MFD combining IFR GPS navigation, COMM/NAV and enhanced situational awareness capabilities.

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™ 325  is a Mode A/C panel-mounted full-featured, TSO'd certified transponder offering a simple, affordable replacement for standard Mode C transponders. It features aural alerts, total air temperature (TAT), pressure altitude readout, altitude monitor function, density altitude readout, built-in timers and automatic ALT/GND mode.  ‬It replaces the popular GTX™ 327 ‬and is essentially the same unit‮—‬but carries the GTX™ 335/345‭ ‬display and button layout‭. ‬It would be a meaningful ‬choice for the replacement of an older Mode C ADS-B‭ ‬Out transponder. 

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

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).

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 Turn Coordinator is used for displaying the angular rate and sideslip of turning in horizontal flying and turning. The inclinometer indicates the slip angle of the aircraft while in a turn. A power failure flag drops into view whenever the voltage drops below a level for proper operation. The Turn Coordinator incorporates a built-in voltage regulator so it can be used with either 14VDC or 28VDC power system. It is compact in size and light weight eliminating radio interference.

This small, lightweight unlighted turn coordinator is excellent for homebuilt aircraft. Works for 14 Volt or 28 Volt systems. Features, power out warning flag with a 0° Panel. Fits Standard 3-1/8" Cut Out, 3-3/4" long.

The RAY ALLEN (RAC) RP4 LED position indicator is designed to be installed in the cockpit providing an indication of the servo output shaft position. This indicator supercedes and it is a direct replacement for previous RAC RP3. The RP4 indicator uses ten LED lights to show the position of a actuator output shaft (or position sensor arm). There are also two amber colored LED's, one on each end of the indicator scale, to act as a reference for the green indicator light, especially in dark conditions. The 10 LEDs are the brightest available for superior visibility in sunlight, but can be dimmed for night flight. It can be installed horizontally or vertically. 

The RAC RP4 position indicator is panel mounted using a faceplate and two countersunk, 2-56 x 7/16" screws (two spare finishing screws are included). The distance between the screw holes is identical to the older Ray Allen RP3 LED indicator. Although the faceplate dimensions are identical between the RP3 and RP4 indicators, the panel cutout size is slightly different between the RP3 and RP4. If you are replacing and older unit with a new RP4, you will only need to increase the size of your panel hole. The RP4 faceplate will cover the older RP3 panel hole.The RP4 faceplate measures 1.75"(45 mm) X .75"(19 mm) and it is 1.6"(41 mm) in depth. It is now the standard position indicator included in Ray Allen trim systems, or can be purchased separately for special applications such as a cowl or wing flap indicator.

The RP4 includes a RP4-L1 label (featuring Elev1, Elev2, Ail, Rudder, Flaps). A RP4-L2 label (featuring Cowl Flaps, < >, on/off) is also available and is sold separately. 

NOTE: Labels can only be ordered together with . In ordering these high quality labels please be advised that rocker switches and needle indicators require a large label, LED indicators use a small label. Can be only included in orders of respective RP4 position indicator(s) (not separately).

KANARDIA diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters includes different RPM, CHT, EGT and oil/temperature engine gauges. 

KANARDIA INDU Series round RPM gauges are offered as standalone (master) or as slave gauges. The slave version requires an engine monitoring unit (DAQU) to be present on the bus. KANARDIA INDU Series round RPM gauges are available for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15"). They can be supplied in the following scales:

-RTX Rotax scale (7000) and markings (yellow, green, red)

-JAB Jabiru scale (3500). Markings must be specified at the time of ordering

-LYC Lycoming scale (3000). Markings must be specified at the time of ordering

-D D-motor scale (3100). Markings must be specified at the time of ordering

-CUS Custom made scale

KANARDIA INDU Series round standalone CHT and EGT indicators are offered for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15"). Respecive sizes of these gauges are 62 x 62 x 45 mm and 82 x 82 x 45 mm. The 57 mm gauges weights 150 g and requires a 102 mA power.

KANARDIA INDU Series round standalone Fuel Pressure, Oil Temperature and Oil Pressure indicators are available for 57 mm (2.25") and 80 mm (3.15") standard panel hole diameters with same sizes and weight power characteristics as those of CHT/EGT gauges.

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 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

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

GARMIN AERA 660 Portable GPS provides affordable feature-rich navigation, stunning display and streamlined database updating. It features a 5-inch capacitive touchscreen display, Connext® wireless capabilities for database updating , Garmin WireAware™ wire-strike avoidance technology, 3D Vision of rising terrain near the aircraft, while overlaying GPS-derived airspeed, altitude and vertical speed alongside flight plan information and more. Offered with different navigation databases.

ACS PRODUCTS is a supplier of quality parts and accessories to the aircraft industry while many of their products are also used in a wide variety of other fields including marine, recreational vehicles, and industrial applications. Their product lines include cable assemblies, ignition switches as well as machined and custom products.

ACS Pitot / Pitot Static Tubes include different models. Model 15144 'L' shaped, aluminum pitot heads are simple, inexpensive, good-quality suitable for homebuilts. They are available either as pitot only or pitot static. Both have flange mounting to aid underwing fitting. 

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.

Revolution Counters (Tachometers)/HOBBS meters are used in BRP-ROTAX® aircraft engines. They are offered as certified or non certified parts from BRP-ROTAX® but also from other manufacturers.  Non certified parts can be used in ultralights or other aircraft not requiring certification of parts for their installation. Certified parts are designated by the letters "CERT" after the part number in the product reference number (SKU).

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.

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. 

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.

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.

KANARDIA INDU Series round altimeters are part of INDU diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters. They feature colour LCD display, one or two pointers  with possibility to personalise scales (in feet or meters) and LCD displays. They are offered as standalone (master) altimeters with internal pressure sensors or as slave instruments. The slave version requires 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") with one pointer and 80 mm (3.15") with two pointers. They can also be ordered with integrated backup battery at additional cost. The backup battery can also handle and additional indicator, typically an airspeed indicator.

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.