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

DUKANE SEACOM, wholly-owned subsidiary of HEICO Corporation, is the world’s leading supplier of FAA / EASA  & BSH qualified (Certified) high-impact underwater acoustic beacons for  the commercial air transport, business and regional jets, as well as fixed and rotary wing commercial and military markets. Other products in DUKANE SEACOM range include marine underwater beacons for Voyage Data Recorder (VDR) applications and Emergency Locator Transmitters (ELT) separately listed.

The DK120/90 was the first ULB certified to provide a minimum of 90-day underwater operating life. Certified to TSO-C121b & TSO-C142a and ESO ETSO-C121b & ETSO-C142a. Airframe mounted DK180 series low frequency beacon is designed and qualified to meet the newly developed standards FAA TSO-C200 / ETSO-C200 dated 6/26/2012 as per SAE–AS6254 & ARINC 667. For applications not requiring compliance to the 90-day operating requirement, the DUKANE SEACOM DK120/90 and DK140 (short) are still available.  An overview of DUKANE SEACOM Aviation  Underwater Location Beacons is provided in the Product Description Section.

 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 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.

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.

The AVIASPORT fuel pressure gauges  have been designed especially to measure fuel pressure in Rotax® engines 912 and work both with 12V and 24V systems. Unlike mechanical gauges, the AVIASPORT ielectronic gauges use a high precision sensor to be installed close to the engine, preventing fuel lines in the cockpit. These gauges are sold without sending units or as kits with matching senders whenever specified.

YAESU rechargable batteries are intended for use with YAESU handheld transceivers.

Lightweight, FAA-PMA approved compact power supply unit from WHELEN AEROSPACE TECHNOLOGIES (WAT) for installation in the wingtips and tail of the aircraft, eliminating long runs of high voltage interconnecting cables. Only an 18 gauge low voltage wire supplies power to each power supply and between wingtip mounted power supplies and switch. This system is not synchronized. Flashes 50 times per minute (comet flash).

Product Specifications:

Wt. 1.2 lbs.

Size: 5"L x 3"W x 3.06" H.

Current 1.7A -14V, 0.85A - 28V.

FAA-PMA Approved.

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.

The EDM 930 by JPI collects and displays engine data in a useful way. This EDM monitors engine temperatures and voltages, adjusts the fuel/air mixture, and diagnoses engine malfunctions. The EDM 930 display screen is arranged into three sections. The top left is the RPM and MAP section. The bottom left is the Scanner® section. And the right side is the Bar Graphs section. 

The RPM and MAP Display shows the RPM (Revolutions per Minute) and the MAP (Manifold Pressure).

The Bar Graphs Display shows:

- Oil temperature

- Oil pressure

- Fuel pressure

- Bus voltage

- Amps load or charge/discharge

- Outside air temperature (or owner selectable )

- Fuel flow, units per hour

- Left fuel quantity (or owner selectable)

- Right fuel quantity (or owner selectable)

The Scanner Display has the exhaust gas temperature (EGT) bar graph presentation as its central part with additional Cylinder Head Temperature (CHT) and TIT indications.

EASA Certified 10 W Comm Radio with 25 kHz spacing.

Manufactured with high quality PC/ABS, the AERA 500 Panel Doc by AIRGIZMOS, maximizes its use by placing the GPS right in the aircraft  panel and hold securely in place without blocking any other instruments. Aera 500 Panel Dock™ is suitable for the  Garmin AERA™ 500 series of GPS (500/510/550/560). 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 500 series  by using a docking connector. This docking connector has been integrated in the design and nests into the back of AIRGIZMOS Panel Dock.

The PAI-700 TSO'd Vertical Card Compass is manufactured exclusively by Precision Aviation, Inc. This non-liquid (dry) type compass is magnet driven thus it is subject to lead and lag, however, these tendencies are greatly reduced due to the absence of pendulosity.  It is inherently stable due to the use of eddy current damping which is a natural phenomenon built into the basic design and as such has no overshoot. The PAI-700 has been designed to replace the float/liquid type compasses eliminating leaking fluid or backward azimuth readings. Available for Southern and Northern Hemisphere and different supply systems (5V, 14V and 28V). Precision Avionics Inc. also manufactures different compass brackets for overhead or glare shield mounting.

The Precision PAI-700  Vertical Card Compass consists of a 2" vertical rotating dial which is compared with a fixed miniature airplane (lubber line) to present the magnetic heading of the aircraft at all times. Heading information is more natural because the heading is read at the12 o'clock position and off the nose of the miniature aircraft. The compass card rotates and presents all quadrants in their true relation to line of flight. Requires no power (except for lighting) to operate. Installed in many current production aircraft & helicopters. Size: 2-7/8"H x 2-3/8"W x 2-1/8"D. Wt. 0.6 lb. After installing compass must be compensated using standard compensation procedures. Also used in sailplanes.

Note: Compass deviation card is included. A mount, sold separately, is required for installation with the unit.

The  MID CONTINENT® INSTRUMENT (MCI) MD–90 Series Precision Quartz Clocks provide  an ideal solution for accurate time-keeping, and consist original equipment for many major aircraft manufacturers. Designed for accurancy, the 2-inch MD–90 Series clocks are manufactured to meet rugged aircraft environmental standards, they are FAA/PMA certified and offered in standard MD–90–1 and MD–90L versions, both operating with 8–32 VDC power input. Their key features include:

Precision quartz movement

Compact 2-inch size — fit standard panel cutout

Lighted version available with field-replaceable light tray

Transient and reverse polarity protection

Extremely low current consumption (3 mA) 

Continuously powered by aircraft battery

FAA PMA certified

Designed and built in the USA

One-year limited warranty

Product Specifications:

Power Input: 8–32 VDC - 3 mA max (without lighting) 

Accuracy:  ±30 seconds in 24 hrs 

Dimensions: 2.5 x 2.5 x 3.2 inches max 

Weight: 0.5 lbs 

Temperature: –40°C to +82°C (–40°F to +180°F) 

Altitude: –1,000 to +55,000 feet 

Humidity: 0 to 95% at 25°C 

Vibration: .02 in. dbl. ampl., 1.5g @ 5 to 50 Hz 

Mounting: Front or rear panel mounted 

Connector: #6-32 threaded terminals

For additional information please consult the supplied documentation.

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. 

Solid State Cockpit Voice Recorders (SSCVR) and Flight Data Recorder (FDR), aka "black boxes", are required by Civil Aviation Authorities to be installed in large commercial aircraft and some smaller commercial, corporate, and private aircraft used to help reconstruct the events leading to an aircraft accident. Manufactured by various manufactuers such as HONEYWELL AEROSPACE, UNIVERSAL™ AVIONICS and others they are offered in different models, as CVR, FDR or combined systems, certified by FAA, EASA and other CAAs and available in NEW Condition but also as USED (OVERHAULED) units for straight purchase or exchange. For additional information please consult the Product Description section, the supplied documentation or contact us for a quotatin.

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™ 328 solid-state Mode S digital transponder covers EU VFR Mode S requirements and is IFR certified for aircraft operating under 15,000 feet and with a true airspeed of under 175 knots. The GTX™ 328 includes many of the features of the GTX™ 330 transponder  at an affordable price such as outside air temperature, count up/down timers, altitude monitoring, density altitude functions, front-panel input for flight ID and has a digitised voice output for pilot warning of altitude limits or timer expiration.

1-1/4 inch TSO'd Electronic Fuel Pressure Gauges from UMA INSTRUMENTS. Black & White dial marking. Available in different pressure (PSI) ranges. Case: Aluminum. Weight: 4.0 oz. UMA sensors are sold separately.

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).

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

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.