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.

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 V16 VHF Aviation Radio Transceiver by MGL AVIONICS  is the latest generation and the first in a new ecosystem of Comm Radios, Nav Radios and controllers designed with modern components and ingenuity for the lowest cost. It is a Non-TSO'd split design remote-mount COMM Radio (replacing MGL V6) for use in experimental and light-sport aircraft, which can be controlled directly by an MGL Avionics iEFIS (Gen 3 and above), with or without RAZOR/VEGA Controls or by a mix (and any number) of MGL RAZOR or VEGA series Control Heads, enabling dual radio displays and controls. It boasts 10 Watts of transmit power (unmodulated carrier). When paired with a RAZOR/VEGA control, the control can be connected to any EFIS or display that communicates with SL30/SL40 protocols, to tune the radio and load frequency lists. The V16 includes a 2-place intercom with a wide-range VOX system. Multiple headsets can be connected to the passenger channel if necessary. The advanced voice-activated intercom provides clear audio in noisy cockpits. In extreme cases the intercom can be activated via a switch connected to V16 (intercom PTT). For additional information please refer to the attached documentation.

RAMI AV-300 Antenna is a passive three frequency (121.5, 243 & 406 MHz) fiberglass rod antenna for use with an ELT (Emergency Locator Transmitter) in low speed general aviation aircraft (up to 350 knots).

Product Specifications:

Application: Airbone ELT

Frequency: 121.5, 243 & 406 MHz

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

Max Height: 14.00 inches max

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.

KANARDIA INDU Series round Airspeed Indicators 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) IAS units 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"). As an option they can be ordered with an Outside Air Temperature (OAT) digital sensor at additional cost. When static pressure (altitude) is present on the CAN bus, OAT sensor enables also the TAS  as well.

Scale Ranges:

-KMH Scale in kilometers per hour (0-280)

-KTS Scale in knots (0-140)

-MPH Scale in miles per hour (0-150)

NOTES:

A high speed sensor option is also available at additional cost (up to 460 km/h, 250 kts, 285 mph)

Arc colors need to be specified  at the time of order.

This line of FAA PMA'd  miniature engine gauges from Mitchell is ideal for a wide variety of general aviation applications. They measure nearly 1-1/2 inches square 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.

FAA Approved. If individual gauges are ordered, appropriate backplate with pigtail must be ordered to mount and connect the gauge. If more than one gauge ordered to be mounted together, a special order cluster that requires custom backplates.

RAMI AV-200 Antenna is a passive two frequency (121.5 & 406 MHz) whip antenna for use with a 406 MHz ELT (Emergency Locator Transmitter) in low speed general aviation aircraft (up to 250 knots). It has met DO-160G, Section 8, Category U requirements for robust vibration and is qualified for installation on helicopters with unknown related rotor frequencies.

Product Specifications:

Application: Airbone ELT

Frequency: 121.5, 406 MHz

Impedance: 50 ohms nominal

VSWR: 2.0:1 Max at 121.5 MHz, 1.5:1 Max. at 406 MHz

Polarization: Vertical

Pattern: Omni-Directional

RF Power Capacity: 10 Watts CW

Connector: BNC Female

Max Weight: 0.19 lbs.

Max Height: 24″

FAA TSO C126a

The FLIGHTCOM 403MC is a 4-place panel mount, easy to use, voice-activated mono intercom with 3-position transmit capability designed to fit almost anywhere in the panel.

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

JPI FS-450 Fuel Scan is a top choice low price unit for fuel management of an aircraft, offeredin different versions with single transducer available for gravity, pressure and ROTAX engines or with a Flow Scan 201 or 231 transducer and harness for pressurized carb engines.

Amphenol MS MIL-C-5015 Circular Plug Connectors are designed to meet the demanding performance requirements of military standards. These cable mount circular plug connectors have proven electrical capability for equipment applications where durability is important. The Amphenol plugs have threaded couplings and single key/keyway shell polarization for an accurate and reliable connection. The solid shells of these MS Series circular MIL-C-5015 connectors are made from high grade aluminium alloy. The shells are electrically zinc plated with an olive drab chromate finish which ensures a high resistance to corrosion. The inserts of these military circular connectors are made from resilient synthetic rubber which offers a high dielectric strength and resistance to vibration.

The MS3106A-10SL-3S plug can be used with Turn Coordinator TC02E-3-2 or Turn & Bank Indicator TB02E-2-1.

The RAMI AV-10 COMM Antenna is designed for high-performance aircraft applications. It exhibits excellent electrical characteristics and incorporates an efficient aerodynamic 4-bolt mounting base. The antenna essentially matches the styling of the communication antennas currently used on most singles and light twins. 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 2.70 lb @ 250 mph.

Product Specifications:

Application: Airborne Communications

Frequency: 118 to 137 MHz

Impedance: 50 Ohms Nominal

VSWR: 2.0 to 1 Maximum

Polarization: Vertical

Pattern: Omni-Directional

Connector: Type "BNC" Female

Max Weight: 8 oz

Max Height: 20-1/4"

RF Power Capacity: 25 Watts

The FAA TSO'd RCA26AK (14V) and 26BK (28V) series of electric attitude indicators (artificial horizons) by KELLY MFG (RC ALLEN) are known for their dependability and ruggedness. They incorporate tremendous advances in presentation, precision, and reliability.With a proven track record for dependability and ruggedness, the attractive new extended color schemes and ultra-precise spherical presentation (eliminating old parallax problems) they set a new standard for safety.These gyros provide a more accurate IFR reference for the beginning instrument pilot or a Cat II captain. A new three phase motor/inverter is designed into the gyro enabling it to operate at lower temperatures which extends to useful life. The instruments employ a new, high precision air erection system which provide erection torque for maintaining a proper vertical alignment reference. The erection air is supplied by a turbine pump which is integrally coupled with the gyro motor. Through maximum utilization of unitized construction the design is free of resonant frequencies below 100 HZ and thus cannot respond to low frequency disturbances which can cause dither and premature wear out of the unit. The display portion of the instruments has a directly coupled roll movement, and a pitch movement mechanism identical to that of the field proven vacuum gyros produced by R.C.Allen since 1966. A "pull to cage" spring type force limited mechanism assures immediate alignment and stability whenever power has been applied to the gyro, a feature non-existent on vacuum driven gyros. These artificial horizons have a hybrid inverter which converts the aircraft DC power to the required voltage and frequency for motor operation. All units have a pull cage knob and a power failure flag that drops into view whenever the supply voltage is lost or when the voltage has dropped below a level of acceptable for proper operation of the gyro. Slip indicator can be added to satisfy FAA AC91-75 upon request. Available in 14V or 28V voltage versions with fixed or movable pointer, lighted or unlighted, power failure flag, panel tilt and optional inclinometer. Mating connector MS3116E8-4S and panel screws are now included with each new instrument at no extra charge.

Dimensions: 3.38"W x 3.38"H x 8.14"L

Weight: 2.3 lbs.

RAMI AV-100 Antenna is intended for use with an ELT (Emergency Locator Transmitter) for general aviation. It has a passive two frequency (121.5 & 406 MHz) wire whip, designed for low speed aircraft (up to 250 knots).

Product Specifications:

Application: Airborne ELT

Frequency: 121.5 MHz, 406 MHz

Impedance: 50 Ohms Nominal

VSWR:

121.5 MHz 2.0:1 Maximum

406 MHz 1.5:1 Maximum

Polarization: Vertical

Pattern: Omni-Directional

Connector: "BNC" Female

Weight: 3 oz. Maximum

FAA TSO: C126a

Color: Black

TSO'd Electronic Fuel Quantity gauges from UMA INSTRUMENTS (indicated by the letter "T" in the PN) are offered in 1-1/4 in. and 2-1/4 in. sizes for installation in respective panel hole diameters and mounted with (4) 6-32 screws. Smaller 1-1/4 in. instruments can be cluster mounted as close as 11/2” centers utilizing 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 black analog dials with white easy to read markings indicating empty to full fuel level. Each gauge uses rugged aircore meter movement for vibration resistance and repeatability. Available in different versions based on their sender type and range. UMA sensors are sold separately.

HONEYWELL BENDIX KING® Aviation Database Services are offered for database updates of different navigation BENDIX KING® devices. They cover different geographical areas and are available for use in single or multiple devices, as single (one cycle) or multiple scheduled annual update cycles per year. They can be distributed through media (database cards/cartridges) and/or internet downloads (eliminating media and shipping costs). Database upgrades are subject to copyright restrictions and are allowed for use only in the specific aircraft and devices specified at the time of ordering. Orders for HONEYWELL BENDIX KING® database updates are fulfilled by AVIATIONEU TRAINING SYSTEMS & SERVICES which offers aviation database services, in cooperation with respective database providers, on a simplified subscription-based ordering process saving man effort, time and costs for customers. Please refer to our listed services or contact us for additional information.

ROTAX® aircraft  engines form part of the product portfolio  of BRP-Powertrain GmbH & Co. KG which develops and manufactures engines for snowmobiles, watercrafts, boats, roadsters, all-terrain and side-by-side vehicles, motorcycles, carts, and aircrafts.

BRP-ROTAX® product range includes certified and non certified internal combustion engines, parts and accessories for light and ultralight aircraft.

Fuel pressure gauges are used in BRP-ROTAX® aircraft engines and offered as certified or non certified parts from their respective manufacturers. Non certified parts can be used in ultralights or other aircraft not requiring certification of parts for their installation.

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 BRP-ROTAX® 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 manufacturer for the correct part number before ordering.

Fuel pressure gauges are no longer offered as ROTAX Part Numbers. These part numbers are provided for reference only. For these gauges please refer to our product presentation on AVIASPORT Fuel Pressure Gauges or contact us.

The KANNAD 406 AS (P/N S1823502-03) is a aeronautical survival beacon. Thanks to its small size and light weight, the Kannad 406 AS fits easily inside a liferaft. It is supplied with a floating collar.

The KANNAD 406 AS is qualified by the French Civil Aviation in Europe with JTSO-2C91a & JTSO-2C126 and by FAA with TSO-C91a & TSO-C126 applied to “survival” beacons.

The ELT is programmed with either the aircraft tail number, a serial number or the aircraft operator designator. It can be installed inside an aircraft on a mounting bracket or in a carry-off bag (both on options).

The mounting bracket option includes a locking pin to avoid accidental activation before ELT removal. The locking pin can be ordered separately with the carry off version.

The ELT can be fitted with a "Water Switch Sensor" to be activated automatically when in contact with water. A buzzer and a led indicate activation.

An integrated “self test” checks the main functions of the beacon. The test result is given by the led flashing sequence.

Product Features:

Battery replacement is only every 6 years.

Precise pinpointing (<1NM) due to the unparalleled frequency accuracy of the 406 transmitter.

Three frequency transmitter (121.5 / 243 / 406 MHz)

Weight (including battery, auxiliary antenna and floating collar) 2.53 lbs (1150 g)

Options:

P/N S18 20 511-03 carry-off bag

P/N S1820511-02 Mounting bracket with locking pin

P/N S1820514-14 Water Switch Sensor

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.