers worldwide for use in most production aircraft.. They are temperature compensated and provided with a zero adjustment screw on the face of the case in the seven oclock position. Power: Static system. Size: 3-1/8" x 3-1/8" x 4", Wt. 0.7 lb. Available in unlighted and lighted versions.

UMA Electronic Hydraulic Pressure Gauges are offered in TSO'd and Non TSO'd models and 1-1/4"  or 2-1/4" diameters to fit respective aircraft panel openings. They are housed in aluminium or Valox 420 plastic cases (depending on the model) and connect to  precision, high pressure transducers which mount directly to the aircraft's hydraulic system. Standard markings are black and white. Recommended for new design projects and applications. 

Note: Pressure Transducers (Senders) ARE NOT INCLUDED in the prices of the pressure gauges. They are sold separately and are not TSO'd.

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 MID CONTINENT® INSTRUMENT (MCI) 3" TSO'd Turn Coordinators are value priced  and engineered for reliability and a long service life. Depending on the model, they can be a direct replacements for most coordinators with 3-pin or 5-pin connectors. 

These instruments show  a standard 2 minute turn when balance ball reaches either side of display. MCI turn coordinators feature a HEA non-glare glass screen for easy readings, an operating range of temperatures from -30 to +50 deg. C and altitude-1000 to 35000 ft and they can operate on a voltage range from 10-32 VDC for convenience. Power consumption is 0.28 A. They can be front or rear panel mounted in a 3 1/8" hole. Dimensions: 3 1/4"X3 1/4"X5". Max Weight: 1.4 lbs. Available in lighted and unlighted versions. FAA TSO certified to C3b.

The “B” models are equipped with a proven AC rotor powered by a solid-state inverter, creating less heat behind the panel. Utilizing a brushless rotor design, these models exhibit top industry ratings of 4,800 hours MTBF. They are ideal for use in high performance aircraft and cold-climate applications.

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.

The AVIASPORT indicators (gauges) are reliable, accurate and solid, combining the accumulated experience of more than twenty years with the latest technology  They have been designed for ROTAX engines and their display areas are divided into red, green and yellow zones in line with Rotax limits. They use a pointer that turns 240º or 320º, providing high resolution. AVIASPORT range of gauges includes CHT, EGT, tachometers, oil and fuel pressure, oil and coolant temperature, fuel level, voltmeters & ammeters and offered with casings of different sizes: 80mm; 57mm and 52mm.

AVIASPORT Oil Pressure indicators (gauges) are designed specifically for ROTAX 912/914 aircraft engines with painted red, green, and yellow gauge markings. are available in two sizes: 52 and 57 mm. They are offered in two unit versions for readings in PSI or Bars. They work with different pressure sensors depending on these installed in ROTAX 912/914 engines: the VDO sensor (Before September 2008) or the 4..20mA sensor (after 2008).

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.

This 2-1/4 inch flap indicator uses a resistance potentiometer as a flap position sensor. Transmitter is required. Wt: 9.8 oz.

HONEYWELL BENDIX KING® KI-229 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 KI-229 RMI 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.

The KI-229 requires inputs from ADF, HSI and NAV receivers.

Product Features:

14/28 volt lighting

Compatible with Nav Receivers such as KN-53, KNR-615, KNR-630/631/632/633, KNR-634, KNR-665, and KNR-665A

Compatible with Nav systems including RNAV such as KNS-80 and KNS-81

Compatible with ADF receivers such as KR-87 and KDF-806

Compatible with Compass systems such as KCS-305 and KCS-55/55A

Requires input ARINC Compass System

TSO'd

Product Specifications:

TSO Compliance: Env. Cat. RTCA DO-160A A1C1/A/SKP/XXXXXXA/B/AAA

Weight: 2.8 lbs. (1.3 kg)

Temperature: -20 to +55°C

Altitude: 35,000 feet

TSO (Compass): TSO C6c

TSO (ADF): TSO C41c Class A

TSO (VOR): TSO C40a

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

VOR Video Input: 0.5VRMS 0 deg. phase composite 30Hz variable AM and 30Hz reference FM on a 9960Hz carrier (0.7VRMS maximum)

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.

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.

DAVTRON Μ475 Series 2-Function voltmeter/ammeter digital indicators are FAA-PMA approved and come in 475VA/475VAA models and versions, both with lighting capability. Model M485VA ls made primarily for remote shunts. They are both designed for low current drain ( .001 Amp) and are also used in standby and emergency battery packs. Other features include: 

Plus Or Minus Amp Range: 150.0 

Plus Volt D.C. Range: 100.0 

Sunlight Readable Display

One Tenth Amp Resolution

One Tenth Volt Resolution

1.3" case depth

2-1/4" Standard mount

Designed to help the pilot determine altitude by measuring existing atmospheric pressure, the altimeter translates the measurement into “height above sea level.” This is indicated on the dial of the instrument in feet, which requires setting the barometric pressure in the Kollsman window.

UNITED INSTRUMENTS 5934 series are FAA TSO'd 3"/ 3-pointer altimeters, intended for use with most single engine, turbo/piston prop aircraft. They are offered in 5934 and 5934A models with respective maximum calibrated ranges  of -1.000 to 20.000 feet and  -1.000 to 35.000 feet respectively. All lighted instruments require a light tray sold separately.

Product Features:

Affordable, certified 3-1/8" case for half the cost of existing systems

United series 5934

All units approved to FAA TSO (C10b,C2b and C4c)

Anti-reflective glass enhances visibility and reduces pilot fatigue

Altimeter available with right-hand or left hand knob 20,000 or 35,000 ft. Hg or Mb

All instruments are made in the USA

One year limited warranty

Product Specifications:

Typical Weight: 13 oz

Number of Pointers: 3

Barometric Setting: 28.1 to 31.0 in HG / 946 to 1050 mb

Calibrated Ranges: -1,000 to +20,000 or +35,000 feet

Static Pressure Connection: 1/8-27 ANPT

Installation: Removable Spring Nuts and screws

For additional information please consult the supplied documentation.

UMA airspeed indicators are fully FAA TSO'd to C2d specifications for installation on certified aircraft. Installable in a fixed wing aircraft with a reciprocating or turboprop engine. Must be installed in a temperature controlled environment form -55 to 85°C, to a max altitude of 25,000 ft. These airspeed indicators are available in different versions, 2-1/4",Single Speed MPH and 3-1/8" single or dual scale (MPH/Knots) versions with an outside/Inside scale: 40-200 MPH/40-170 Knots, housed in a Valox 420 Plastic case and weighting 8.6 oz. They are offered with or without certification. ASI markings are sold separately for each unit at additional cost. Please select the markings option if markings are required. 

4-Pin connector by AMPHENOL for use in all electrical gyros (DG or Horizon) including Falcon models.

UNITED INSTRUMENTS 8000/8100 Series Air Speed Indicators (ASI) are FAA TSO'd for installation on certified aircraft. 

The 8000 Series ASI indicate the speed relative to the air at sea level altitude. The 8100 Series True ASI indicate the speed relative to the air at sea level or the desired altitude.The indicator has an inner dial to indicate true airspeed. The altitude and temperature are the conversion factors used to obtain this reading with the use of a setting knob. 

When properly connected to an airspeed tube, the 8000/8100 Series airspeed indicators measure the differential pressure developed between the pitot and static opening. 

The pressure is indicated in units of airspeed mph (M) and/or knots (K).

Product Specifications:

Certification: FAA TSO C2b 

Case Configuration: MS33638, 3 inch

Typical Weight: 0.7 pounds

Static, Pitot Pressure Connector:   1/8-27 ANPT

Installation: Removable spring nuts and #6-32 screws

Lighting: Available upon request. All lighted instruments require a light tray sold separately. Please refer to offered SIGMA-TEK 5000B 14V or 28V Light Tray.

Electric 12V Fuel Quantity Sender 10-180 Ohm for Mitchell Fuel Quantity Gauge D1-211-5074. For 24V operation, order P/N PE-111-4074 Resistors for each instrument.

KANARDIA HORIS Air Data-Attitude/Heading Reference System (AD-AHRS) includes several state of the art sensors and combines them into a small PFD display. It can serve as standalone PFD displays and it can be used as a primary instrument or as a perfect backup. It is offered as standalone (master) device with integrated sensors or as a slave unit when an I-ALT-IAS or EMSIS PFD or NESIS are present on the CAN bus. AD-AHRS standalone unit shows: attitude (roll, pitch), airspeed (IAS and TAS), vertical speed (Vario) indication, altitude, outside temperature, QNH setting, heading rate (1 minute and 30 seconds turn), tracking course (True or Magnetic). It is offered for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15") and comes supplied with digital outside temperature sensor.

Product Features:

very low power consumption (< 2W at 12V),

low cost,

precise altitude pressure and IAS (indicated airspeed) sensor – connects to pitostatic,

precise angular rate sensors – gyros and accelerometers,

GPS receiver,

digital outside temperature sensor,

lightweight design (weighs only 235 g),

CAN bus compatible.

Available Options for HORIS AD-AHRS 57/80 (sold separately). They must be specified at the time of ordering.

MAGU Electronic magnetic compass.

AP-K Two servos for the two axis autopilot function. Must include also AMIGO.

AMIGO Autopilot panel for direct access to Autopilot functions. Must include also AP-K.