EASA Certified 10 W Comm Radio with 25 kHz spacing.

UMA  2-1/4" electric tachometers with their high resolution and easy to read displays were designed to offer aviation styling and performance for all types of aircraft. The analog model has a 270° sweep which provides great resolution in both the 3500 and 7000 ranges. The digital model has a bright LED display. Separate power source required. Installation is simple and instructions are included. They can replace mechanical tachometers in Lycoming/Continental engines.

Current: 80 milliamps ­ Size: 2.25" round x 2.75"deep.

 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.

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

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. 

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 AV-532 is a VOR/LOC/GS receive only antenna which consists of taper ground high-strength 17-7PH stainless steel elements to reliably withstand vibration and wind loads. The insulators are weather-sealed compression-molded bakelite with the mounting holes provided. The unit may be mounted with the V pointed either forward or aft. The antenna is designed to operate at speeds up to 350 mph and altitudes up to 50,000 ft. It has a drag force of 3.42 lb @ 250 mph.

The BOSE A20® Series light weight (12 ounces) Aviation Headsets are engineered to be more comfortable and provide clear audio  with more noise reduction than any other of company headsets featuring in addition customizable audio prioritization control, intuitive “plug-and-play” operation, a high-performance microphone, an optional  Bluetooth audio and communications interface and an optional coil cord. The ergonomic control module includes an auxiliary audio input with intercom/AUX priority switching, ideal for dedicated GPS and traffic warning systems. The BOSE A20®  Series headsets also feature a customizable audio prioritization control with “mute” and “mix” settings, and flexible power circuitry with auto-on that switches to and from battery power and aircraft power. Select models also include Bluetooth connectivity for taking calls or listening to music. The BOSE A20® Series headsets are offered in dual plug, 6-pin plug and U174 plug models and a variety of configurations designed for use in all types of general aviation aircraft, including helicopters (*).

Key Product Features:

- 30% greater active noise reduction than conventional aviation headsets

- 30% less clamping force than conventional aviation headsets

- Automatically shapes and equalizes incoming signals for enhanced clarity and intelligibility

- Bluetooth Connectivity to Bluetooth-enabled devices (Only available for Bluetooth headset versions)

- Customizable audio prioritazation. Choose “mute” to immediately mute an auxiliary audio signal when receiving a communication. Choose “mix” to mix in-bound communication with your Bluetooth or plugged-in audio signal

-  Offered in different headset plugs (GA, U-174, LEMO, XLR-5 depending on the selected model variant)

- Certified to FAA TSO and E/TSO-C139 standards

- Side-Swappable Mic. Connect the mic to either the left or right earcup

- 45+ hour battery life with just two AA batteries

Product includes:

Selected A20® Aviation Headset

In-line clothing clip

Control module

2 AA batteries

Aux-in cable adapter

Carrying case

For additional information please refer to the Product Description section, the supplied documentation or contact us.

(*) Please refer to the Note on Headset Connectors at Product Description.

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

AERO INSTRUMENTS® Company, now part of AEROCONTROLEX® Group, Inc., has been a supplier of Air Data Sensors for aircraft applications for over 85 years. AEROCONTROLEX® current manufacturing  of Air Data Sensors has been transitioned to AEROSONIC® Corporation which manufactures aviation instrumentation and avionics equipment including air data systems, standby displays, digital and mechanical standby instruments, sensors and probes.

AEROSONIC® / AEROCONTROLEX® extensive portfolio of pitot probes, including pitot, pitot static and pitot/angle-of-attack probes, are designed and today in use  on a wide range of aircraft ranging from military and large commercial transports to helicopters and UAVs , meeting the requirements of virtually any type of aerospace application. Product range  includes electrically heated pitot probes, pitot-static probes, static pressure ports, angle of attack, temperature sensors and flight test equipment for the aerospace and defense industries. They are designed to meet or exceed all applicable standards, including SAE AS393, DOD MIL-T-5421B, TSOC-16, AN5813 and BS2G.135 and feature heating elements to prevent ice accretion and water ingression for reliable operation in the most adverse environmental conditions. AEROSONIC® / AEROCONTROLEX® Pitot Probes are designed with rugged heating elements to prevent ice accretion and water ingression for reliable operation in the most adverse environmental conditions. Probes may be configured as stand alone with pneumatic outputs to the Air Data Computer, or they may integrate the computing function and eliminate the pneumatic connection.

Product Information & Features:

All probes are customizable to customer requirements

Common plating options available: chrome, dull chrome and electroless nickel

Electrically heated for anti-icing protection. 

Enhanced dual heat zone in the mast and sleeve.

Multiple voltages available: 12V, 24V, 28V, 115V

Accuracy up to 600 knots

Temperature range -65°C to +70°C

Angle of attack ranges from -40° to 40°

Aircraft Applications:

Chinook CH-47

Cessna Citation

General Atomics Predator

Eurocopter EC135/145

Dash-8

Bell Helicopter 204/206/407/429/430

Boeing Apache

Piper Maibu

Agusta Westland AW609

FALCON GAUGE  Electrical Turn Coordinator is used for displaying the angular rate and sideslip of turning in horizontal flying and turning. The inclinometer indicates the slip angle of the aircraft while in a turn. A power failure flag drops into view whenever the voltage drops below a level for proper operation. The Turn Coordinator incorporates a built-in voltage regulator so it can be used with either 14VDC or 28VDC power system. It is compact in size and light weight eliminating radio interference.

This small, lightweight unlighted turn coordinator is excellent for homebuilt aircraft. Works for 14 Volt or 28 Volt systems. Features, power out warning flag with a 0° Panel. Fits Standard 3-1/8" Cut Out, 3-3/4" long.

Pitot tubes scan the static and dynamic pressure, and they are used on aircraft to determine the aircraft airspeed. FALCON Non TSO'd (non-certified) pitot tubes have been used for many years on different types of experimental or other aircraft where no certification is required. Available in different heated and unheated versions for 12 or 24 V electical supplies, for vertical or flat installations. Standard (3/4") and long (4") mounting brackets are offered. Heated Material: Stainless Steel. Please consult the supplied documentation or contact us for further information.

FLYBOX® EFC-P Electronic Flap Controller by MICROEL SRL allows selection of the desired position of the flaps of an aircraft. EFC-P Controllers are offered in Rectangular (P/N: EFC-P-102010) or Round (P/N: EFC57-P-103010) versions. They are intended for use in ultralight and experimental aircraft. The working mode consist in selecting one of the four positions previously stored by the user, then the EFC-P will automatically moves the flaps in the exact position. The LEDs show the current position of the flaps or, when in movement, the position that they are reaching. For further information please refer to the attached documentation.

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").

Splits the signal from a single NAV antenna into two NAV receivers and one glide slope receiver.

Static ports are located on the side of an aircraft and function as small air inlets. Their purpose is to measure static air pressure, also known as barometric pressure. The pressure within the static port is collected and then utilized by the altimeter and the vertical speed indicator (VSI). Different static ports are offered, both certified and non certified (the latter with an intended use in homebuilt/experimental aircraft).

Several offered non certified static ports are briefly described below. For certified static ports plese refer to their separate product presentations.

Aluminum Cessna Type

Aluminum single engine Cessna type static port. Externally mounted through a 19/64” hole. Can be used on fabric, composite or aluminum. No need for rivets. 1-3/8” dia.x1” depth.

Aluminum 15160

Aluminum static port for external mounting through 1/4" diameter hole in side of the fuselage. Base has 1/8" NPT female port for connecting to static line (polyethylene fitting included). Installation with 3/32" diameter flush rivets.

Aluminum 15161

Aluminum static port for external mounting through 1/4" diameter hole in side of the fuselage. Base has 1/8" NPT female port for connecting to static line. Installation with 3/32" diameter flush rivets.

Aluminum 15176

Aluminum static port externally mounted in a 1-1/4" base OD outside of the fuselage through 5/16" ID hole. Installation with 4 countersunk 3/32" rivets to skin with pal nuts & lock washers on inside.

Sigma-Tek Light tray to connect lighting to Sigma-Tek 5000B Attitude Gyro and other avionics and instruments. Available in 14V or 28V versions.

SAFE FLIGHT (SF) is the world's leading manufacturer of aircraft lift instrumentation and control systems. SAFE FLIGHT FAA certified Lift Detectors & Angle of Attack (AoA) Sensors are installed on hundreds of aircraft worlwide.

SF’s Lift Detector is the foundation of SAFE FLIGHT’s Stall Warning systems. This was the first and still the industry standard for stall warning in light aircraft. It  consists of a small tab or vane which senses the change of the stagnation point on the wing and an alerting device used for stall warning. The  detector warns by light and horn of any danger of an approaching stall regardless of the flight maneuver. It comes in different variations complete with installation kit & instructions. 

SF’s SCc Angle of Attack (AoA) system meets FAA requirements by providing both flashing red LEDs and an unmistakable audio output to alert the pilot of increasing AoA and an impending stall. It consists of two key components, the Lift Transducer and the the Indexer Computer. Available for retro-fit. Including the Lift Transducer, the Indexer Computer, and all necessary wiring, connectors and installation hardware.

For additional information please refer to the Product Description section and the supplied documentation.

UMA line of precision electronic pressure senders feature precision, solid state sensors and circuitry to give unequalled performance and are designed for rugged use in just about any environment.  They are offered in TSO'd and Non TSO'd models and gauge, differential and absolute types. UMA TSO'd electronic pressure senders are the most economical TSO’d units on the market. They are compatible with avgas, jet fuel, engine oil and many other fluids. Because they have internal voltage regulation, they are compatible with indicating instruments that do not have precision output voltages. Units for fuel and oil pressure are certified under TSO C47. Units for manifold pressure are under TSO C45a. For additional information please refer to the attached documentation.