Static dischargers, commonly known as static wicks or static discharge wicks, are installed on the trailing edges of aircraft, including (electrically grounded) ailerons, elevators, rudder, wing, horizontal and vertical stabilizer tips. They are high electrical resistance (6-200 megaohm) devices with a lower corona voltage than the surrounding aircraft structure and used on aircraft to allow the continuous satisfactory operation of onboard navigation and radio communication systems during precipitation (p-static) conditions.  This wick comes with 2 holes to rivet to trainline edge and plain wire extension. Eligible For Installation in aircraft: Beech Baron 58, Cessna 402, Eurocopter: BK117, BK117 C-2.

DAVTRON Μ475 Series 2-Function voltmeter/ammeter digital indicators are FAA-PMA approved and come in 475VA/475VAA models and versions, both with lighting capability. Model M485VA ls made primarily for remote shunts. They are both designed for low current drain ( .001 Amp) and are also used in standby and emergency battery packs. Other features include: 

Plus Or Minus Amp Range: 150.0 

Plus Volt D.C. Range: 100.0 

Sunlight Readable Display

One Tenth Amp Resolution

One Tenth Volt Resolution

1.3" case depth

2-1/4" Standard mount

SWIFT AIRCRAFT manufactures Swift two-seater low wing composite aircraft with striking elliptical wings and double curvature surfaces. Comfortable, safe and environmentally sound they are designed and manufactured entirely in the UK, and available globally,

The company also manufactures Swift aircraft gauges specializing in precision-engineered gauges, including Exhaust Gas Temperature (EGT) and Cylinder Head Temperature (CHT) gauges, commonly used in aviation.

Sigma-Tek 5000B Series Attitude Indicators (Artificial Horizons) are air-driven gyros that have a pictorial horizon mask and fixed airplane. The mask moves to indicate climb, dive, and bank. Bank and pitch attitudes are displayed so that the pilot’s sensing of the gyro indication is the same as the interpretation of the relation between the wings of the aircraft and the natural horizon during visual flight. These instruments are FAA certified (TSO-C4c), and can be used to replace the aircraft’s turn coordinator when equipped with an inclinometer. Different versions available mainly based on the layout, dispay colors, warning flag and lighting capabilities. Lighted indicators do not include lamp trays which are sold separately based on the aircraft voltage (14V or 28V).

 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.

The SWITCHCRAFT® line of jacks and plugs is ideal for instrumentation and audio connections. They can be used in a variety of applications such as medical equipment, manufacturing data equipment, GPS tracking and data logging systems or security applications.

The product line includes 1/4", .141", .206", 3.5 mm, DC Power, Bantam TT, .101" Micro, Aircraft jacks and plugs and 2.5mm Surface Mount,  MDSMT series jacks.

The SWITCHCRAFT® range of Headphone/Microphone jacks come with nut and washer and feature contact springs are of special alloys for long life, insulation is high dielectric strength phenolic, tinned terminal lugs for easy soldering and short frame. They mount by 3/8-32 threaded bushing and nut. Open circuit until plug inserted. Different jacks are offered including:

SWC-11-JJ-034 MONO Headphone Jack - 2 circuit conductor

SWC-12B STEREO Headphone Jack - 3 circuit conductor 

SWC-S12B -JJ-033 Microphone Jack - 3 circuit conductor 

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

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.

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

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

DYNON AVIONICS AOA/Pitot probes perform two functions: airspeed and angle of attack sensing. These functions require having two pressure ports on the tip of the probe. The normal pitot pressure port is on the front face of the probe and is designed to be insensitive to angle of attack. The second pressure port is located on an angled surface just under the pitot port and is designed to be very sensitive to AOA. They are under-wing mount, L-shaped  probes which can be installed  easily with simple plug-n-play integration with Dynon and Advanced Products.Their installation requires a mounting bracket sold separately. The pressure from each port is delivered via separate air lines to the instrument where they are compared to previously calibrated scenarios specific to the aircraft. Competitively priced, they are offered in Non-Heated and Heated versions. The Heated AOA Pitot includes a nichrome heating element that is regulated by a separate pitot heater controller unit supplied with the pitot. The controller actively monitors a temperature sensor embedded within the pitot head and regulates the power to maintain a constant temperature. This not only conserves energy but additionally prolongs the life of the heater. The controller also outputs a signal that can be wired to a warning light in the cockpit to warn the pilot anytime there is a malfunction or that the pitot is turned off.

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

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.

JEPPESEN NavData Databases are offered for different GARMIN AERA portable GPS models such as 500/510, 550, 695 and 795. They are available for different geographical regions. JEPPESEN NavData databases can be included only in the respective orders of GARMIN AERA GPS units. Orders for these database and their 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.

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.

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.

Air data include total pressure of the airflow measured by pitot tubes, static pressure of the ambient air by static ports (or both pressures by pitot-static tubes), total temperature (higher than the actual air temperature due to friction and adiabatic compression) by TAT sensors, and angle of attack (i.e. angle between the airfoil and the airflow) by AoA sensors. All these data are vital for aircraft flight and in the case of large civil or military aircraft, once collected are fed to  an air data computer (ADC).

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. Their 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. 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.

AEROSONIC® fuselage mounted static pressure ports are engineered to meet or exceed industry specifications to supply ambient static pressure measurements to air data computers, altimeters, airspeed indicators and vertical speed indicators in numerous types of aerospace applications. The Static Pressure Ports’ electrical heating elements prevent ice accretion and water ingestion ensuring the performance of primary flight instruments is not degraded even under the most severe atmospheric conditions.

For additional information please refer to the Product Description section.

OMRON M2C Series cylindrical indicators have the basic design as the A3C pushbutton switches. They have a cylindrical 20-mmX12-dia. body making panel cutouts easier and provide good illumination with even surface brightness. These indicators are offered in lighted and non lighted versions, different colors, display shapes, with LED or incandescent lamps and different socket units. UL (E41515) and CSA (LR45258) approved. Please consult the supplied documentation for ordering.

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.