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 analog and digital portable two-way radios (walkie talkies), manufactured by QUANZHOU YANTON ELECTRONICS CO., LTD., come in different models covering UHF or VHF and UHF frequency bands and different power outputs for communication over different distances. They have an ergonomic design and cover the needs of various operations. YANTON radios are approved by the Ministry of Information Industry in China and the European CE, RoHS and USA FCC certified/approved for use in other countries.

Installation parts and accessories used in different GARMIN® GMA Audio Control Panels are offered, including connector kits, mounting trays, back plates, audio and USB cables and others. Parts and accessories come with a Certificate for Conformance as standard. For parts used in GARMIN® GMA certified Audio Control Panels, these can be accompanied by FAA Export 8130-3  Forms at additional cost whenever required. Please specify the needed certification at the time of ordering.

UMA Non TSO'd airspeed indicators are offered in 2-1/4" and 3-1/8" Single (MPH) and Dual Range (MPH/Knots) versions for installation on experimental aircraft only. They are housed in Valox 420 plastic cases and weigh 8.6 oz. . Depending on the selected indicator, ranges are in MPH, Knots or kilometers. Some inicators are also offered as certified (FAA TSO'd) units. Standard dial markings are black and white. Optional custom range markings and optional internal lighting(*) are also offered upon request at additional cost. Please indicate the markings option (if markings are required) and lighting option at the time of ordering. 

(*) Note: An inverter is required for the Internal Lighting Option.

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.

Connectors are used on electrical wiring harnesses and are essentially enclosures (i.e., shells) which house contacts with wires. The electrical connection into the system at the contact termination is either a soldered or crimped connection (the latter removable from the connector with the use of a special tool). The shell and insert may be moisture resistant or a hermetic seal. The inserts in each connector must be oriented for correct mating, and the shell or insert usually contains a keying feature to prevent miss-mating that could damage the connector or result in an electrical problem. 

Connectors can be of a Plug (“male”) or Receptacle (“female”) type. Receptables are also termed as sockets or jacks. Plugs have prolonged connecting pins which fit into the mating sockets. Receptables have mounting features such as a flange with holes. Connectors used in aircraft are mostly those complying with Military Standards (MIL-STD) and Military Specifications (MIL-SPEC).

Different connectors, structured in series, are offered as part of our own branded (AVIATIONEU NEW ERA) product lines to provide cost-effective solutions for a variety of applications. Sourced by quality suppliers, they are available in plug or receptable types. 

AVIATIONEU NEW ERA MIL Standard MS5015 series connectors meet MIL-C-5015 specification. They ensure high electrical capability and durability at an acceptable cost and can be used for a range of applications including military ground support equipment, aircraft installations and others. Available in different case sizes (10SL,14S,16S,18,20,22,24,28 and 32) and  sold by the piece (pc.).

Product Specifications:

Shock: 490 m/s2

Relative humility: 95+-4% at 40℃ 

Insulation resistance: 5.000 Mega ohms minimum (at 25°C) 

Frequency Range: 10-2000Hz/147m/s2

Voltage Rating: 500VAC 700VDC 

Mating Type: threaded coupling

Termination : Solder

Durability (mating) ≧ 500 cycles 

Temprature Range:  -55°C ~ +125°C

EASA Certified VHF transceiver 57mm with 6W output power. Automatic selection of 8.33kHz/25kHz spacing and OLED display.

Manufactured with high quality PC/ABS, the AERA 660 Panel Dock by AIRGIZMOS, maximizes its use by placing the GPS right in the aircraft  panel and hold securely in place without blocking any other instruments.  It makes GPS touch screen controls easier to navigate and matches the look and feel of the rest of the avionics stack, resulting in a pleasant, professional looking panel. Dimensions are 6.25" wide by 4.25" high.

Garmin has reduced the number of connectors on the AERA 660  by using a docking connector. This docking connector has been integrated in the design and nests into the back of AIRGIZMOS Panel Dock. For upgrades from an older Garmin GPS, this panel dock has been designed to fit the same opening as those for AERA 496 or 500 and uses the same hole layout for mounting.

White LED White LED Anti-Collision Head Light Assemblies by WHELEN AEROSPACE TECHNOLOGIES (WAT) consist of the Anti-Collision Light (P/N: 01-0771987-00) and the Flasher Assembly  (P/N: 01-0771985-17) sold separately. They are designed to replace the legacy strobe light (01-0770818-00) and power supply (01-0770006-12 and 01-0770006-17) system on Cessna single engine restart aircraft 1996 & newer. FAA/PMA Approved. When replacing either the 01-0770818-00 strobe assembly or 01-7000617 power supply, both 01-0771985-17 and 01-0771987-00 are needed to convert to LED.

Technical Specifications:

LED Color - Aviation White

Current Draw: 28 Volts 0.3 amps avg. 

Dimensions:  

01-0771987-00 Anti-Collision Light: L 3.17" (81mm) x W 1.42" (6mm) x H 1.18" (30mm) 

01-0771985-17 Flasher Assembly:  L 3.93" (100mm) x W 3.10" (79mm) x H 1.38" (35mm) 

Weight:  

01-0771987-00 Anti-Collision Light: 0.14 pounds

01-0771985-17 Flasher Assembly: 0.48 pounds

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

LORD Corporation AM Series Low Profile Avionics Mounts (also referred to as isolators)) set the standard for compact, highload, high-capacity isolators. They are designed to support and protect avionics equipment in all types of aircraft. Inertial guidance and navigation systems and radar components are examples of applications where these mounts are used. In addition, AM Series mounts are used to isolate engine/aircraft accessories such as fuel controls, pressure sensors and oil coolers. These mounts  are tested and approved to the environmental tests appearing in MIL-STD-810 or MIL-E-5400. They may be used in a temperature range of -65°F to +300°F (-54°C to +149°C) for BTR® Silicone and -40°F to +300°F (-40°C to +149°C) for BTR® II Silicone. They are made with specially compounded silicone elastomers which exhibit excellent resonant control evidenced by the low transmissibility at resonance. These designs also provide linear deflection characteristics.

LORD Corporation AM Series vibration isolators are offered in different sizes and capacities. Please refer to the attached documentation.

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.

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

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.

Electric 12V Fuel Quantity Sender 10-180 Ohm for Mitchell Fuel Quantity Gauge D1-211-5074. For 24V operation, order P/N PE-111-4074 Resistors for each instrument.

RS FLIGHT SYSTEMS develops and manufactures avionics for general aviation and flight test equipment. RS FLIGHT SYSTEMS range of avionics includes Engine Management Units for Rotax 912 iS / 915 iS engines, engine panels, automatic propeller speed control unit (SCU), and SCU front panel, iS Data Recorder for Rotax iS engines (912iS / 915iS / 916iS), control panels, portable test bench for independent drive of BRP Rotax iS engines, real-time wind indication system, Fly by wire control sticks, CANaerospace based flight test instrumentation  and more. 

The RS FLIGHT SYSTEMS 2nd generation ROTAX® 912iS/915iS Engine Management Units (EMU) include 2 cockpit mounted engine monitoring, data logging & propeller control devices, EMU 912iS evo & EMU 9xiS. Both feature the same hardware, software and functionality but differ in dimensions and weight. They integrate seamlessly into the Rotax 912iS/915iS engine wiring harness, providing indications of all available engine parameters, engine status, ECU faults and additional sensor inputs. Suitable for 14 V and 28 V aircraft electrical systems with minimum installation effort. Configurable for use with different unit systems. Additional features: sunlight-readable backlit display, dual optically isolated CANaerospace data bus interfaces for retained redundancy, continuous monitoring and health checking of both ECU display buses, georeferenced data recording of all parameters at 10 Hz over up to 2,000 hours, simple data transfer & software update via an integrated memory card slot, sophisticated visualization & processing tool for recorded data, Google Earth file export of recorded data inc. GNSS and engine data. Wiring Harness Kit (incl. power supply wires) is also available (sold separately). A separate module (sold separately) provides connection to 912/914 carburetor Rotax engines.

For more information on RS FLIGHT SYSTEMS products please consult the Product Description section and the supplied documentation.

For use with most GPS and TAWS systems. Works well with most of today's mode S transponders.

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.