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.

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.

The RCA 22 Series of vacuum artificial horizon are controlled by air driven precision gyros to present the pilot with pitch and roll information. The attractive color scheme of blue sky and brown ground presents a realistic spherical display of flight. Unless otherwise indicated all instruments have a  "standard" display (dark blue/brown display with fixed pointer) and are unlighted.

All R.C. Allen vacuum gyros run off of 4.5" Hg, erect time is 3 min. The instrument fits in a standard 3 1/8 panel cutout. A ¼ -18 NPTF nylon tube slip fitting is recommended for vacuum hose installation. A 1/8 – 27 NPTF nylon tube slip fitting is recommended for vacuum gauge installation. 

Dimensions: H: 3-3/8", W: 3-3/8", L: 6"

Weight: 2.75 lbs.

Certification: Meet or exceed all requirements of FAA TSO C4c and Aeronautical Standard AS396B.

Made in the USA

NOTE: The RC Allen RCA22-7 Vacuum Horizon Gyro can be an alternate device for Cessna Gyro Horizon C661076-0101.

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.

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

The RCA 82A/83A Series TSO'd turn coordinators by KELLY MFG (RC ALLEN) can be found in many production aircraft around the world. They Incorporate an electrical gyro turn indicator with an inclinometer. The turn motion is presented by an airplane symbol banking on a fixed horizon. The inclinometer, by movement of a ball in relation to the lubber lines, indicates the slip angle of aircraft while in a turn. The airplane on the dial rotates with reference to the indices. A power failure flag drops into view whenever the supply voltage is lost or when dropped below a level acceptable for proper operation of the gyro. Operates from 11 to 30VDC. Available in lighted and unlighted versions. First installation requires electrical connector and clamp. Mating Connector: MS3106A-10SL-3S.

Product Specifications:

Meet or exceed requirements of FAA TSO C3b 

Made in the USA

Dimensions

Length: 6 1/5 in. Max

Width: 3 3/8 in Max

Height:3 3/8 in Max

Weight: 1.9 lbs.

Description: 

Unlighted

Mating Connector:

MS3106A-10SL-3S

Connector pin out:

A: +12 -30VDC

B: Ground

C: Spare

KELLY MANUFACTURING (RC ALLEN) RCA 15AK series are TSO'd 3-1/8" ( 80mm) electric directional gyros suitable for both fixed wing and rotor wing aircraft.

Series 200 Turbine Flow Transducers by FLOSCAN INSTRUMENT CO. INC. measure flows of hydrocarbon fuels such as gasoline, kerosene, and #2 diesel fuel and other light transmitting, non-corrosive liquids of similar viscosity.  Typical fuel flow applications include aircraft fuel monitoring systems; gasoline, diesel, and gas turbine engine test stands; and industrial furnaces. The transducers give repeatable signals on gasoline across a 100 to 1 flow range down to 0.3 GPH.  The higher viscosity of diesel fuel reduces signal repeatability at flow rates below 2 GPH.  Pressure drops are very low compared to other turbine flow transducers.  The transducer bearing system is rated for continuous operation at the upper end of the flow range. The transducers produce a current pulse signal from an opto-electronic pickup with a preamplifier. 

Because of their superior accuracy and extraordinary repeatability, FLOSCAN transducers have quickly become the dominate fuel flow measuring sensors for general aviation but are also used in marine and other applications.

FLOSCAN aviation products are NOT TSO, PMA or STC'd.

Please refer to the specification table for additional information.

KANARDIA INDU Combo IAS/Altitude/Vertical Speed 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 scales and LCD displays. They are offered as standalone (master) or as slave gauges. Slave versions require some PFD like KANARDIA NESIS, EMSIS, AETOS or HORIS to be present on the bus. KANARDIA INDU Combo IAS/Altitude/VSI gauges are available for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15"). Arc colors need to be specified  at the time of order.

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.

MID CONTINENT® INSTRUMENT (MCI) FAA/PMA approved precision quartz lighted clock meeting rugged aircraft environmental standards. Available in 14 Volt or 28 Volt versions.

MITCHELL FAA PMA'd D1-211 Series  modular 1-1/2 " fuel quantity square  gauges can be stacked in horizontal and/or vertical rows in any position in the aircraft panel. These  modular gauges are internally lighted and are plug removable from the front of the panel for easy maintenance. Available in different sender resistances for the indication of fuel quantity in the aircraft's left or right fuel tank.

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.

Revolution Counters (Tachometers)/HOBBS meters are used in BRP-ROTAX® aircraft engines. They are offered as certified or non certified parts from BRP-ROTAX® but also from other manufacturers.  Non certified parts can be used in ultralights or other aircraft not requiring certification of parts for their installation. Certified parts are designated by the letters "CERT" after the part number in the product reference number (SKU).

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.

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.

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.

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.

UMA Non TSO'd airspeed indicators are offered in 2-1/4" and 3-1/8" Single (MPH) and Dual Range (MPH/Knots) versions for installation on experimental aircraft only. They are housed in Valox 420 plastic cases and weigh 8.6 oz. . Depending on the selected indicator, ranges are in MPH, Knots or kilometers. Some inicators are also offered as certified (FAA TSO'd) units. Standard dial markings are black and white. Optional custom range markings and optional internal lighting(*) are also offered upon request at additional cost. Please indicate the markings option (if markings are required) and lighting option at the time of ordering. 

(*) Note: An inverter is required for the Internal Lighting Option.

The Vertical Speed Indicators (VSI)  provide an accurate indication of rate of change of altitude. 

UMA 8-210 Series Non TSO'd VSIs are offered in 2-1/4" and 3-1/8" versions. They are temperature compensated precision instruments provided with a zero adjustment screw on the face of the case in the seven o' clock position. They are powered by the aircraft static system. They are available in different ranges such as 0-2000 FT, 0-3000 FT, 0-4000 FT, or 0-6000 FT and different dial legends: Vertical Speed, Climb, Rate of Change, Cabin Climb.

3 1/8″ and  2 1/4″ VSIs are available with internal electroluminescent lighting in 3 colors: blue-white, aviation green and red. External DC-AC inverter required.  Weight 3 1/8″: 8.8 Oz - Weight: 2 1/4″ 7.4 Oz.

Case: Valox 420 Plastic

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).

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.