4-Pin connector by AMPHENOL for use in all electrical gyros (DG or Horizon) including Falcon models.

PS ENGINEERING has revolutionized audio control in general aviation airplanes. At that time, the original PMA6000 took the audio panel from a collection of switches added as an afterthought, to a multitalented intersystem focal point for cockpit audio.

Radio selection, cockpit communications and even music were seamlessly combined in the modern audio control panel. The PMA6000-series set a benchmark for all GA audio panels that followed.

The next generation PMA6000B benefits from PS Engineering's long experience of audio panel control design and manufacturing experiences. It is an excellent low cost audio panel alternative to the higher end systems that PS Engineering has become so famous for. 

The PMA6000B combines an audio selector panel with a top-quality manually adjusted 4 place VOX mono intercom and a slew of features to enhance versatility and utility. The PMA6000B holds both FAA TSO as well as EASA ETSO and was designed to be made easier to install because of a single 44-pin Sub-d connector. Different PMA6000B models offered with or without marker beacon receiver.

Product Features:

Built-in 4 place mono intercom PS Engineering's ""Set-it and Forget-it"" manual VOX

Optional built-in marker beacon receiver

Split mode for dual audio capability

2 - Com Capability

3 - Intercom isolation modes - Pilot Isolate, All, and Crew

2 - Music inputs with Soft Mute™

2 - Unswitched inputs

6 - Switched inputs

A patented ""swap"" function allows selection of Com 1 or Com 2 from remote pushbutton

Fail-safe feature automatically hard-wires the pilot to Com1 in the case of an outage

Single 44-pin connector making installation easier

Certification: FAA TSO/EASA ETSO

Warranty: 24 months

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 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.

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.

The AVIASPORT indicators (gauges) are reliable, accurate and solid, combining the accumulated experience of more than twenty years with the latest technology  They have been designed for ROTAX engines and their display areas are divided into red, green and yellow zones in line with Rotax limits. They use a pointer that turns 240º or 320º, providing high resolution. AVIASPORT range of gauges includes CHT, EGT, tachometers, oil and fuel pressure, oil and coolant temperature, fuel level, voltmeters & ammeters and offered with casings of different sizes: 80mm; 57mm and 52mm.

AVIASPORT Oil Pressure indicators (gauges) are designed specifically for ROTAX 912/914 aircraft engines with painted red, green, and yellow gauge markings. are available in two sizes: 52 and 57 mm. They are offered in two unit versions for readings in PSI or Bars. They work with different pressure sensors depending on these installed in ROTAX 912/914 engines: the VDO sensor (Before September 2008) or the 4..20mA sensor (after 2008).

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.

The STRATOMASTER VEGA range instruments/indicators from MGL AVIONICS includes different 2 1/4" (57mm) microprocessor based color display instruments operating over a wide supply voltage range of 8 to 30V DC with with built in reverse and over voltage protection. They are non certified and only suitable for installation in experimental and sport  (LSA) aircraft. Using a high resolution color graphics display, these instruments/indicators provide excellent daylight readability with built in backlighting making them easy to read at night time. They include a rotary control plus 2 independent keys for easy menu navigation and to access specific instrument features. Sensors are also offered to enhance their functionality. The MGL AVIONICS STRATOMASTER VEGA Series instruments/Indicators include: Artificial Horizon & Magnetic Compass Display, Altimeter/VSI, ASI, ASI/VSI, Engine Monitoring System (EMS), Fuel Computer, Information Display, Manifold Pressure, Température, RPM, Hobbs, Universal Engine/Rotor RPM, Hobbs, 4-Channel Thermocouple (EGT/CHT), 4 Channel Universal Analog Input (Pressure/Temperature/Voltage/Current) and NAVCOM Control head for MGL N16 NAV/COMM or V16 COMM VHF.

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).

The HONEYWELL BENDIX KING® KI 525A HSI is a pictorial navigation indicator used in the KCS-55A compass system which also includes KG-102A Directional Gyro, KMT-112 Magnetic Azimuth Transmitter (flux valve), KA-51B Slaving Control & Compensator Unit and optionally KA 52/KA 57 Autopilot Adapters. It was a popular avionics upgrade for light aircraft until the advent of the Sandell electronic HSI and, more recently, glass-cockpit systems from Garmin, Aspen and others. This indicator combines the display functions of both the standard directional gyro and the course deviation indicator offering the pilot a single view of the horizontal navigation situation. It greatly simplifies course orientation, interception, and tracking resulting in less work from the pilot. Internally lighted, the KI 525A operates at 14 or 28 VDC.

The HONEYWELL BENDIX KING® KI 525A HSI is available in different models to serve application requirements:

- with bootstrap heading synchro to provide source of slaved heading information for any device, such as an autopilot

- with glideslope needle damping for use in high vibration environments such as helicopter

- capable of operating at either 30Hz or 400Hz

- capable of operating at 14 or 28VDC and 5 volt operation

Like other KCS 55A compass system components, the  KI 525A indicator can be furnished in NEW condition or as USED in Serviceable or Overhauled conditions indicated respectively by the letters "SV" and "OH" in the product reference numbers (SKU and  accompanied by the relevant certification (e.g. yellow tag, 8130-3 form). They are also offered as exchanges / trade-ins  for returned customer owned units indicated by the letter "EX" in the SKU.  In the case of an exchange/trade-in option of a customer unit, the  full selling price of the ordered unit is charged and the core credit is refunded or credited towards future orders when our co-operating supplier verifies that the unit is in a reasonable, repairable condition. It is recommended that this option is selected by our customers mainly for upgrades and only in cases when their units are functioning properly at the time removal from the aircraft. In cases when customer units are found by our supplier to be non-repairable, the core deposit shall not be refunded and shipping charges shall apply if customers wish the return of these units to them. Please refer to the Product Description section for technical specifications and additional information.

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.

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

Designed to help the pilot determine altitude by measuring existing atmospheric pressure, the altimeter translates the measurement into “height above sea level.” This is indicated on the dial of the instrument in feet, which requires setting the barometric pressure in the Kollsman window.

UNITED INSTRUMENTS 5934 series are FAA TSO'd 3"/ 3-pointer altimeters, intended for use with most single engine, turbo/piston prop aircraft. They are offered in 5934 and 5934A models with respective maximum calibrated ranges  of -1.000 to 20.000 feet and  -1.000 to 35.000 feet respectively. All lighted instruments require a light tray sold separately.

Product Features:

Affordable, certified 3-1/8" case for half the cost of existing systems

United series 5934

All units approved to FAA TSO (C10b,C2b and C4c)

Anti-reflective glass enhances visibility and reduces pilot fatigue

Altimeter available with right-hand or left hand knob 20,000 or 35,000 ft. Hg or Mb

All instruments are made in the USA

One year limited warranty

Product Specifications:

Typical Weight: 13 oz

Number of Pointers: 3

Barometric Setting: 28.1 to 31.0 in HG / 946 to 1050 mb

Calibrated Ranges: -1,000 to +20,000 or +35,000 feet

Static Pressure Connection: 1/8-27 ANPT

Installation: Removable Spring Nuts and screws

For additional information please consult the supplied documentation.

Range of special accessories by FRANZ AIRCRAFT ENGINES for use in BRP-ROTAX® aircraft engines and other applications.

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

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.

EASA Certified VHF transceiver with 6W output power and 8.33kHz frequency spacing.

RAY ALLEN (RAC) R2S Rocker Switch provides a very positive snap action in 2 directions and returns to a center off position. It was designed specifically for Ray Allen trim systems. It is wired to connect both power leads to ground when the rocker is released. This eliminates motor coasting and allows very precise trimming. The RS2 switch is rated at 1amp. The faceplate measures 1.75" (44mm) x 1.0" (25mm) x 1.47" (37mm) deep. Self adhesive labels are not included. Sold separately.

This 2-1/4 inch flap indicator uses a resistance potentiometer as a flap position sensor. Transmitter is required. Wt: 9.8 oz.