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.

Fuel pressure gauges are used in BRP-ROTAX® aircraft engines and offered as certified or non certified parts from their respective manufacturers. Non certified parts can be used in ultralights or other aircraft not requiring certification of parts for their installation.

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.

Fuel pressure gauges are no longer offered as ROTAX Part Numbers. These part numbers are provided for reference only. For these gauges please refer to our product presentation on AVIASPORT Fuel Pressure Gauges or contact us.

These precision quartz electric aircraft clocks are constructed for easy installation in a wide variety of replacement applications for home builts. The rugged quartz movement is accurate within 2 sec. in 24 hrs under normal operations and runs accurately in temperatures from -30º to 180ºF. Available in 14 Volt or 24 Volt versions.

Product Specifications:

OD: 2-1/4"

Depth: 2"

Weight: 4 ounces

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

WULTRAD INC. is a manufacturer of non-certified flight and engine instruments under FALCON GAUGE brand for experimental and homebuilt aircraft. Although their products are Non-TSO, they are made to TSO or MIL specifications for quality.

FALCON GAUGE Electrical Attitude Gyro is intended for use in experimental aircraft only. It provides a continuous visual display of the aircraft attitude with respect to the earth for maneuvering around the longitudinal (pitch), and lateral (roll) axes, and yaw. A precision AC brushless motor is featured in the electrical attitude gyro. The Power failure drops into view whenever the power is insufficient for operation of the gyro. Electrical gyro can be caged by pulling the "Pull to Cage" knob. It is offεred with or without internal lighting and is designed to work with a 12V system. Dimension: 3-3/8"X 6.46/164mm.

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.

HONEYWELL BENDIX KING® KI-229 Radio Magnetic Indicator (RMI) provides bearing information to either ADF or VOR stations by means of two pointers each of which is read against compass card.

The KI-229 RMI combines three data points on one indicator. The current aircraft heading from an HSI is shown on the card. The magnetic headings to VOR and NDB stations are shown by the twin needles. By combining all this information visually, less interpretation is required thus enhancing overall situational awareness, something especially helpful when the workload is high.

The KI-229 requires inputs from ADF, HSI and NAV receivers.

Product Features:

14/28 volt lighting

Compatible with Nav Receivers such as KN-53, KNR-615, KNR-630/631/632/633, KNR-634, KNR-665, and KNR-665A

Compatible with Nav systems including RNAV such as KNS-80 and KNS-81

Compatible with ADF receivers such as KR-87 and KDF-806

Compatible with Compass systems such as KCS-305 and KCS-55/55A

Requires input ARINC Compass System

TSO'd

Product Specifications:

TSO Compliance: Env. Cat. RTCA DO-160A A1C1/A/SKP/XXXXXXA/B/AAA

Weight: 2.8 lbs. (1.3 kg)

Temperature: -20 to +55°C

Altitude: 35,000 feet

TSO (Compass): TSO C6c

TSO (ADF): TSO C41c Class A

TSO (VOR): TSO C40a

Heading Input: Operates from any slaved magnetic compass with ARINC X,Y,Z outputs

VOR Video Input: 0.5VRMS 0 deg. phase composite 30Hz variable AM and 30Hz reference FM on a 9960Hz carrier (0.7VRMS maximum)

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.

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.

HONEYWELL BENDIX KING® manufactures a range of TSO'd VOR/LOC/Glidescope indicators. These navigation instruments include VOR/LOC left-right needles, To-From indicator, VOR/LOC warning flag, glideslope deviation needle, glideslope warning flag and 30Hz OBS resolver. Depending on the model, the feature rectilinear instead of pendulum type meter movements for more precise indicator readings, 14/28 volt internal lighting, metal bezel with glass lens and course datum synchro for autopilot use.

These indicators are commonly used with BENDIX KING® remote mounted VOR/LOC converters such as KN-72 or KN-77, remote mounted Glideslope Receivers such as KN-73 or KN-75, KNS-80, KNS-81 nav systems and KX-155/KX-165 NAV/COMM transceivers.

The KI203 model features an internal VOR/ LOC converter and it is compatible with the BENDIX KING® KX155 transceiver. It has a rectilinear meter movement. Compatible with the BENDIX KING KX155 NAV/COMM transceiver.

The KI 204 VOR/LOC/Glideslope Indicator features a built-in VOR/LOC converter and scallop rejection filter, rectilinear needle movement and an optically coated glass lens. Requires input from external glideslope receiver. Compatible with the BENDIX KING® KX 155 or KX 155A NAV/COMMs. Requires input from external glideslope receiver.

The KI 206 VOR/LOC/Glideslope Indicator is rectilinear and internally lighted. It is used with the KNS 80/81 units, KX 165  transceiver and the KNR 634 VOR/LOC/GS/MB receiver. It is available with course datum synchro.

The KI208 model features a built-in VOR/ LOC converter and it is compatible with the BENDIX KING® KX 155 or KX 155A NAV/COMMs. It has a  pivoted needle action and a plastic lens.

The KI209 model features an internal VOR/ LOC converter and it is compatible with the BENDIX KING® KX155 transceiver. It features a pivot needle action.  The KI209 model includes GPS interface capability.

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.

UMA Electronic Hydraulic Pressure Gauges are offered in TSO'd and Non TSO'd models and 1-1/4"  or 2-1/4" diameters to fit respective aircraft panel openings. They are housed in aluminium or Valox 420 plastic cases (depending on the model) and connect to  precision, high pressure transducers which mount directly to the aircraft's hydraulic system. Standard markings are black and white. Recommended for new design projects and applications. 

Note: Pressure Transducers (Senders) ARE NOT INCLUDED in the prices of the pressure gauges. They are sold separately and are not TSO'd.

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

WULTRAD INC. is a manufacturer of non-certified flight and engine instruments under FALCON GAUGE brand for experimental and homebuilt aircraft. Although their products are Non-TSO, they are made to TSO or MIL specifications for quality. 

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

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

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.

UMA NON TSO'd Electronic Amp Meter Gauges (Ammeters) are available in different series for different measurement ranges and installation in different panel hole diameters. 1-1/4" series allow utilization of panel space without compromising readability. They can be powered from 14 or 28 volts. Signals are acquired from remote mounted sensors, processed and displayed on analog dials with easy to read markings. Each gauge uses rugged aircore meter movement for vibration resistance and repeatability. Each gauge can be placed in a 1-1/4” diameter hole and mounted behind the panel with (4) 6-32 screws. They can be cluster mounted as close as 11/2” centers. Also available as new manufacture electric with 2-1/4" dia. Other UMA series of electronic ammeters include 2-1/4" series with moving coil and 85° Sweep and 2-1/4" Dual Amp/ 0-30 volt meters with moving coil  and 85° sweep.

NOTES:

These ammeters come with the suitable shunt. Different shunts are used depending on ammeter part number.

All Part Numbers beginning with the letter "T" are TSO'd for Certified Aircraft.

Amphenol MS MIL-C-5015 Circular Plug Connectors are designed to meet the demanding performance requirements of military standards. These cable mount circular plug connectors have proven electrical capability for equipment applications where durability is important. The Amphenol plugs have threaded couplings and single key/keyway shell polarization for an accurate and reliable connection. The solid shells of these MS Series circular MIL-C-5015 connectors are made from high grade aluminium alloy. The shells are electrically zinc plated with an olive drab chromate finish which ensures a high resistance to corrosion. The inserts of these military circular connectors are made from resilient synthetic rubber which offers a high dielectric strength and resistance to vibration.

The MS3106A-10SL-3S plug can be used with Turn Coordinator TC02E-3-2 or Turn & Bank Indicator TB02E-2-1.

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.

Series 200 Turbine Flow Transducers by FLOSCAN INSTRUMENT CO. INC. measure flows of hydrocarbon fuels such as gasoline, kerosene, and #2 diesel fuel and other light transmitting, non-corrosive liquids of similar viscosity.  Typical fuel flow applications include aircraft fuel monitoring systems; gasoline, diesel, and gas turbine engine test stands; and industrial furnaces. The transducers give repeatable signals on gasoline across a 100 to 1 flow range down to 0.3 GPH.  The higher viscosity of diesel fuel reduces signal repeatability at flow rates below 2 GPH.  Pressure drops are very low compared to other turbine flow transducers.  The transducer bearing system is rated for continuous operation at the upper end of the flow range. The transducers produce a current pulse signal from an opto-electronic pickup with a preamplifier. 

Because of their superior accuracy and extraordinary repeatability, FLOSCAN transducers have quickly become the dominate fuel flow measuring sensors for general aviation but are also used in marine and other applications.

FLOSCAN aviation products are NOT TSO, PMA or STC'd.

Please refer to the specification table for additional information.

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.