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.

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.

GARMIN® GMA 245 Audio Control Panel draws on Garmin audio technology for “home theater” quality sound. Offers instant upgrade as a slide-in replacement for older GMA 240 and GMA 340 units installed in experimental and light sport aircraft.

Key features include: 

Bluetooth wireless connectivity for easy access to phone calls & audio entertainment (1 device allowed connection)

Audio Inputs: 3 Transceivers (including TEL), 5 Receivers (NAV1, NAV2, AUX1, AUX2, AUX3)

3D audio processing helping pilots to “locate” inputs coming into their headsets

6 Position Intercom: pilot, co-pilot, 4 passengers with 2 volume controls by pilot/co-pilot or passengers

Clearance playback

Impressive audio mixing and distribution

USB charging port powering smartphones, tablets, music players and more

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.

HONEYWELL BENDIX KING® KX 155A and KX 165A TSO'd Panel-Mounted NAVCOMM Transceivers update the concept of the combined navigation and communications radio for the 21st century. With such features as programmable comm channels, support for 8.33 kHz Comm tuning (KX 165A model only), GPS QuickTune, multiple operating modes, remote channel increment with flip-flop tuning & a built-in timer, they combine a sophisticated appearance with a number of advanced capabilities including:

Programming of up to 32 Comm channels in a non-volatile memory circuit for ready recall of regularly used frequencies.

Pre-selected frequencies stored in a non-volatile memory circuit.

When interfaced to the KLN 94 GPS, both the standby Comm and Nav frequencies can be selected and remotely tuned from the GPS database.

The KX155A (a KX155 upgrade) provides access to all 200 NAV and 760 COMM frequencies, along with its optional 40-channel glideslope. In addition to its standard use, it incorporates new features including a bearing-to-station mode and a radial-from-station mode, an internal Course Deviation Indicator (CDI) for use when the external CDI is being driven by a GPS receiver, and an elapsed-time and approach timer. The KX 155A system offers 10W minimum COMM transmitter power.

The KX-165A NAV/COMM replaces BENDIX KING® KX-155, KX-155A and KX-165 NAV/COMMs which are discontinued but are still available for outright sale or in exchange for returned customer owned units in USED Serviceable or Overhauled Conditions with FAA 8130-3 Form certification. The letters "SV","OH" and "EX" in the product reference numbers (SKU) indicate the condition/sale terms. 

Very similar to KX 155, the BENDIX KING® KX 165 NAV/COMM additionally incorporates an internal VOR/LOC Converter to directly drive the BENDIX KING®  KI 525A HSI (part of the KCS 55A Compass System). It can also display the current radial from the active VOR instead of the standby NAV frequency. Other features include 10 watts min transmitter power, easy-to-read, bright gas-discharge display, large, self-dimming, microprocessor- controlled gas discharge readouts and solid-state electronic tuning for fast, accurate selection of all 200 NAV and 760 COMM frequencies.

The KX 165A (-0201 model) NAV/COMM is a slide in 8.33 kHz replacement for its predecessors, the KX 155A which is discontinued and KX 165A 25 kHz NAV/COMMs (-0101 model). Completely redesigned, it features programmable Comm channels, support for 8.33kHz Comm tuning, GPS Quick-Tune, multiple operating modes, remote channel increment with flip-flop tuning and a built-in timer.

Mounting racks, connectors and manuals  for the installation of the NAV/COMMs are also offered.

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

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

The GARMIN® GTR series COMM TSO'd panel mounted transceivers together with the GARMIN® GNC series NAV/COMM radios (please see separate presentation) 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. 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.

The ICOM IC-A210 Series of VHF 760 COMM transceivers operating in 118-136.975MHz range are offered as non certified radios. Featured with OLED displays,"flip-flop" arrow button switches between main and stand-by channels, GPS memory function, a built-in DC-DC converter accepting 12/24VDC power source, a built-in voice activated intercom allowing pilot-copilot communication via the headset and two types of rear-panel adapters included for streamlined plug-in connectivity, ICOM A210 series transceivers are a meaningful choice for radio upgrades and replacecements as they are interchangeable with IC-A200, KY96A/KY97A & SL40 radios. IC-A210E is compatible with 8.33kHz channel spacing in addition to the widely used 25kHz. For a certfied model please refer to the  TSO/ETSO certified IC-A220T.

The TT31 is a power-efficient, inexpensive, Mode S transponder by TRIG AVIONICS  that meets the European elementary surveillance requirements. The TT31 fits in the same mounting tray as the BENDIX KING KT76A transponder, making it a great choice for either upgrades or new installations. The TT31 plug and play design minimises the cost and downtime for the upgrade. The TT31 is TSO approved for fitting to European and FAA registered aircraft. With a new software upgrade and a connection to an appropriate GPS, this will make the TT31 compliant with the FAA final rule on ADS-B Out (TSO C166b) for 2020.

Product Features:

European Mode S (*)

Low Power Consumption

No Cavity Tube

240 Watts Nominal Output

Plug and Play Installation

Backlit LCD Display

Easy to Use Rotary Knobs

Timer/Stopwatch Function

Altitude Monitor

Certified 1090ES/ADS-B Out (TSO C166b)

NOTE (*): All Mode S transponder upgrades for EASA certified aircraft must be carried out by a licensed engineer using a Minor Change approved by EASA. 

Pre-approved Minor Changes for popular aircraft types may be available for this device. In this case no EASA fees for the issue of Minor Change approval apply. Contact us for more information.

Automatic portable radio beacons (ELT(AP) АРМ-406П (ARM-406P), АРМ-406П1 (ARM-406P1) and АРМ-406АС1 (ARM-406AC1) are safety devices designed to transmit via satellite to the stations COSPAS-SARSAT distress radio signals with aircraft coordinates received from the onboard computer system.Such information facilitie identification of the aircraft and guidance of S&R facilities to the accident site. Located in the aircraft cabin these devices offer the possibility of quick use in an emergency.

The automatic portable radio beacon АРМ-406П1 (APM-406P1) includes:

- monoblock P, consisting of a double protective casing with shock absorbers installed in it, an overload sensor (DP) and an AC1A monoblock;

- remote control PDU-406 (ПДУ-406) installed in the cockpit;

- external antenna ANT-406VA (АНТ-406ВА), mounted on the aircraft body.

The АС1А monoblock is  a portable radio beacon, including a PM-AC1A (ПМ-АС1А) transmitting module, an АРМ-043-01 autonomous power supply unit and an ANT-APM-01 (АНТ-АРМ-01) antenna. The emergency mode of operation of the AC1A monoblock can be switched on both from the remote control and from the DP, as well as manually when removing it from the protective casing when leaving the emergency aircraft.

Autonomous power supply (APS) units are also offered for use with the radio beacons. АРМ-043 (CDKT.436140.590) 14.4V are intended for use for beacons manufactured before 2013 while АРМ-043-01 (CDKT.436140.590-01) 10.8V for beacons manufactured after 2013. Unless otherwise specified their replacement frequency is once every 3 years with a 3-year self life.

For additional information please refer to the supplied documentation or contact us.

The AV-534 is a TSO'd heavy-duty stainless steel bent whip VHF communications antenna with porcelain insulators and mounting hardware. The AV-534L is same antenna as AV-534 but furnished with 96" lead of RG58 A/U cable with male BNC and ground strap with lugs.

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

R.A. MILLER INDUSTRIES (RAMI) aircraft antennas cover a wide range of functions including communications, NAV antennas, GPS, ADS-B, transponder, VOR localizer, glide slope antennas, and marker beacons. They are known for their streamlined aesthetics, quality, and reliable performance. Offered in different TSO models, RAMI wire whip and rod antennas ELT (Emergency Locator Transmitter) devices are intended for use on low-speed General Aviation aircraft. 

RAMI AV-100 FAA TSO C126a Airborne ELT Antenna is a passive two frequency (121.5 & 406 MHz) whip antenna, designed for speeds up to 250 knots. Impedance 50 Ohms Nominal, VSWR (Maximum):121.5 MHz 2.0:1 / 406 MHz 1.5:1, Polarization Vertical, Pattern Omni-Directional, Connector BNC Female, Weight: 3 oz. Maximum, Color: Black.

RAMI AV-200 FAA TSO C126a Airborne ELT Antenna is a passive two frequency (121.5 & 406 MHz) whip antenna, designed for speeds up to 250 knots. It meets DO-160G, Section 8, Category U requirements for robust vibration and is qualified for installation on helicopters with unknown related rotor frequencies. Impedance 50 Ohms Nominal, VSWR (Maximum):121.5 MHz 2.0:1 / 406 MHz 1.5:1, Polarization Vertical, Pattern Omni-Directional, RF Power Capacity 10 Watts CW, Connector BNC Female, Weight: 0.19 lbs. Maximum, Max Height 24″.

RAMI AV-300 FAA TSO Airborne ELT Antenna is a passive three frequency (121.5, 243 & 406 MHz) fiberglass rod antenna, designed for speeds up to 350 knots. Impedance 50 Ohms Nominal, VSWR: 2.0:1 max at 121.5 MHz,2.0:1 max at 243 MHz, 1.5:1 max. at 406 MHz,  Polarization Vertical, Pattern Omni-Directional, RF Power Capacity 10 Watts CW, Connector BNC Female, Max Weight 9 oz, Max Height 14″.

The GARMIN® GTN 650Xi (*) GPS/Nav/Comm/MFD panel-mount platform replaces discontinued GTN 650 (**) offering more pixels, processing power, speed and performance.  It’s approved for installation in many of makes and models of fixed-wing aircraft and helicopters providing high-resolution terrain mapping, graphical flight planning, traffic target surveillance, multiple weather options, taxiway diagrams and a host of other advanced navigation features. It comes with Americas or International Database (specified at the time of ordering).

The GARMIN® GTN 650Xi features:

- a brighter, faster, sharper, better Do-It-All intuitive touchscreen interface providing quick access to navigation, radio tuning, multifunction display features and more,

- powerful fast response dual-core processors boosting the GTN Xi series graphical display capabilities — with faster zooming, panning and map rendering on the display,

- high-resolution  4.9” display with almost double the pixel count of its predecessor and wider viewing angles,

- multi-function display cpability supporting multiple inputs of moving maps, terrain, traffic, weather, airport diagrams and more,

- easy data entry with the use the on-screen QWERTY keyboard or traditional concentric knobs to enter frequencies, waypoint identifiers, routings and more,

- Telligence™ voice control technology helping reduce pilot workload by responding to hundreds of spoken commands with the press of a button on the yoke,

- finger swipe gestures enabling pilots to pan across the map display or use a smartphone-like pinch-to-zoom motion to scale up or down on any map, traffic or terrain page.

GARMIN® GTN 650Xi Specifications

TSO applicability: C34e; 2C34f; C36e Class A; 2C36f Class A; C40c; 2C40c; C74d Class A; C112e; C128a; 2C128; C146e Class 3; C151d Class A, B; C157b Class 1, 2; 165b; C169a Class C, E, 3, 4, 5, 6; 2C169a Class C, E, H2, 3, 4, 5, 6; C194; C195b Class B1, B3, B5, B7; C209

Display size: 4.9" (125 mm) diagonal

Display resolution: 834 pixels (W) x 370 pixels (H)

Unit bezel height: 2.65" (67 mm)

Unit bezel width: 6.25" (159 mm)

Unit depth with connectors: 11.25" (286 mm) (measured from face of aircraft panel to rear of connector backshells)

Unit weight: 5.5 lbs (2.48 kg)

Input voltage range: 11 VDC - 33 VDC

Operating temperature range: -20° C to 55° C (-4° F to 131° F)

Number of GPS channels: 15 (12 GPS and 3 GPS/WAAS/SBAS)

LAT/LON position accuracy: <1.25 meter RMS horizontal, < 2 meter vertical, with WAAS

Maximum velocity: 1,166 knots

Position update Interval: 0.2 sec (5 Hz)

Notes:

(*) The GARMIN® GTN 650Xi can be supplied as kit with 4 feet pigtail wire harness without certification . If cerification is required installation must be done by a GARMIN® Authoried Service Center.

(**) The GARMIN® GTN 650 can be supplied as USED (Serviceable) Certified unit (FAA 8130-3 Form) with GPS antenna, rack, connector, existing Database, 6 nonth warranty.

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. 

GARMIN® GA 35 GPS WAAS is a FAA TSO'd antenna suitable for use with Garmin GPS devices like the GTN 650 GPS/NAV/COMM/MFD. Antenna connection is female TNC out. For installation of this GPS antenna the use of  RG 400 or RG 142  and a male RG400/142 TNC connector is recommended. The mounting plate for this antenna is sold separately.

ETSO'd Slimline Panel Mounted 16 W VHF Radio with built in 2-place intercom with auxiliary inputs for stereo music and audio warnings. Available with 8.33 kHz or  25kHz frequency spacing options.

The AV-525 is a VOR/LOC/GS antenna similar in style to the AV-12 but utilizes an internal balun transformer. The antenna is rated at speeds up to 350 mph and altitudes up to 50,000 feet. It is a direct replacement for the CI 157P.

Product Specifications:

Model: AV-525

Application: VOR/LOC/GS Receive Only

Frequency: 108-118 MHz (VOR/LOC) -328-336 MHz (GS)

Impedance: 50 Ohms Nominal

VSWR: 3.0:1 Maximum 108-118 MHz - 2.0:1 Maximum 329-335 MHz

Polarization: Horizontal

Pattern: Omni-Directional

Connector: “BNC” Female

Max. Weight: 0.50 lbs.

Certification: FAA TSO C34e, C36e, C40c

The new OROLIA-KANNAD INTEGRA 406 GPS ELT is a major step forward in the development of ELT technology and aircraft safety. Major benefits over standard ELTs include  a fail-safe automatically activated system for transmission of both the unique identification and GPS position in case of ditching of the aircraft or a crash landing as well as the ability for the pilot/ crew to remove the ELT from a downed aircraft. In addition,it features internal 406MHz and GPS antennas saving significant cost on aircraft  installation without the need for an  external antenna (national authorities’ rules and regulations permitting) and additional external GPS interface.

The 406 INTEGRA fixed ELT(AF) transmits on both the international 406MHz satellite search and rescue system (min  24 hours from activation) and on 121.5MHz for local direction finding. Minimum operating temperature is -20°C. The internal battery life of the INTEGRA is 6 years. Complies with European and FAA standards.

406 INTEGRA ELT(AF) is designed for flat installation on fixed wing aircraft and can be connected to an outside antenna (sold separately). 

This ELT comes with:

the COMPACT universal mounting bracket

RC200 remote control panel

DIN-12 connector

SUB-D 9 pts female connector

Note: Hazardous Material

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.