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

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.

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

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.

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.

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.

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.

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.

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. 

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.

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.

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.

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.

BENDIX KING KG 102A TSO'd Remote Mounted Directional Gyro can be used in in BK KCS 55A compass system  in conjunction with KMT 112 Magnetic Azimuth Transmitter to provide a gyro-stabilized magnetic heading to KI 525A HSI.

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

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 HONEYWELL BENDIX KING® KCS 55A Compass System provides the pilot with a simple, comprehensive visual display of the aircraft's heading and position in relation to a desired course. The system simplifies course orientation, intercept and tracking. Although only the KI 525A Pictorial Navigation Indicator (PNI) and the KA 51B Slaving Control & Compensator Unit appear in the aircraft panel, other remote components  of the KCS 55A system include the KMT 112 Magnetic Slaving Transmitter, the KG 102A Directional Gyro for stabilization of the system and optionally the KA 52 or KA 57 Autopilot Adapters making the KCS 55A a complete slaved compass system. Installation parts and manuals of the above components are sold separately. For further information on these components please refer to their individual product presentations. For additional information on  KCS 55A and technical specifications please consult the Product Description section.

The HONEYWELL BENDIX KING® components of KCS 55A Compass System 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. 

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.

Range of special accessories by FRANZ AIRCRAFT ENGINES for use in BRP-ROTAX® aircraft engines and other applications.