CMM Series male-to-male in-line check valve with compact overall length. CMM check valves are available in brass, steel and stainless steel and in different sizes.

The RBC® BEARINGS offers a full line of airframe control ball bearings to the aerospace industry  in both “Standard” and “Precision” series. The prefix “M” in a bearing number indicates that it is of a precision series. Although designed and manufactured under demanding quality control requirements for airborne systems, these bearings have been successfully used in many industrial applications, where oscillatory movement, high loads, or corrosive environments are prevalent.

RBC® BEARINGS airframe control ball bearings conform to SAE-AS7949 (formerly MIL-B-7949) and many major OEM specifications. These bearings are of lightweight design, corrosion-resistant, grease-lubricated, and typically sealed. Airframe control bearing rings and balls are made of hardened bearing alloy, AISI 52100, with all exposed surfaces, except bearing bore, caps and seals, plated for corrosion protection. For improved corrosion protection, RBC® BEARINGS  supplies bearings made of hardened stainless steel alloy, AISI 440C. This alloy may be passivated or plated with cadmium or zinc nickel for enhanced corrosion protection.

The RBC® BEARINGS Airframe Control Ball Bearings are offered in different series. The KP/KP-A and KSP/KSP-A series, presented separately, are briefly discussed below.

KP (Heavy Duty) and KP-A (Medium Duty) SAE-AS7949 Series radial ball bearings  manufactured with Plyoseals. KP heavy duty single row sealed bearings comply with MS27640 specifications while KP-A medium duty single row ball deep groove sealed bearings with MS27641 specifications. Both KP and KP-A radial ball bearings are prelubricated for life and feature PTFE seals and CRES sealcaps, cadmium plated exposed surfaces except bore, caps, and seals. Both are also offered with CRES 440C material and/or zinc nickel plating per OEM specifications. Load limit ratings: Radial 1230-lbs, thrust 300-lbs.

KSP/KSP-A Series SAE-AS7949 Series single/double row, self-aligning, light and heavy duty ball bearings with bonded PTFE seals and cadmium plated exposed surfaces except bore, caps, and seals. Like those of KP/KP-A Series, both KSP and KSP-A bearings are prelubricated for life and are also offered with CRES 440C material and/or zinc nickel plating per OEM specifications.

For additional information please refer to the supplied documentation in the respective product presentations.

The CONFOR™ foam family (formerly Temperfoam™) by Aearo Technologies LLC (E-A-R), are open cell elastomeric, ergonomic, urethane foams forming part of their specialty foams for comfortable seating, crash protection and noise and vibration control.

CONFOR™ foams offer enduring seating comfort, and absorb a much higher amount of impact shock compared to common polyfoam. They can be used for long period seating applications in aviation, automotive, recreational, office, in medical hospital bedding, sports equipment, wheelchair cushions, industrial operations, or as protective packaging for high value devices.

Standard CONFOR™ product line has been replaced by CONFOR™ M & AC RoHS compliant foams with the same slow recovery attributes as the replaced ones. They come in different sheet sizes (the most popular 16" x 18", 18" x 20", 18" x 24"),and densities, corresponding to different foam weights per cubic foot and denoted by a respective color code (Yellow/Very Soft (CF40 M/AC), Pink/Soft (CF42 M/AC), Blue Medium ((CF45 M/AC), and Green Firm (CF47 M/AC).

CONFOR™ M slow-recovery foams, offer a unique combination of physical characteristics, high energy absorption properties and temperature-softening behavior. They provide impact protection and isolation for dynamic loads, while maintaining consistent static load performance. Their unique combination of slow recovery and high energy absorption allows these materials to offer effective damping and vibration isolation. In addition, as open-celled foams, they are breathable, non-irritating in dermal contact, and thus suitable for highly diverse applications, for medical and body contact cushioning applications to electronics packaging. The respective CONFOR™ AC foams have been engineered for the aircraft market. They are flame resistant and comply with FAR 25.853(a) Appendix F Part I (a)(1)(ii)(12 sec) burn specification requirements, consisting an excellent choice for use on aircraft. CONFOR™ CF42AC & CF45AC foams  are softer and provide more comfort. CONFOR™ green firm density foam CF47AC provides the best energy absorption protection. 

CONFOR™ AC foams are offered in different thicknesses, as solid pieces (e.g. in 1" thickness) or various pre-built  laminates resulting in higher thicknesses. DYNAFOAM is also often used as comfort foam on top of CF-47AC foams. Indicative offered laminations include:

- 1" thickness CF47AC sheet and 0.5" thickness DYNAFOAM sheet. Total laminate size - 16" x 18" x 1.5". Ideal balance for most pilots. 

- 1" thickness CF45AC and 1" thickness CF47AC sheet. Total laminate size - 16" x 18" x  2". Ideal for maximizing safety providing comfort at the same time.

- 0.5" thickness CF47AC and 0.5" thickness DYNAFOAM sheet. Total laminate size - 16" x 18" x 1". Ideal for tall pilots with minimal head clearance.

Third party accessories, such as protective covers, are also available to maximize CONFOR™ foam life.

For additional information please consult the supplied documentation.

BRIDGESTONE® CORPORATION is the world's largest manufacturer of tires and other rubber products, delivering a wide range of innovative, premium product portfolio whch includes passanger and light truck tires, motorcycle tires, commercial truck and bus tires, aircraft and mining tires. The company also manufactures industrial rubber and chemical products, sporting goods, and other diversified products. Tires account for 80 percent of Bridgestone Group sales worldwide with sales of tires and other products in more than 150 nations.

BRIDGESTONE® has more than 80 years of experience and insistence on quality in aircraft tire manufacturing. The company supplies new and retread (*) tires to airlines and wheelshops worlwide remaining one of the most trusted brands in the aviation industry.

BRIDGESTONE® range of aircraft tires includes Bias, Radial and Revolutionarily Reinforced Radial Tires (RRR). They work under extremely severe conditions, carrying the weight of an aircraft up to 569 metric tons while accelerating up to 245 mph at takeoff, in addition to enduring varied environmental stress when in flight and taxiing.

The company manufactures its new aircraft tires in Japan while it operates aircraft tire retreading plants in Japan, the United States, Belgium and Hong Kong. Bridgestone provides airlines with seamless, global support for all of their product and maintenance needs in tires. 

BRIDGESTONE® Bias tires feature enhanced tire durability, greater overload durability, reduced weight, new cord and performance improvements due to the integration of Tension Control Optimization (TCOT) and Aircraft Tire Tension Control Optimization (ACOT) Theory principles.

BRIDGESTONE® Radial tires feature lighter design, reduced rolling resistance, rigged belt design, added strength to belt and carcass plies and increased number of landings.

BRIDGESTONE® Revolutionarily Reinforced Radial Tires (RRR) feature superior safety, higher cut resistance, more casing durability after received Foreign Object Damage (F.O.D.), economy, less weight and more landing cycles (improved tire wear). They have been selected by Airbus and Boeing as OE tires for their respective aircraft.

Please refer to the supplied documentation and the Aircraft Tire Application Table for additional information.

(*) Retread tires have undergone a remanufacturing process to replace the worn tread on used tires with new tread to help extend the life of the tire. The number of times the  tread has been replaced in the tire casing is indicated by a number just after the letter "R" in the product reference number (SKU), namely R1, R2, R3 and so on.

FAA-PMA Approved original equipment TCM Bendix magneto ignition switches  with 3 positions (Right/Left/Both Mags). They come complete with two keys and faceplate. For dual ignition aircraft systems, ignition switch grounds both magneto P-leads in off position.

The SPRL fuel locking and non-locking caps have secure sealing and easy finger tip operation. These caps are made from the highest quality modern engineering plastics with Viton o ring seals (which can be easily replaced). The mounting rings are anodized aluminum with the flange recessed to give a perfect flush fit whether it is riveted under a metal skin, as in the RV series, or built into a composite structure. The SPRL caps are non vented and recommended to keep the fuel in, the water out and in the locking version, other unwanted items out of your tank. 

SPRL-L (locking) and SPRL-S (non-locking) fuel  caps have an 65 mm O.D. and can be used on Europa, Compair, Glasair, Lancair, Murphy, OMF, Rocket, Velocity, Zenith and many more experimental aircraft. Wt: 80 grams.

AERO INSTRUMENTS® Company, now part of AEROCONTROLEX® Group, Inc., has been a supplier of Air Data Sensors for aircraft applications for over 85 years. AEROCONTROLEX® current manufacturing  of Air Data Sensors has been transitioned to AEROSONIC® Corporation which manufactures aviation instrumentation and avionics equipment including air data systems, standby displays, digital and mechanical standby instruments, sensors and probes.

Air data include total pressure of the airflow measured by pitot tubes, static pressure of the ambient air by static ports (or both pressures by pitot-static tubes), total temperature (higher than the actual air temperature due to friction and adiabatic compression) by TAT sensors, and angle of attack (i.e. angle between the airfoil and the airflow) by AoA sensors. All these data are vital for aircraft flight and in the case of large civil or military aircraft, once collected are fed to  an air data computer (ADC).

AEROSONIC® / AEROCONTROLEX® extensive portfolio of pitot probes, including pitot, pitot static and pitot/angle-of-attack probes, are designed and today in use  on a wide range of aircraft ranging from military and large commercial transports to helicopters and UAVs. Their product range  includes electrically heated pitot probes, pitot-static probes, static pressure ports, angle of attack, temperature sensors and flight test equipment for the aerospace and defense industries. They are designed to meet or exceed all applicable standards, including SAE AS393, DOD MIL-T-5421B, TSOC-16, AN5813 and BS2G.135 and feature heating elements to prevent ice accretion and water ingression for reliable operation in the most adverse environmental conditions. Probes may be configured as stand alone with pneumatic outputs to the Air Data Computer, or they may integrate the computing function and eliminate the pneumatic connection.

AEROSONIC® fuselage mounted static pressure ports are engineered to meet or exceed industry specifications to supply ambient static pressure measurements to air data computers, altimeters, airspeed indicators and vertical speed indicators in numerous types of aerospace applications. The Static Pressure Ports’ electrical heating elements prevent ice accretion and water ingestion ensuring the performance of primary flight instruments is not degraded even under the most severe atmospheric conditions.

For additional information please refer to the Product Description section.

The ORION A600 PG/PR code 4 lighting system by WHELEN AEROSPACE TECHNOLOGIES (WAT) combines a wing tip anti-collision white strobe with forward and tail position conventional navigation lights in one unit which can be used as a replacement for conventional teardrop type navigation lights. Tail position light eliminates the need for a tail mounted position light. 

WHELEN A600 PG/PR incorporates red or green nav light on the forward section, a strobe light with magnifying glass lens in the center and a clear tail position light on the aft portion. Newly developed magnifying strobe lens (A 612) concentrates the maximum xenon light energy in the horizontal plane increasing the light intensity by two to five times. The tail position light on the wingtip gives turning reference to the aircraft behind by displaying angle and white bank while turning. It also eliminates the need for a tail mounted position light which may be omitted when using A600 lighting system. FAA-PMA Approved. Available in 14 or 28 VDC and in a radio-shielded versions. 

Available in 14 or 28 VDC and in a radio-shielded version. The forward position lamp is 26 watts and the taillight lamp is 25 watts.

Product Specifications:

Weight: 0.8 lbs. (363gm)

Position Lamps Power Consumption: 4 amps @ 14 VDC; 2 amps @ 28 VDC 

Exposed Height: 2.4” (61mm) 

Length: 5.63” (143mm) 

Width: 1.7” (43mm) 

This product series is no longer available.  Please refer to model 90340 which is a direct replacement (exact footprint) for the model A600PG/PR without replacing the current strobe power supply. 

For a number of years CLEVELAND WHEELS & BRAKES offered standard organic & heavy-duty asbestos brake linings for their wheels and brakes. In January 1988 these two types of brake linings were discontinued and a single, improved brake lining was introduced with improved performance and durability compared to older linings. Different versions are available to fit aircraft models based on their year of construction. Brake linings are sold as pad only or as kits together the required number of rivets. Most light aircraft take 2 linings per wheel. Extra rivets are also available. Please refer to the attached Application Guide for additional information.

This kit consists of two GE #4509 12V, 100 watt sealed beam lamps rated to draw 7.69 amps, brackets for installation, switch, switch plate, 60 ft. of 2-conductor hookup wire and instructions. Black and white wrapped 18 gauge wire can be used for installation. It is suitable for experimental / homebuilt aircraft only. No FAA approval.

Size: 4-1/2"H x 5-1/4"W x 2-1/4"D with bulbs installed. 

LED lighting is the ideal technology for aviation applications. Whelen LED lights are time and field-tested for reliability and long-life performance under the tough conditions required by Fire, Emergency, DOT and Law Enforcement professionals around the world.

PARMETHEUS PLUS PAR36 LED lights by WHELEN AEROSPACE TECHNOLOGIES (WAT) are FAA-PMA Approved LED lights with a convenient “Drop In” design for ease of installation, intended for use as direct replacements for outdated PAR36 Halogen and HID lamps. Power wiring attaches to brass screw terminals. Weight is virtually identical to previous PAR36 lamps. Assembly design includes clocking notch. They are lightweight, low-current and moisture resistant and provide stable light output for thousands of operating hours. The WAT PARMETHEUS PLUS  LED lights have a 40% brighter output than the original PARMETHEUS Series assemblies.

Product Features:

Offered in Landing and Taxi versions

Lightweight

STC-PMA

Direct replacement for outdated PAR36 Halogen and HID lamps

First commercially available PAR36 LED for Aviation applications

10.000 hour operating life

Polycarbonate, replaceable, hard-coated outer lens

Metal, heat dissipating coated housing

Whelen TIR™ (Total Internal Reflector) technology rivals strobe in intensity and effectiveness

Designed and manufactured in the USA.

Five year warranty

GROVE manufactures axles and hardware for use in GROVE wheels as well as those of other manufacturers.

GROVE 500x5 wheel axles (P/N. 5013 standard and P/N. 5018 with wheel pant stub) are produced from solid 2024-T3 aluminum with anodized finish. They have a 1-15/16" Bolt Circle hole pattern and 1/4" diameter holes.

500x5 1-1/4" diameter standard axle (P/N. 5013) is the most popular axle for 500x5 wheels. It is designed to fit Grove 50-1, 51-1, 56-1, 57-1, 57-5 and Cleveland 500x5 wheels. Axle Weight: 0.92 lbs. Static Load Rating 1,250 lbs.

500x5 1-1/4" diameter axle (P/N. 5018) has built-in wheel pant stub with 1/4-28 thread. It is designed for use with Grove 50-1, 51-1, 56-1, 57-1, 57-5 and Cleveland 500x5 wheels. Axle Weight: 0.95 lbs. Static Load Rating 1,250 lbs.

Both axles require two spacers per axle (P/N. 5710) sold separately.  I.D: 1-1/4", O.D. 1-3/4", Thickness: 1/4". They can be used with 500x5 axles.

Standard axle nuts and axle bolt kits sold separately are also offered as part of GROVE product portfolio. Castle type nuts are manufactured to MIL Specification MS21025 using 4140 steel. Mild steel nuts are not acceptable for use on certificated aircraft. 1-1/4" dia. nuts for 500 x 5 axles, 1-1/2" dia. nuts for 600 x 6 axles.

Filler opening caps are parts basically circular in shape, designed to cover or seal the filler-neck or inlet opening of a fuel tank, radiator, oil reservoir, liquid storage tank or the like. They are either permanently attached or provided with a means of removal and replacement. 

Pressure refuel caps are used to lock, seal, and vent the pressure refuel port for an aircraft fuel tank. Pressure refueling allows for single point refueling on larger aircraft and can be used with all aircraft fuels. To fuel the aircraft, the caps are manually actuated by pressing down on the handle, which will vent and unlock the cap for removal by twisting. The cap remains attached to the aircraft by a lanyard. Once refueling is complete, the cap is inserted back onto the adapter and twisted until locked into place, which effectively reseals the pressure refuel port.

Pressure refuel caps are offered by different manufacturers such as Parker Aerospace, Eaton Coporation and others. They are designed in accordance with military specification MIL-C-8605B (for technical requirements) and MS29526-2(for envelope requirements).

Those from Parker Aerospace are 4.5 inches diameter, with an indexing feature and they fit into a 2.5-inch pressure refuel adapter per military specification MS24484. Their main features include an aluminum base and handle, a fluorosilicone O-ring seal, and antisparking brass chain lanyard (per industry standard RR-C-271) with a plastic tubing cover and corrosion resistant steel hooks.  Lanyards can also be fabricated with corrosion-resistant steel or flexible plastic and fuel resistant tubing. Optional features are also available such as key lock, ventilation, hinge, visual fluid level indicator, dust cover easy-lift handle and contoured adapter.

For additional information please consult the supplied documentation or contact us.

DUNLOP AIRCRAFT TYRES manufactures several different types of aircraft tIre for many applications: bias tIres for modern jet and military aircraft, radial tires for military jets, bias tires for helicopters and chined tyres used for nose wheel applications primarily on rear-engined jet aircraft   Different tire size designations grouped into various 'types' are also used such as Type III mainly for low-pressure service on older piston-driven aircraft or Type VII related to high-pressure tires with high load capacity designed for modern jet and turboprop aircraft. All DUNLOP aircraft tires are manufactured in accordance with TSO-C62, MIL-PERF-5041 or AIR8505A and/or applicable airframe manufacturer specifications.

DUNLOP aircraft tires are offered as NEW or RETREAD ( the second designated by the letters "RT" after the product reference number (SKU).

DUNLOP does not mandate a maximum shelf life for its tires, so long as the storage conditions are met. The company recommends that tires be kept in a store for no more than 12 years from their date of manufacture, if they are to stay serviceable.

DUNLOP aircraft tires have a warranty of 12 months from the date of their delivery. The company undertakes at its option to repair or replace them or refund the customer for any of the tires which are defective by reason of defective material, design or workmanship.

DUNLOP AIRCRAFT TYRES also produces aircraft inner tubes manufactured to rigorous standards which meet or exceed all commercial and military performance requirements, including MIL-I-5014 military specification (except for packaging).

They are made from natural rubber which ensures maximum life and meets cold temperature performance requirements.

DUNLOP inner tubes are factory balanced. The heavy spot is marked in red. If there is no red mark, the valve is considered the heavy spot. The valve stem, core and cap are manufactured for aircraft use and designed for high and low pressure requirements.

For additional information on DUNLOP AIRCRAFT TYRES  products please consult the supplied Guide and tire specification sheets.

High quality vinyl toggle switch covers that do not have a nipple at the end of the cover. Suitable for MS35058 series switches. Available in different colors.

CURTIS PLT-275AV Flush Valves 6 Holes' Adapter Plates Assembly.

Product Specifications:

Diameter: 2.75 in.

Depth: 640,000-650,000

From Mounting Surface to Bottom Hole Diameter: 1-1/2 in.

Not Certified

MAGNUM aircraft rescue ballistic parachute systems (also known as  Vertical Launch Systems, VLS) are manufactured by STRATOS 07 S.R.O with knowledge and long experience in the construction of system components including rocket motors. They include different series produced for many years (like 450, 450 Speed, 501, 601) & newer certificated rescue systems like Magnum 1201 & 1401 for heavier aircraft and higher deployment speeds. They are intended for use in hang-gliding, paragliding, powered hang-gliding, powered paragliding,  unpowered and powered gliders,  gyroplanes as well as a wide range of two- and multi-seat airplanes and helicopters, including Light Sport, Experimental and Ultralights with a maximum 3,960 pounds gross weight, and deployment speeds of up to 199 MPH. Magnum Ballistic Parachutes come in sofpacks or canisters. Rescue systems packed in the softpack are usually installed inside of the aircraft. Rescue systems packed in a duralminium container are installed mostly outside of the aircraft.

Please refer to tables of specifications and notes below for the selection of a right rescue system.

Notes:

The max take-off weight of the aircraft MUST NOT EXCEED the max allowable load of the rescue system.

If the aircraft Vne exceeds the max limiting speed for the rescue system deployment, mounting of the system should be done so that the pilot is informed of this speed.

MAGNUM ballistic parachute systems  are packaged in two parcels (one containing the parachute and the second containing the rocket). Because of the rocket, Haz-Mat shipping is required.

Appearing prices of MAGNUM rescue systems DO NOT INCLUDE cords between parachute and fuselage which are SOLD SEPARATELY. During the order, the length of activating cord from parachute to fuselage must be indicated. Other parts and accessories are also available at additional cost.

Aircraft braking systems serve a vital function during takeoff, landing and taxiing. Along with landing gear, aircraft wheels and brakes are critical to ensure safe and reliable aircraft ground operations under extreme forces, stress, as well as wear and tear from general operation and the environment. Commercial aircraft brakes are arranged in multiple disk pairs commonly referred to as Heat Sinks or Heat Packs (as they convert the kinetic energy of the moving airplane to heat energy). Initially made metal (steel) heat sinks are gradually replaced by those from carbon fibres (particularly on larger, long-haul commercial airplanes) due to their higher efficiency in braking applications, longer life-span, lower weight and resulting less fuel consumption and lower CO2 emission by the engines. 

Carbon and steel heat packs and parts are offered as part of our own labelled (AVIATIONEU NEW ERA) product lines. Sourced from quality suppliers these heat packs  feature high quality, safety, improved design, significant cost savings and fast deliveries. They can be used as  cost effective alternatives in many commercial aircraft platforms equalling or exceeding standards of  respective OEM products by leading manufacturers such as Honeywell Aerospace, Collins Aerospace/Goodrich Wheels & Brakes, Parker Meggitt Aircraft Braking Systems and Safran Landing Systems (formerly Messier-Bugatti-Dowty). They are  PMA approved (*) parts by the Civil Aviation Administration of China (CAAC) for use on an extensive list of Western and Eastern commercial (civil ) aircraft platforms including Boeing, Airbus, McDonnell Douglas, Ilyushin and others and are currently installed in aircraft operating by different air transport operators in China and other countries in the Middle-East, South and Central Asia and Africa.

Typical Aircraft Applications for steel and carbon heat packs include Boeing 737 / 757, Airbus A318 / A319 / A320 / A330 , McDonnell Douglas: MD82 /MD90  Xian MA60 etc. 

(*)  Parts Manufacturer Approval (PMA) is a combined design and production approval granted by a competent Civil Aviation Authority (CAA) to a manufacturer of aircraft parts for modification and replacement. Use of Civil Aviation Administration of China (CAAC) approved parts in other countries depends on existing bilateral agreements between CAAC and respective competent authorities in these countries.

For additional information please contact us.

When battery terminals with heavy current capacity and high conductivity are required AVIATIONEU NEW ERA SC HEAVY DUTY lug type battery terminals are recommended. Similar to the AVIATIONEU NEW ERA SC brass battery terminals except that they are are produced from pure copper  and tin plated, they are available in three versions: SC(JGA), SC(JGY) and SC(JGB). Please refer to the specifications table. They can be used with wire sizes 1.5-1000mm2 (16AWG - 777MCM). Sold in packs of 20 pieces each with Minimum Order Quantity (MOQ) 5 packs. The appearing price is for reference only. Please contact us for quotation.