DUKANE SEACOM, wholly-owned subsidiary of HEICO Corporation, is the world’s leading supplier of FAA / EASA  & BSH qualified (Certified) high-impact underwater acoustic beacons for  the commercial air transport, business and regional jets, as well as fixed and rotary wing commercial and military markets. Other products in DUKANE SEACOM range include marine underwater beacons for Voyage Data Recorder (VDR) applications and Emergency Locator Transmitters (ELT) separately listed.

The DK120/90 was the first ULB certified to provide a minimum of 90-day underwater operating life. Certified to TSO-C121b & TSO-C142a and ESO ETSO-C121b & ETSO-C142a. Airframe mounted DK180 series low frequency beacon is designed and qualified to meet the newly developed standards FAA TSO-C200 / ETSO-C200 dated 6/26/2012 as per SAE–AS6254 & ARINC 667. For applications not requiring compliance to the 90-day operating requirement, the DUKANE SEACOM DK120/90 and DK140 (short) are still available.  An overview of DUKANE SEACOM Aviation  Underwater Location Beacons is provided in the Product Description Section.

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.

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.

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.

GARMIN GI-106B TSO'd panel-mounted CDI is a high-quality course deviation indicator which includes a VOR/LOC/GPS needle as well as a glideslope needle, that can be hidden and disabled by an installer if the glideslope functionality is not needed. The GI 106B contains LED-lit GPS, NAV and VLOC mode annunciators, for an easy-to-read and modern look. TO/FROM annunciators are also LED, and when invalid, the needles are simply hidden out of the pilot’s view instead of using conventional invalid flags. The GI 106B replaces existing Garmin GI-102A & GI-106A models. It is compatible with the same pinout connections as the legacy GI 102A and GI 106A course deviation indicators, allowing for an easy upgrade path. It also features anti-reflective lenses and LED flood lighting for viewing at night.

The  MID CONTINENT® INSTRUMENT (MCI) MD–90 Series Precision Quartz Clocks provide  an ideal solution for accurate time-keeping, and consist original equipment for many major aircraft manufacturers. Designed for accurancy, the 2-inch MD–90 Series clocks are manufactured to meet rugged aircraft environmental standards, they are FAA/PMA certified and offered in standard MD–90–1 and MD–90L versions, both operating with 8–32 VDC power input. Their key features include:

Precision quartz movement

Compact 2-inch size — fit standard panel cutout

Lighted version available with field-replaceable light tray

Transient and reverse polarity protection

Extremely low current consumption (3 mA) 

Continuously powered by aircraft battery

FAA PMA certified

Designed and built in the USA

One-year limited warranty

Product Specifications:

Power Input: 8–32 VDC - 3 mA max (without lighting) 

Accuracy:  ±30 seconds in 24 hrs 

Dimensions: 2.5 x 2.5 x 3.2 inches max 

Weight: 0.5 lbs 

Temperature: –40°C to +82°C (–40°F to +180°F) 

Altitude: –1,000 to +55,000 feet 

Humidity: 0 to 95% at 25°C 

Vibration: .02 in. dbl. ampl., 1.5g @ 5 to 50 Hz 

Mounting: Front or rear panel mounted 

Connector: #6-32 threaded terminals

For additional information please consult the supplied documentation.

AIRPATH certtified (FAA TSO) Magnetic Compasses are used in almost all production aircraft. They are offered in in different panel mount and pedestral models,  lighted or non lighted versions, black & white markings, black finish, and capabilities for operations in South or North Hemisphere. 

AIRPATH C2300 panel mount magnetic compasses fit in a 2.25 in. hole and need 3 in. of clearance from behind the panel. Offered Models(*): C2300, C2300-SF, C2300-L4, C2300-L4-SF.Compass fluid is included inside the units and come with the mounting screws and nuts required for their installation. A compass deviation card and card holder can be ordered separately. 

AIRPATH C2400 series pedestral magnetic compasses have been specifically designed for installation either for streamline-type bracket housing or a pedestal-type housing. Wire lead length, voltage, and lighting color are specified under each respective part number. Each model is provided with mounting hardware, deviation card, deviation card window and either an attached cardholder, deviation plate, or standard unattached cardholder depending on the application. All compasses in the C-2400 series meet FAA TSO-C7c requirements and are offered in different versions for operations in South or North Hemisphere. They fit in a 2.25 hole. Lighting: Red 12 VDC. Meet FAA TSO-C7c requirements.

(*) Letter “L” after the dash in the part number indicates a lighted version. Letters “SF” indicate South Hemisphere.

 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.

GARMIN® GTX™ transponder product line includes Mode A/C and Mode S TSO'd panel mounted transponders offered in a‭ ‬wide variety of configurations to choose‭ ‬from‭, ‬depending on desired functions‭.‬ Different models are listed under separate product presentations. 

GARMIN® GTX™ 328 solid-state Mode S digital transponder covers EU VFR Mode S requirements and is IFR certified for aircraft operating under 15,000 feet and with a true airspeed of under 175 knots. The GTX™ 328 includes many of the features of the GTX™ 330 transponder  at an affordable price such as outside air temperature, count up/down timers, altitude monitoring, density altitude functions, front-panel input for flight ID and has a digitised voice output for pilot warning of altitude limits or timer expiration.

The HONEYWELL BENDIX KING® KY 196A/197A series of TSO'd VHF COMM transceivers have a flatpack design, measure 1.3" x 6.3", weight just 2.8 pounds and have the same capabilities except that the 28-volt KY 196A delivers 16 watts and the 14-volt KY 197A 10 watts minimum transmit output power. Both incorporate solid-state construction and feature 9 pilot-programmable memory channels (11 including those in "USE" and "STBY"), flip-flop frequency transfer between active and standby frequencies, a 118.00MHz to 136.975MHz operating range and a digital frequency synthesizer generating 760 COMM frequencies. Despite their wide range of capabilities, KY 196A/197A radios were designed to be easy to read and logical to operate. An audio leveling feature automatically amplifies weak audio signals and mutes strong signals. Racks & connectors (for new installations) and manuals are sold separately. 

The HONEYWELL BENDIX KING® KY 196A/197A  VHF COMM transceivers are available in different versions  including those with Silver Crown Plus faceplates. They 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. Please refer to the Product Description section for technical specifications and information on USED avionics.

1-1/4 inch TSO'd Electronic Fuel Pressure Gauges from UMA INSTRUMENTS. Black & White dial marking. Available in different pressure (PSI) ranges. Case: Aluminum. Weight: 4.0 oz. UMA sensors are sold separately.

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.

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.

The R.A. MILLER (RAMI) TSO'd AV-74 (.425 Stud Length) & the AV-74-1 (.800 Stud Length) are broadband blade type antennas for transponders or DME applications. The antenna housing is constructed of an acrylonitrile-styrene-acrylic (ASA) shell. The white color allows maximum performance without losses due to color pigments or unseen dirt. The antennas are supplied with cellular neoprene mounting pad and hardware. Designed to operate at speeds up to 350 mph and altitudes up to 50,000 ft. They have a drag force of 0.09 lbs @ 250 mph. These antennas are direct replacements for the CI-105 antennas.

Product Specifications:

Application: Transponder/DME

Frequency: 960 - 1220 MHz

Impedance: 50 Ohms Nominal

VSWR: 1.5:1 Maximum

Polarization: Vertical

Pattern: Omni-Directional

Connector: "BNC" Female

Max Height: 3.4"

RF Power Capacity: 2.5 kW Peak

FAA TSO: C66c, C74c

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 GARMIN® GTR series COMM TSO'd panel mounted transceivers (please see separate presentation) together with the GARMIN® GNC series NAV/COMM radios are replacement products for the popular SL30 and SL40 models. They include new features to reduce pilot workload, while also offering an affordable solution to meet the requirements of the 8.33 kHz channel spacing European Union mandate under the Single European Sky (SES) initiative. They are more powerful than their SL-series predecessors with 10- or 16-Watt transmit power available versions. 

The GARMIN® GNC series NAV/COMM radios are offered with either a 10 W (GNC 255A) or 16W (GNC 255B) COMM featuring a 25 kHz or 8.33 kHz spacing. Both come with a an internal VOR/LOC converter, a 40-channel glideslope (GS) receiver and include the rack, connector kit, and back plate. They are offered as units only or as kits with a 4ft harness to AUDIO Panel.  If purchased with the 4ft harness, they can only be used  in experimental aircraft.

UMA NON TSO'd Electronic Amp Meter Gauges (Ammeters) are available in different series for different measurement ranges and installation in different panel hole diameters. 1-1/4" series allow utilization of 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 analog dials with easy to read markings. Each gauge uses rugged aircore meter movement for vibration resistance and repeatability. Each gauge can be placed in a 1-1/4” diameter hole and mounted behind the panel with (4) 6-32 screws. They can be cluster mounted as close as 11/2” centers. Also available as new manufacture electric with 2-1/4" dia. Other UMA series of electronic ammeters include 2-1/4" series with moving coil and 85° Sweep and 2-1/4" Dual Amp/ 0-30 volt meters with moving coil  and 85° sweep.

NOTES:

These ammeters come with the suitable shunt. Different shunts are used depending on ammeter part number.

All Part Numbers beginning with the letter "T" are TSO'd for Certified Aircraft.

WULTRAD INC. is a manufacturer of non-certified flight and engine instruments under FALCON GAUGE brand for experimental and homebuilt aircraft. Although their products are Non-TSO, they are made to TSO or MIL specifications for quality.

FALCON GAUGE Electrical Attitude Gyro is intended for use in experimental aircraft only. It provides a continuous visual display of the aircraft attitude with respect to the earth for maneuvering around the longitudinal (pitch), and lateral (roll) axes, and yaw. A precision AC brushless motor is featured in the electrical attitude gyro. The Power failure drops into view whenever the power is insufficient for operation of the gyro. Electrical gyro can be caged by pulling the "Pull to Cage" knob. It is offεred with or without internal lighting and is designed to work with a 12V system. Dimension: 3-3/8"X 6.46/164mm.

In addition to their panel mounted VHF transceivers, ICOM RADIOCOMMUNICATIONS offers handheld transceivers for aviation & marine applications. Their ICOM A25 series are powerful air band handheld transceivers offered in communications only (A25C) or NAV/COM versions (A25N) with 6 watts of power and an IP57 waterproof rating. They include a large 2350mAh Li-ion battery, providing a long operating time. The easy-to-use interface and large 2.3-inch LCD display combine to provide stress-free programming and in-flight operation. Built-in Bluetooth®, GPS and VOR navigation. ICOM A25 transceivers come with Antenna, Belt Clip, Handstrap, Battery Case, Battery Pack, Headset Adapter, Power Adapter and Battery Charger. ICOM IC-M25 VHF Marine transceiver is a slim depth light weight floating marine radio, floatable into the water with  flash and sound alarms. With its IPX7 waterproof construction, the 700 mW audio output, 11 hours of battery life, buoyancy in water and many other features it can effectively serve a wide range of marine applications. For additional information please consult the Product Description section.

Both GARMIN® GMA 345 and 350 are certified (TSO'd) Audio Control Panels for General Aviation aircraft.

Bringing rich “home theater” quality sound and wireless Bluetooth¹ audio connectivity to your avionics stack, the GARMIN® GMA 345 digital audio panel offers a superior inflight audio experience at an affordable price. Featuring 3-D spatial sound processing, a USB charging port, marker beacon receiver, advanced auto squelch, clearance playback and impressive audio mixing and distribution features, this all-digital unit offers the ideal blend of capabilities for pilots who want to hear and do more with less effort in the cockpit. In addition, it’s an easy slide-in upgrade to legacy GMA 340 units and selected third-party audio panels. Offered with optional 3-COMM support.

The GARMIN® GMA 350 is the first truly all-digital audio panel, introducing a number of new technologies to the cockpit, including Telligence™ Voice Command, 3-D audio processing and advanced auto squelch. Virtual 3-D audio processing adjusts audio in the headset to mimic how the human ear normally hears and registers sounds in space. Advanced auto squelch automatically adapts to a quiet or noisy cockpit without clipping words or cutting out in the middle of phrases. Offered with or without Bluetooth connectivity.

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

Installation parts and accessories for GARMIN® Audio Control Panels are sold separately. Please refer to the respective product presentation.