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.

FALCON GAUGE Non Certified Airspeed Indicators have been one of the most chosen flight instruments by fixed wing airplanes, helicopters and ultralights. The great advantages of these gauges are excellent slow speed characteristics, very progressive increments, a variety of ranges, light weight, short length, and affordable price. FALCON GAUGE Airspeed Indicators ranging up to 80 MPH, 100 MPH, 120 MPH and 150 MPH make for excellent MPH increments for helicopters and ultralight aircraft. All FALCON GAUGE Airspeed Indicators are housed in an aluminum case and consist of all metal parts. They come in 2-1/4" and 3-1/8" sizes. Available ranges: MPH, Knots, KPH; single range or dual range readings. Optional: Custom color range markings can be special ordered. For additional information please refer to the supplied documentation or contact us.

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.

These UMA new manufacture NON TSO'd electric ammeters offer accuracy, rugged construction, and contemporary styling. They are available in different  measurement ranges with a 270° sweep and are suitable for installation in 2-1/4" panel hole diameters. Made in U. S. A. and furnished with shunt.

The HONEYWELL BENDIX KING® KMT 112 is a Magnetic Azimuth Transmitter (aka Flux Detector or  Valve) which senses the direction of the earth’s magnetic field and continuously transmits this information through the slaving circuitry to a directional gyro (such as the HONEYWELL BENDIX KING® KG 102A or KSG 105 slaved directional gyros). This sensor is mounted remotely, usually in a wingtip, to eliminate the possibility of magnetic interference. The KMT 112 is typically used in HONEYWELL BENDIX KING® KCS 55A and KCS 305 compass systems. The KMT-112 flux valve is a sealed unit and cannot be serviced or have parts replaced. The unit must be replaced when/if it fails.

Like other KCS 55A compass system components, the  KMT 112 transmitter 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. 

Installation parts and manuals are sold separately. 

For additional information and technical specifications please refer to the Product Desscription section, the product presentation of the HONEYWELL BENDIX KING® KCS 55A compass system or contact us.

AN5771-4A style 2-1/4 inch hydraulic pressure gauge with steel case connecting directly to the aircraft's hydraulic system. Fits in a 2-1/4" dia. panel opening and has a threaded 1/4"  connection for a fitting. Range: 0-2000 PSI. Only available in Overhauled Condition. Certified with fresh Matte-white dial. Yellow-tagged. Limited availability.

For new design projects and applications please refer to the presentations of alternative TSO'd and non TSO'd electronic hydraulic pressure gauges and pressure senders offered. 

Pressure Transducers (Senders) whenever required, ARE NOT INCLUDED in the prices of hydraulic pressure gauges. They are sold separately.

Note: A yellow tag is similar to a FAA 8130-3 Serviceable tag both denoting the "Serviceable" condition of the product i.e. it has been  repaired as needed, tested according to the manufacturer's procedure, meet the manufacturer's performance specifications and ready to return to service. Yellow tags are issued and widely accepted in North America while a FAA 8130-3 Serviceable tag is is accepted worldwide. The acceptance of yellow tags by national Civil Aviation Authorities should be checked by potential buyers prior to ordering.

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.

OMRON A16 series pushbutton 16-dia. cylindrical body switches are detachable switches. The same contacts can be used for both standard loads and microloads. Their miniature design of 28.5 mm makes these switches the smallest class in the industry. Easy-to-wire terminal arrangement. Certified for EN 60947-5-1. These switches are offered in lighted and non lighted versions, different colors, display shapes, with LED or incandescent lamps and different socket units. Please consult the attached documentation for ordering.

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

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

DAVTRON M301 Series Outside Air Temperature (OAT) digital indicators are FAA-PMA approved and come complete with digital probe, in Fahrenheit or Celsius models and different versions. They require minimum panel space. Other features include: light weight, automatic dimming, miniature remote probe, sunlight readable display and a laser engraved faceplate. A 3-pin connector is installed on probe as an option for an additional charge.

KANARDIA HORIS Air Data-Attitude/Heading Reference System (AD-AHRS) includes several state of the art sensors and combines them into a small PFD display. It can serve as standalone PFD displays and it can be used as a primary instrument or as a perfect backup. It is offered as standalone (master) device with integrated sensors or as a slave unit when an I-ALT-IAS or EMSIS PFD or NESIS are present on the CAN bus. AD-AHRS standalone unit shows: attitude (roll, pitch), airspeed (IAS and TAS), vertical speed (Vario) indication, altitude, outside temperature, QNH setting, heading rate (1 minute and 30 seconds turn), tracking course (True or Magnetic). It is offered for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15") and comes supplied with digital outside temperature sensor.

Product Features:

very low power consumption (< 2W at 12V),

low cost,

precise altitude pressure and IAS (indicated airspeed) sensor – connects to pitostatic,

precise angular rate sensors – gyros and accelerometers,

GPS receiver,

digital outside temperature sensor,

lightweight design (weighs only 235 g),

CAN bus compatible.

Available Options for HORIS AD-AHRS 57/80 (sold separately). They must be specified at the time of ordering.

MAGU Electronic magnetic compass.

AP-K Two servos for the two axis autopilot function. Must include also AMIGO.

AMIGO Autopilot panel for direct access to Autopilot functions. Must include also AP-K.

The LXNAV G–Meter  (accelerometer) is a standalone unit, designed to measure, indicate and log g–forces. The unit is offered in 57 mm or 80 mm diameters for installation into the aircraft instrument panel. It comes in two versions, standard and with flight recorder (FR).

The LXNAV G–Meter has an integrated high precision digital pressure sensor and inertial system. The sensors are sampled more than 100 times per second. Real Time Data is displayed on a QVGA 320x240 pixel 2.5″ high brightness color display. To adjust values and settings the LXNAV g–meter has three push buttons with fixed functions. The top button is ESC (CANCEL), the middle is to switch between modes and the lower button is the ENTER (OK) button.

The unit's inertial platform integrates a  ±8g accelerometer. Device is showing current g–load in navbox/needle and it’s min-max values in bar. Last flight min/max load navboxes are persistent till next flight. Min/Max limits with Warning zones can be defined.

Real Time Data is displayed on a QVGA 320×240 pixel 2.5-inch high brightness color display.

The Logbook menu displays the list of flights. If the RTC time is set properly the take-off and landing time shown will be correct. Each flight item consists of the maximum positive g–load, the maximum negative g–load from the flight and the maximum IAS. This function is available only with “FR” version.

Product Features:

• An extremely bright 2.5″ QVGA color display readable in all sunlight conditions with the ability to adjust the backlight.

• Three push buttons are used for input.

• RS232 input/output.

• Micro SD card

• 320x240 pixels color screen for additional information such as minimum and maximum g–force

• Built in RTC (Real time clock)

• Logbook

• 100Hz sampling rate for very fast response.

• Power supply cable included

UMA  2-1/4" electric tachometers with their high resolution and easy to read displays were designed to offer aviation styling and performance for all types of aircraft. The analog model has a 270° sweep which provides great resolution in both the 3500 and 7000 ranges. The digital model has a bright LED display. Separate power source required. Installation is simple and instructions are included. They can replace mechanical tachometers in Lycoming/Continental engines.

Current: 80 milliamps ­ Size: 2.25" round x 2.75"deep.

 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.

MITCHELL FAA PMA'd D1-211 Series  modular 1-1/2 " fuel quantity square  gauges can be stacked in horizontal and/or vertical rows in any position in the aircraft panel. These  modular gauges are internally lighted and are plug removable from the front of the panel for easy maintenance. Available in different sender resistances for the indication of fuel quantity in the aircraft's left or right fuel tank.

The RCA 82A/83A Series TSO'd turn coordinators by KELLY MFG (RC ALLEN) can be found in many production aircraft around the world. They Incorporate an electrical gyro turn indicator with an inclinometer. The turn motion is presented by an airplane symbol banking on a fixed horizon. The inclinometer, by movement of a ball in relation to the lubber lines, indicates the slip angle of aircraft while in a turn. The airplane on the dial rotates with reference to the indices. A power failure flag drops into view whenever the supply voltage is lost or when dropped below a level acceptable for proper operation of the gyro. Operates from 11 to 30VDC. Available in lighted and unlighted versions. First installation requires electrical connector and clamp. Mating Connector: MS3106A-10SL-3S.

Product Specifications:

Meet or exceed requirements of FAA TSO C3b 

Made in the USA

Dimensions

Length: 6 1/5 in. Max

Width: 3 3/8 in Max

Height:3 3/8 in Max

Weight: 1.9 lbs.

Description: 

Unlighted

Mating Connector:

MS3106A-10SL-3S

Connector pin out:

A: +12 -30VDC

B: Ground

C: Spare

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.

GARMIN GI-106B TSO'd panel-mounted CDI is a high-quality course deviation indicator which includes a VOR/LOC/GPS needle as well as a glideslope needle, that can be hidden and disabled by an installer if the glideslope functionality is not needed. The GI 106B contains LED-lit GPS, NAV and VLOC mode annunciators, for an easy-to-read and modern look. TO/FROM annunciators are also LED, and when invalid, the needles are simply hidden out of the pilot’s view instead of using conventional invalid flags. The GI 106B replaces existing Garmin GI-102A & GI-106A models. It is compatible with the same pinout connections as the legacy GI 102A and GI 106A course deviation indicators, allowing for an easy upgrade path. It also features anti-reflective lenses and LED flood lighting for viewing at night.

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.