Automatic portable radio beacons (ELT(AP) АРМ-406П (ARM-406P), АРМ-406П1 (ARM-406P1) and АРМ-406АС1 (ARM-406AC1) are safety devices designed to transmit via satellite to the stations COSPAS-SARSAT distress radio signals with aircraft coordinates received from the onboard computer system.Such information facilitie identification of the aircraft and guidance of S&R facilities to the accident site. Located in the aircraft cabin these devices offer the possibility of quick use in an emergency.

The automatic portable radio beacon АРМ-406П1 (APM-406P1) includes:

- monoblock P, consisting of a double protective casing with shock absorbers installed in it, an overload sensor (DP) and an AC1A monoblock;

- remote control PDU-406 (ПДУ-406) installed in the cockpit;

- external antenna ANT-406VA (АНТ-406ВА), mounted on the aircraft body.

The АС1А monoblock is  a portable radio beacon, including a PM-AC1A (ПМ-АС1А) transmitting module, an АРМ-043-01 autonomous power supply unit and an ANT-APM-01 (АНТ-АРМ-01) antenna. The emergency mode of operation of the AC1A monoblock can be switched on both from the remote control and from the DP, as well as manually when removing it from the protective casing when leaving the emergency aircraft.

Autonomous power supply (APS) units are also offered for use with the radio beacons. АРМ-043 (CDKT.436140.590) 14.4V are intended for use for beacons manufactured before 2013 while АРМ-043-01 (CDKT.436140.590-01) 10.8V for beacons manufactured after 2013. Unless otherwise specified their replacement frequency is once every 3 years with a 3-year self life.

For additional information please refer to the supplied documentation or contact us.

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.

KANARDIA INDU Series round Vertical Speed Indicators (Variometers) are part of INDU diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters. They feature an LCD display with possibility to personalise the displays and scales. They are offered as standalone (master) VSIs with internal pressure sensors or as slave instruments. The slave version requires a master altimeter or 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") and 80 mm (3.15").

Scale Ranges:

-M scale in meters per second (-10, 10)

-FT scale in feet per minute (-2000, 2000)

-KTS scale in knots (-20, 20)

KANARDIA INDU Series round Airspeed Indicators are part of INDU diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters. They feature an LCD display with possibility to personalise the displays and scales. They are offered as standalone (master) IAS units with internal pressure sensors or as slave instruments. The slave version requires a master altimeter or 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") and 80 mm (3.15"). As an option they can be ordered with an Outside Air Temperature (OAT) digital sensor at additional cost. When static pressure (altitude) is present on the CAN bus, OAT sensor enables also the TAS  as well.

Scale Ranges:

-KMH Scale in kilometers per hour (0-280)

-KTS Scale in knots (0-140)

-MPH Scale in miles per hour (0-150)

NOTES:

A high speed sensor option is also available at additional cost (up to 460 km/h, 250 kts, 285 mph)

Arc colors need to be specified  at the time of order.

KANARDIA INDU Combo IAS/Altitude/Vertical Speed Indicators are part of INDU diverse family of non-certified gauges for use in ultralight aeroplanes, autogyros and helicopters.They feature an LCD display with possibility to personalise scales and LCD displays. They are offered as standalone (master) or as slave gauges. Slave versions require some PFD like KANARDIA NESIS, EMSIS, AETOS or HORIS to be present on the bus. KANARDIA INDU Combo IAS/Altitude/VSI gauges are available for two standard panel hole diameters of 57 mm (2.25") and 80 mm (3.15"). Arc colors need to be specified  at the time of order.

Accelerometers (aka G-Meters) are used extensively in a wide range of applications including Aviation, Marine, Automotive, Military, and others. They are also used  in inertial navigation and guidance systems in airplane and ship autopilots.They help in a better understanding of static, such as gravity, or dynamic forces due to motion or vibration acting on an object.

Original Mechanical and more recent Digital accelerometers, used on civil and military aircraft, measure the instantaneous acceleration (or G-force) of an aircraft and its occupants compared to Earth's standard gravitational pull, in units of "G" (e.g., 1G, 2G). They enable pilots to monitor flight conditions, maintain safety, or practice aerobatics or combat maneuvers. Made by different manufacturers, they are offered as non-certified instruments, for use on  experimental and homebuilt aircraft, or certified products, installed on civil transport an military aircraft.

Mechanical accelerometers, separately listed, use traditional components like proof masses, springs, and damping to measure acceleration based on displacement, offering high accuracy and durability for specific applications like flight stabilization and weapons communication. They are often of larger size and more expensive. Digital accelerometers, included in this listing, are often Micromachined Micro-electromechanical (MEMS) systems, integrating sensors with microelectronic circuits for smaller size, lower cost, and high precision, making them ideal for flight stabilization, AHARS, and autopilot systems.

The choice of an accelerometer depends on the application's need for accuracy, size, cost, and resistance to harsh environments. 

Please consult the Product Description section and the supplied documentation for more information on different brands of our offered accelerometers.

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.

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.

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.

KELLY MANUFACTURING (RC ALLEN) RCA 15AK series are TSO'd 3-1/8" ( 80mm) electric directional gyros suitable for both fixed wing and rotor wing aircraft.

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 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 RCA 22 Series of vacuum artificial horizon are controlled by air driven precision gyros to present the pilot with pitch and roll information. The attractive color scheme of blue sky and brown ground presents a realistic spherical display of flight. Unless otherwise indicated all instruments have a  "standard" display (dark blue/brown display with fixed pointer) and are unlighted.

All R.C. Allen vacuum gyros run off of 4.5" Hg, erect time is 3 min. The instrument fits in a standard 3 1/8 panel cutout. A ¼ -18 NPTF nylon tube slip fitting is recommended for vacuum hose installation. A 1/8 – 27 NPTF nylon tube slip fitting is recommended for vacuum gauge installation. 

Dimensions: H: 3-3/8", W: 3-3/8", L: 6"

Weight: 2.75 lbs.

Certification: Meet or exceed all requirements of FAA TSO C4c and Aeronautical Standard AS396B.

Made in the USA

NOTE: The RC Allen RCA22-7 Vacuum Horizon Gyro can be an alternate device for Cessna Gyro Horizon C661076-0101.

The RCA 56 Series of electric turn and bank indicators by KELLY MFG (RC ALLEN) are an all volt instrument, with a power warning flag, a black or white ball inclinometer and either lighted or non-lighted. These rate-of-turn pointer controlled instruments are powered by an electrically driven DC precision gyro with an inclinometer providing the pilot with turn and bank information.  They meet or exceed requirements of FAA TSO C3b. Made in the USA. Weight: 1.9 lbs.

Dimensions: Length: 6 1/4 in. Max, Width: 3 3/8 in. Max, Height: 3 3/8 in. Max

Mating Connector: MS3106A10SL-3S.

Connector Pin Out: A: +11-30 VDC, B: Ground, C: Spare

 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.

LONE STAR AVIATION manufactures multiple fans and blowers for OEM applications.

The CYCLONE 100 FAA-PMA approved 1 port blower is the smallest (1 x 2 x2 ), most efficient (brushless dc motor), and the most versatile cooling fan for avionics and or other electronics needing thermal cooling. Its universal mounting bracket makes it easy to set-up and install on on many make and model aircraft and or rotor-craft.  Also installed in Land-Mobile, Marine and Military Vehicles for many PED, radio, GPS applications. Offered in Input 12VDC/24VDC versions.

Lone Star Aviation's new FAA-PMA approved Cyclone 1 port blower is the smallest (1 x 2 x2 ), most efficient (brushless dc motor), and the most versatile cooling fan for avionics and or other electronics needing thermal cooling. Its universal mounting bracket makes it easy to set-up and install on on many make and model aircraft and or rotor-craft.  Also installed in Land-Mobile, Marine and Military Vehicles for many PED, radio, GPS applications. 

The CYCLONE 21 FAA-PMA approved 3 port blower is a compact (3 x 3 x 1") aircraft electronics cooling fan that delivers 21 cubic feet per minute of forced air cooling to a variety of avionics equipment. It is the top FAA approved avionics blower for 14/28 volt aircraft with the smallest footprint and the highest output but also the number one choice for OEM and aftermarket sales world-wide for many make and model aircraft and rotor-craft.

For more information on the above products please consult the Product Description section and the supplied documentation.

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

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.

MGL AVIONICS XTreme full featured instrument series include an Electronic Flight Instrument System (XTreme-EFIS) with navigation/autopilot capabilities and anEngine Monitoring System (XTreme-EMS). Their light weight, small size and high level of functionality makes them an excellent choice for use in non-certified aircraft. Both instruments fit a standard 3 1/8” (80mm) instrument panel hole. All information is displayed in an easy to read format on a high resolution wide viewing angle 4.3” sunlight readable color display. The XTreme-EFIS includes all the functions of the XTreme-EMS version. It a compact, multifunction electronic flight information system intended as a main flight instrument in smaller aircraft or as a backup/secondary flight instrument in larger aircraft. It integrates all the necessary functionality to replace several flight and engine monitoring instruments.The XTreme-EMS is a compact universal engine monitor replacing several engine monitoring instruments. All engine sensors are connected to a RDAC (Remote data acquisition unit) normally mounted behind the aircraft firewall. A simple CAN communication link is then necessary to connect the XTreme-EMS to the RDAC.

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 N16 split design remote-mount VHF Navigation Receiver by MGL AVIONICS belongs to a new generation of navigation receivers based on RF direct conversion technology. The N16 is identical in size to the V16 COMM radio and can be used in a simple configuration as combined NAV/COMM solution for both MGL EFIS systems using the MGL protocols or, if at least one MGL VEGA or RAZOR control head is used these heads can provide NAV/COMM data output on RS-232 that is compatible with most EFIS systems on the market. Like V16 COMM, it is a Non-TSO'd NAV receiver for use in experimental and light-sport aircraft. For stand-alone operation, at least one MGL RAZOR control head or two MGL VEGA heads are required. Using these heads a fully compliant solution is presented that provides both VOR CDI using a rotary control for OBS bearing entry as well as the familiar two bar ILS localizer and glideslope indication. The VOR provides a display for bearing to station and radial from station at the same time for up to two simultaneously-received VOR stations. For additional information please refer to the attached documentation.

FLYBOX® brand  by MICROEL SRL relates to a wide range of avionics and flight instruments specialy designed and developed for ultralight and experimental aircraft. FLYBOX® product portfolio includes 

My-EMS & Vigilus Engine Monitoring Systems

Engimaster EMS Engine Monitoring Systems

Oblò,  Oblò 2 and Eclipse NG Electronic Flight Instrument Systems (EFIS)

Omnia 57 and 80 Series of Legacy Instruments/Indicators

FLYBOX® Autopilot Systems

Flap & Propeller Controllers

For further information please refer to the Product Description section & the supplied documentation.

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.

The MID CONTINENT® INSTRUMENT (MCI) 3" TSO'd Turn Coordinators are value priced  and engineered for reliability and a long service life. Depending on the model, they can be a direct replacements for most coordinators with 3-pin or 5-pin connectors. 

These instruments show  a standard 2 minute turn when balance ball reaches either side of display. MCI turn coordinators feature a HEA non-glare glass screen for easy readings, an operating range of temperatures from -30 to +50 deg. C and altitude-1000 to 35000 ft and they can operate on a voltage range from 10-32 VDC for convenience. Power consumption is 0.28 A. They can be front or rear panel mounted in a 3 1/8" hole. Dimensions: 3 1/4"X3 1/4"X5". Max Weight: 1.4 lbs. Available in lighted and unlighted versions. FAA TSO certified to C3b.

The “B” models are equipped with a proven AC rotor powered by a solid-state inverter, creating less heat behind the panel. Utilizing a brushless rotor design, these models exhibit top industry ratings of 4,800 hours MTBF. They are ideal for use in high performance aircraft and cold-climate applications.

MITCHELL AIRCRAFT PRODUCTS, Inc. is a well known manufacturer of tachometers, gauges, and instruments the general aviation industry, built under an FAA-approved quality system.

Their product range includes:

Mechanical 3-1/8″ Clockwise, & Counter-Clockwise, 2, 2-1/4″ Mechanical Recording & Electric Lighted Tachometers, 

Electric Gauges (Ammeters, Cylinder Head Temperature, Exhaust Gas Temperature, Fuel Quantity Gauges, Outside Air Temperature, Pressure & Temperature Gauges, and Voltmeters,

Mechanical Pressure &Temperature Gauges

Modular Gauges (Ammeters, Blank, Fuel Quantity,Pressure, Temperature Gauges, and Voltmeters, Modular Gauge Frames. This line of FAA PMA  miniature square engine gauges is ideal for a wide variety of general aviation applications. They measure nearly 1-1/2″  and are stackable. The modular design allows them to be plugged from the front of the panel. The units are internally lighted. Complete standard panels are also available. If individual gauges are ordered, appropriate backplate with pigtail must be ordered to mount and connect the gauge. If more than one gauge are ordered to be mounted together, a special order clustering requires custom backplates.

Sending Units (CHT & EGT Thermocouples, Fuel Quantity & Pressure Senders, 1/8″ & 5/8″ Temperature Senders.

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.

MITCHELL FAA PMA'd D1-211 Series  modular electric 12V (PN D1-211-5074) & 24V (P/N PE-111-4074) fuel quantity gauges are lighted and easily installed in a 2-1/4" panel hole. They feature a 2 year factory warranty.

The gauges and senders must be ordered separately.

For the 12V Fuel Quantity Gauge D1-211-5074 the matching sender is PS-211-8038, 10-180 Ohm. For 24V operation, P/N PE-111-4074  resistors for each instrument must be ordered.

MITCHELL Pressure Senders 80 PSI (PN PS-211-9002) and 150 PSI (PN PS-211-9040) are offered for use with D1-211-6089 and D1-211-6092 FAA PMA Pressure Gauges respectively. Both have 2 terminals (one terminal to be grounded).

MITCHELL EGT Gauge 0-1600 Deg. F, PN D1-211-6101 requires PN PS-211-8162 sender (probe).

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.

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.

OMRON A3C series cylindrical pushbutton switches have the basic design as the M2C Series cylindrical indicators. They provide a high-intensity uniform surface lighting while they have a miniature size with excellent feeling of operation. They have a cylindrical 20-mmX12-dia. body making panel cutouts easier. 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.

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

The KANNAD 406 AF automatic fixed Emergency Locator Transmitter (ELT)  is designed to be installed near the tail of the aircraft and to be connected to an outside antenna (sold separately). A sophisticated “shock sensor” will activate the ELT automatically in the event of a crash. Its small size and light weight make it ideal for general aviation aircraft.  The Mounting Bracket (Strap) is not included. 

A separate version (406 AF-H) has been specifically developed for installation on board a helicopter in flat position (to gain space compared with usual installations at 45° downwards). 

Product Features:

Optional Navigation Interface transmits GPS coordinates significantly shortening Search and Rescue response time.

Operates without aircraft power and incorporates an internal alarm/buzzer avoiding costly installation procedures.

Six year lithium manganese battery.

Three frequency transmitter (121.5 / 243 / 406 MHz)

Weight: (Including batteries) 2.44 lbs (1110 g) / max 2.60 lbs (1180g)

Please refer to the supplied documentation for additional information.

Note: The Kannad 406 AF-COMPACT version, designed for private pilots and light aircraft (usually supplied as kit with rod or whip antennas), has been discontinued and is no longer available.

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

LORD Corporation AM Series Low Profile Avionics Mounts (also referred to as isolators)) set the standard for compact, highload, high-capacity isolators. They are designed to support and protect avionics equipment in all types of aircraft. Inertial guidance and navigation systems and radar components are examples of applications where these mounts are used. In addition, AM Series mounts are used to isolate engine/aircraft accessories such as fuel controls, pressure sensors and oil coolers. These mounts  are tested and approved to the environmental tests appearing in MIL-STD-810 or MIL-E-5400. They may be used in a temperature range of -65°F to +300°F (-54°C to +149°C) for BTR® Silicone and -40°F to +300°F (-40°C to +149°C) for BTR® II Silicone. They are made with specially compounded silicone elastomers which exhibit excellent resonant control evidenced by the low transmissibility at resonance. These designs also provide linear deflection characteristics.

LORD Corporation AM Series vibration isolators are offered in different sizes and capacities. Please refer to the attached documentation.

The PS ENGINEERING PMA7000 series of TSO'd audio panels offer a very affordable upgrade for existing BENDIX KING KMA24 units while providing a a great set of capabilities. The PMA7000B with built in Marker Beacon is KMA24 pin compatible. Existing wiring to the KMA24 can be maintained making the cost of the upgrading less expensive. In addition, it is plug and play with the original PMA7000M-S, the PMA6000M-S, and the KMA28 audio panels. PMA7000 series audio panels feature  6-place IntelliVox® automatic Voice Operated Relay (VOX) hi-fi stereo intercom system with Soft Mute™. The PMA7000B provide 3-com capability with the option to easily convert Com 3 to a full duplex cellular telephone interface  and "Split Mode" allowing the pilot to be on Com 1 while the copilot is on Com 2.

Product Features (depending on model selected):

IntelliVox® automatic VOX system with individually gated microphones

6 - Place hi-fi stereo intercom with Soft Mute™

Bluetooth(R) Interface (Model PMA7000BT) allowing music streaming as well as interconnect to an iPhone, iPad, iPod, or any other Bluetooth(R) enabled device that has the Handsfree or A2DP profile.

2 - music mute modes: Mute On and Mute Off

Built-in Marker Beacon Receiver

Cellular telephone input with dedicated On/Off hook switches for unprecedented flexibility

Split mode for dual audio panel capability

2 Hi-fidelity stereo music source inputs

3 - Isolation modes - Pilot Isolate, All, and Crew

4 - Unswitched inputs

Selectable music muting for passengers

Selectable special intercom mode with ""Alternate Intercom Mode""

RAM (Radio Active Mute) eliminates constant back ground noise from radio static

The only knob that is on the panel is a concentric volume control for the Crew and Passengers intercom volume. The all push button controls of the PMA7000B allows for easy selection of Coms and other Nav aids.

Certification: FAA Export 8130-3

Warranty: 24 months

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

The analog and digital portable two-way radios (walkie talkies), manufactured by QUANZHOU YANTON ELECTRONICS CO., LTD., come in different models covering UHF or VHF and UHF frequency bands and different power outputs for communication over different distances. They have an ergonomic design and cover the needs of various operations. YANTON radios are approved by the Ministry of Information Industry in China and the European CE, RoHS and USA FCC certified/approved for use in other countries.

Used on most major civil and military programs, RADIALL™ DSX Series ARINC 404/SAE-AS81659 Connectors offer a proven solution to electrically connect equipment rack to avionics equipment. The DSX series are multipin, rack and panel style connectors designed to electrically connect equipment racks to avionics equipment. Typically the plug is installed on the avionics rack and the receptacle on the equipment box. Applications include commercial and military aircraft and helicopters, railway, radar systems, power circuits, in-flight electronic instrumentation and flight simulators.

Different DSX Series versions are outlined below:

DSX SAE AS81659, available in four shell sizes (1, 2, 3 & 4) with environmental and non-environmental versions as well as EMI/RFI options to improve shielding effectiveness. DSX SAE AS81659 connectors cover both civil and military applications.

DSX ARINC 404 shell type A and B are the original connectors, mainly dedicated today to commercial applications.

DSX-F and DSX-K receptacles, RADIALL™ solution for front release front removable (FR/FR) contacts to facilitate installation and maintenance. Fully intermateable with ARINC 404 type B and SAE AS81659 plugs, they offer the same characteristics as SAE AS81659 connectors.

Shell types are plugs and receptacles made from an aluminum alloy with cadmium yellow chromate or nickel plating options. Mismating is prevented by a polarizing system which provides 216 polarizing positions. For military part numbers, applicable polarizing position range goes from 00 through 99 only. Inserts are offered in various contact arrangements accommodating rear release, rear removable signal (size 22) power (sizes 5, 12, 16 & 20HD), coaxial (sizes 1, 3, 5, 7, 9 & 15), concentric twinax (sizes 5 & 9) triax (sizes 5 & 9) contacts in crimp, wire wrap or PC tail termination. Radiall’s 29504 fiber optic termini are also available. With numerous configurations and a wide variety of contacts and accessories, the  RADIALL™ DSX Series offers for both OEMs and aircraft manufacturers robust and high performance solutions fully compliant to SAE AS81659 specifications listed on the qualified product list (QPL)as well as ARINC 404 commercial connectors.

For additional information please refer to the supplied documentation.

Note: Special Order items. Non-Cancellable/Non-Returnable Upon Order Placement (NCNR). Minimum Order Quantities & long lead times usually apply. Contact us.

Splits the signal from a single NAV antenna into two NAV receivers and one glide slope receiver.

The AV-534 is a TSO'd heavy-duty stainless steel bent whip VHF communications antenna with porcelain insulators and mounting hardware. The AV-534L is same antenna as AV-534 but furnished with 96" lead of RG58 A/U cable with male BNC and ground strap with lugs.

The AV-525 is a VOR/LOC/GS antenna similar in style to the AV-12 but utilizes an internal balun transformer. The antenna is rated at speeds up to 350 mph and altitudes up to 50,000 feet. It is a direct replacement for the CI 157P.

Product Specifications:

Model: AV-525

Application: VOR/LOC/GS Receive Only

Frequency: 108-118 MHz (VOR/LOC) -328-336 MHz (GS)

Impedance: 50 Ohms Nominal

VSWR: 3.0:1 Maximum 108-118 MHz - 2.0:1 Maximum 329-335 MHz

Polarization: Horizontal

Pattern: Omni-Directional

Connector: “BNC” Female

Max. Weight: 0.50 lbs.

Certification: FAA TSO C34e, C36e, C40c

The AV-532 is a VOR/LOC/GS receive only antenna which consists of taper ground high-strength 17-7PH stainless steel elements to reliably withstand vibration and wind loads. The insulators are weather-sealed compression-molded bakelite with the mounting holes provided. The unit may be mounted with the V pointed either forward or aft. The antenna is designed to operate at speeds up to 350 mph and altitudes up to 50,000 ft. It has a drag force of 3.42 lb @ 250 mph.

R.A. MILLER INDUSTRIES (RAMI) aircraft antennas cover a wide range of functions including communications, NAV antennas, GPS, ADS-B, transponder, VOR localizer, glide slope antennas, and marker beacons. They are known for their streamlined aesthetics, quality, and reliable performance. Offered in different TSO models, RAMI wire whip and rod antennas ELT (Emergency Locator Transmitter) devices are intended for use on low-speed General Aviation aircraft. 

RAMI AV-100 FAA TSO C126a Airborne ELT Antenna is a passive two frequency (121.5 & 406 MHz) whip antenna, designed for speeds up to 250 knots. Impedance 50 Ohms Nominal, VSWR (Maximum):121.5 MHz 2.0:1 / 406 MHz 1.5:1, Polarization Vertical, Pattern Omni-Directional, Connector BNC Female, Weight: 3 oz. Maximum, Color: Black.

RAMI AV-200 FAA TSO C126a Airborne ELT Antenna is a passive two frequency (121.5 & 406 MHz) whip antenna, designed for speeds up to 250 knots. It meets DO-160G, Section 8, Category U requirements for robust vibration and is qualified for installation on helicopters with unknown related rotor frequencies. Impedance 50 Ohms Nominal, VSWR (Maximum):121.5 MHz 2.0:1 / 406 MHz 1.5:1, Polarization Vertical, Pattern Omni-Directional, RF Power Capacity 10 Watts CW, Connector BNC Female, Weight: 0.19 lbs. Maximum, Max Height 24″.

RAMI AV-300 FAA TSO Airborne ELT Antenna is a passive three frequency (121.5, 243 & 406 MHz) fiberglass rod antenna, designed for speeds up to 350 knots. Impedance 50 Ohms Nominal, VSWR: 2.0:1 max at 121.5 MHz,2.0:1 max at 243 MHz, 1.5:1 max. at 406 MHz,  Polarization Vertical, Pattern Omni-Directional, RF Power Capacity 10 Watts CW, Connector BNC Female, Max Weight 9 oz, Max Height 14″.

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

The RAMI AV-10 COMM Antenna is designed for high-performance aircraft applications. It exhibits excellent electrical characteristics and incorporates an efficient aerodynamic 4-bolt mounting base. The antenna essentially matches the styling of the communication antennas currently used on most singles and light twins. The antenna is designed to operate at speeds up to 350 mph and altitudes up to 50,000 ft. It has a drag force of 2.70 lb @ 250 mph.

Product Specifications:

Application: Airborne Communications

Frequency: 118 to 137 MHz

Impedance: 50 Ohms Nominal

VSWR: 2.0 to 1 Maximum

Polarization: Vertical

Pattern: Omni-Directional

Connector: Type "BNC" Female

Max Weight: 8 oz

Max Height: 20-1/4"

RF Power Capacity: 25 Watts

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.

SAFE FLIGHT (SF) is the world's leading manufacturer of aircraft lift instrumentation and control systems. SAFE FLIGHT FAA certified Lift Detectors & Angle of Attack (AoA) Sensors are installed on hundreds of aircraft worlwide.

SF’s Lift Detector is the foundation of SAFE FLIGHT’s Stall Warning systems. This was the first and still the industry standard for stall warning in light aircraft. It  consists of a small tab or vane which senses the change of the stagnation point on the wing and an alerting device used for stall warning. The  detector warns by light and horn of any danger of an approaching stall regardless of the flight maneuver. It comes in different variations complete with installation kit & instructions. 

SF’s SCc Angle of Attack (AoA) system meets FAA requirements by providing both flashing red LEDs and an unmistakable audio output to alert the pilot of increasing AoA and an impending stall. It consists of two key components, the Lift Transducer and the the Indexer Computer. Available for retro-fit. Including the Lift Transducer, the Indexer Computer, and all necessary wiring, connectors and installation hardware.

For additional information please refer to the Product Description section and the supplied documentation.

Sigma-Tek Light tray to connect lighting to Sigma-Tek 5000B Attitude Gyro and other avionics and instruments. Available in 14V or 28V versions.

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).

The SIRS "Navigator" magnetic compass delivers extremely accurate readings due to its fully integrated, 4 magnet correction facility.  It has the same features as the "Pegasus", but is mounted with a fully adjustable bracket that allows attachment to a variety of positions including the glare-shield or the windshield. This allows the compass to be located away from magnetic influences. Available in different versions for Northern or Southern hemisphere, unlighted  or lighted 12/28V and has a 3-year warranty. Size: 203/8" H x 2-1/4" W. Product accessories such as installation kit, GS1 glareshield mount, SIRS MF1 short foot bracket and SIRS compass correction key are also available and sold separately.