OMRON M2C Series cylindrical indicators have the basic design as the A3C pushbutton switches. They have a cylindrical 20-mmX12-dia. body making panel cutouts easier and provide good illumination with even surface brightness. These indicators are offered in lighted and non lighted versions, different colors, display shapes, with LED or incandescent lamps and different socket units. UL (E41515) and CSA (LR45258) approved. Please consult the supplied documentation for ordering.

MITCHELL AIRCRAFT PRODUCTS, Inc. is a well known manufacturer of tachometers, gauges, and instruments the general aviation industry, built under an FAA-approved quality system.

Their product range includes:

Mechanical 3-1/8″ Clockwise, & Counter-Clockwise, 2, 2-1/4″ Mechanical Recording & Electric Lighted Tachometers, 

Electric Gauges (Ammeters, Cylinder Head Temperature, Exhaust Gas Temperature, Fuel Quantity Gauges, Outside Air Temperature, Pressure & Temperature Gauges, and Voltmeters,

Mechanical Pressure &Temperature Gauges

Modular Gauges (Ammeters, Blank, Fuel Quantity,Pressure, Temperature Gauges, and Voltmeters, Modular Gauge Frames. This line of FAA PMA  miniature square engine gauges is ideal for a wide variety of general aviation applications. They measure nearly 1-1/2″  and are stackable. The modular design allows them to be plugged from the front of the panel. The units are internally lighted. Complete standard panels are also available. If individual gauges are ordered, appropriate backplate with pigtail must be ordered to mount and connect the gauge. If more than one gauge are ordered to be mounted together, a special order clustering requires custom backplates.

Sending Units (CHT & EGT Thermocouples, Fuel Quantity & Pressure Senders, 1/8″ & 5/8″ Temperature Senders.

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.

MITCHELL FAA PMA'd D1-211 Series  modular electric 12V (PN D1-211-5074) & 24V (P/N PE-111-4074) fuel quantity gauges are lighted and easily installed in a 2-1/4" panel hole. They feature a 2 year factory warranty.

The gauges and senders must be ordered separately.

For the 12V Fuel Quantity Gauge D1-211-5074 the matching sender is PS-211-8038, 10-180 Ohm. For 24V operation, P/N PE-111-4074  resistors for each instrument must be ordered.

MITCHELL Pressure Senders 80 PSI (PN PS-211-9002) and 150 PSI (PN PS-211-9040) are offered for use with D1-211-6089 and D1-211-6092 FAA PMA Pressure Gauges respectively. Both have 2 terminals (one terminal to be grounded).

MITCHELL EGT Gauge 0-1600 Deg. F, PN D1-211-6101 requires PN PS-211-8162 sender (probe).

The HONEYWELL BENDIX KING® KMT 112 is a Magnetic Azimuth Transmitter (aka Flux Detector or  Valve) which senses the direction of the earth’s magnetic field and continuously transmits this information through the slaving circuitry to a directional gyro (such as the HONEYWELL BENDIX KING® KG 102A or KSG 105 slaved directional gyros). This sensor is mounted remotely, usually in a wingtip, to eliminate the possibility of magnetic interference. The KMT 112 is typically used in HONEYWELL BENDIX KING® KCS 55A and KCS 305 compass systems. The KMT-112 flux valve is a sealed unit and cannot be serviced or have parts replaced. The unit must be replaced when/if it fails.

Like other KCS 55A compass system components, the  KMT 112 transmitter can be furnished in NEW condition or as USED in Serviceable or Overhauled conditions indicated respectively by the letters "SV" and "OH" in the product reference numbers (SKU and  accompanied by the relevant certification (e.g. yellow tag, 8130-3 form). They are also offered as exchanges / trade-ins  for returned customer owned units indicated by the letter "EX" in the SKU.  In the case of an exchange/trade-in option of a customer unit, the  full selling price of the ordered unit is charged and the core credit is refunded or credited towards future orders when our co-operating supplier verifies that the unit is in a reasonable, repairable condition. It is recommended that this option is selected by our customers mainly for upgrades and only in cases when their units are functioning properly at the time removal from the aircraft. In cases when customer units are found by our supplier to be non-repairable, the core deposit shall not be refunded and shipping charges shall apply if customers wish the return of these units to them. 

Installation parts and manuals are sold separately. 

For additional information and technical specifications please refer to the Product Desscription section, the product presentation of the HONEYWELL BENDIX KING® KCS 55A compass system or contact us.

 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.

OMRON A3C series cylindrical pushbutton switches have the basic design as the M2C Series cylindrical indicators. They provide a high-intensity uniform surface lighting while they have a miniature size with excellent feeling of operation. They have a cylindrical 20-mmX12-dia. body making panel cutouts easier. 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 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.

Product Specifications:

Case: Aluminum Casting

Weight: 10.6 oz. 

Case: Valox 420 Plastic

Weight: 5.0 oz.

Not FAA Approved

VDO Fuel Level Gauges have always been known for the superb fit, finish, and appearance, as well as the wide range of styles VDO offers. VDO Fuel Level 10-180 ohm Gauges  are offered in 2" and 2-1/4'" diameters with matching Fuel Level Senders  (aka sensors or probes) for their operation. This 12/24 VDC Fuel Level Sender has a resistance rating of 10 ohms when the tank is empty and 180 ohms when full. The unit can be adjusted to read accurately in tanks from 6" to 23" deep. In the case of the 2" 33-240 ohm Fuel Gauge, the appropriate fuel sender is P/N 226-007.  

VDO product range also include Standard Tubular Level sensors mounted direct into the tank with different tube diameters and lengths from 200 mm to 650 mm and different resistances. They feature:

- Resistance output

- Compatibility to the VDO gauges 301-010-00X and X10-110-981-009  (adjustable to 60 to 90 Ohm at empty).

- M4 bolt and hexagon nut or 6,3 x 0,8 mm spade terminal

- Optional ground connector

- Optional warning contact

- Mounting bolt circle 54 mm dip tube fuel senders with different tube diameters and lengths.

For additional information please consult the supplied documentation or contact us.

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.

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 FLYdat has been specially developed by TL ELEKTRONIC for BRP-ROTAX® Aircraft Engines for indicating and storing of engine operation data. The unit  is furnished with 8 sensor input ports, which can be occupied variably according to engine type.

The operating data is permanently compared with the engine specific operating limit. If the signalled operating data exceeds the stored operating limit, the FLYdat will warn the pilot. In addition all the input ports are equipped with a maximum alarm, responding when picked-up value is equal or above the stored limit. The FLYdat keeps the pilot informed on the following actual readings. Besides the topical data, the FLYdat shows also the hours of operation.

•  Engine speed

•  Cylinder head temperature (CHT)

•  Exhaust gas temperature (EGT)

•  Ambient air temperature (not on engines 912 / 914)

•  Temperature of cooling water (only on engines 582 UL, 618 UL)

•  Oil temperature and oil pressure (only on engines 912 / 914)

The TL ELEKTRONIC FLYdat is supplied with a standard configuration. With the standard configuration all trigger levels for warning- and alarm system are set to the maximum of the measuring range.

Configuration is available for the following BRP-ROTAX® engine types: 447 UL SCDI, 503 UL DCDI, 582 UL DCDI, 618 UL DCDI, 912 DCDI series, 914 DCDI series, Standard

By configuration of the TL ELEKTRONIC FLYdat, the engine type, engine number, hour of operation, temperature unit and the respective engine limits are programmed.

The TL ELEKTRONIC FLYdat unit and parts are no longer offered as ROTAX Part Numbers. These part numbers are provided for reference only.  In addition, 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 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 engine manufacturer for the correct part number before ordering.

KANARDIA diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters includes different RPM, CHT, EGT and oil/temperature engine gauges. 

KANARDIA INDU Series round RPM gauges are offered as standalone (master) or as slave gauges. The slave version requires an engine monitoring unit (DAQU) to be present on the bus. KANARDIA INDU Series round RPM gauges are available for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15"). They can be supplied in the following scales:

-RTX Rotax scale (7000) and markings (yellow, green, red)

-JAB Jabiru scale (3500). Markings must be specified at the time of ordering

-LYC Lycoming scale (3000). Markings must be specified at the time of ordering

-D D-motor scale (3100). Markings must be specified at the time of ordering

-CUS Custom made scale

KANARDIA INDU Series round standalone CHT and EGT indicators are offered for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15"). Respecive sizes of these gauges are 62 x 62 x 45 mm and 82 x 82 x 45 mm. The 57 mm gauges weights 150 g and requires a 102 mA power.

KANARDIA INDU Series round standalone Fuel Pressure, Oil Temperature and Oil Pressure indicators are available for 57 mm (2.25") and 80 mm (3.15") standard panel hole diameters with same sizes and weight power characteristics as those of CHT/EGT gauges.

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

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.

KANARDIA INDU Series G-Meter gauges form part of INDU diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters. They feature a LCD display with possibility to personalise the displays and scales. 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. These G-Meter gauges  are available for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15").

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.

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 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.

The RCA 56 Series of electric turn and bank indicators by KELLY MFG (RC ALLEN) are an all volt instrument, with a power warning flag, a black or white ball inclinometer and either lighted or non-lighted. These rate-of-turn pointer controlled instruments are powered by an electrically driven DC precision gyro with an inclinometer providing the pilot with turn and bank information.  They meet or exceed requirements of FAA TSO C3b. Made in the USA. Weight: 1.9 lbs.

Dimensions: Length: 6 1/4 in. Max, Width: 3 3/8 in. Max, Height: 3 3/8 in. Max

Mating Connector: MS3106A10SL-3S.

Connector Pin Out: A: +11-30 VDC, B: Ground, C: Spare

KANARDIA AETOS Basic EFIS Kit is a Non Certified complete navigation, flight and engine system for the ultralight airplanes, autogyros and helicopters. This self-contained state-of-the-art EFIS instrument is optimized for ultralight aircraft.

The AETOS Basic EFIS Kit comes with a large 7" sunlight-readable display with high contrast and integrated AHRS and GPS unit (AIRU), engine monitoring unit (DAQU), OAT probe, GPS antenna, cables & accessories. Engine sensors are not included in this kit. In contrast to NESIS EFIS, AETOS EFIS does not support flight maps. Options are available at additional cost to increase the functionality of this device.

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)