Top quality shielded & jacketed aircraft wire by ACS  conforming to MIL-C-27500 specification which replaces MIL-C-7078/3. It incorporates MIL-W-22759/18 basic wire and features a Tefzel insulation, a shield of tin- plated copper braid and a jacket of Tefzel. It is temperature rated to 150°C & voltage rated at 600 volts. Available in different gauge(*) sizes. Sold in feet in 10 ft increments only. Multiple conductor wires are also available by ACS (please to our separate product presentation).

(*) Wire gauge is a measurement of wire diameter. This determines the amount of electric current a wire can safely carry, as well as its electrical resistance and weight. 8 Gauge shielded wire is used in converting generator systems to alternators.

The EATON AEROQUIP AE102 Aerospace  Firesleeve was specially developed to meet the fire resistance requirements of FAA TSO C53a or TSO-C75. This firesleeve can be indentified by its orange colored outer surface.  It can be used for all fuel, oil, hydraulic, fire extinguisher & propeller feathering lines for "Fire-proof"(*)  hose lines functioning effectively within a continuous operating temperature range of -65F to +450F (-54C to +232C). It is denser and more tightly woven and has more fiberglass than most of the competition. Even the thickness of the protective silicone is better. Available in different internal diameters in inches. Sold by the foot.

The EATON AEROQUIP AE102 can be used with EATON AEROQUIP hoses and 900591B clamps to secure firesleeve material on each end over the basic hose assembly. Please refer to chart for correct size or contact us for additional information. 

(*) Conforming with FAA requirements, "Fire-resistant"hose  lines must withstand a 5-minute exposure under specified flow conditions without failure. "Fire-proof" hose lines must withstand a direct flame for 15 minutes.

Structural screws are made of alloy steel, are properly heat treated, and can be used as structural bolts. Those commonly used in aircraft applications are manufactured to aerospace/military standards/specifications. They are offered as part of our own branded (AVIATIONEU NEW ERA) product lines structured in different series based on the standard of their conformance. Some of the screws commonly used include NAS204 through NAS235 and AN509/AN525 series. 

AN525/AN525R Series high-strength structural washer head (AN525) and cross-recessed (Phillips) head (AN525R) screws, fabricated from alloy steel per specification QQ-S-689. Tensile strength 125,000 PSI. Cadmium plated per QQ-P-416A, Type II, Class 3.  

The AN525 washer head structural screws provide a large contact area. The AN509R (100° countersunk) Phillips head screws are used in countersunk holes where a flush surface is necessary. These have been replaced by MS24694 Series structural screws of the respective materials and finishes.

Structural screws have a definite grip and the same shear strength as a bolt of the same size. Shank tolerances are similar to AN hex head bolts, and the threads are National Fine. Structural screws are available with round, brazier, or countersunk heads. The recessed head screws are driven by either a Phillips or a Reed and Prince screwdriver. Sourced from quality suppliers, AVIATIONEU NEW ERA structural screws are offered in different thread sizes and lengths in inches and sold in pieces. For more information, please refer to the individual product presentations, the supplied documentation or contact us.

In contrast to the commercial cables, aircraft  cables are lubricated providing substantially better fatigue life. They undergo extensive testing and are certified MIL-DTL-83420 and QPL specifications. Available in galvanized or stainless steel versions, diameters in inches, strengths and methods of construction (7X7, 7X19 or 1X19). The strength units are lbs. Unit of measure and sale is feet. 

AN hex head bolts in different series are offered under AVIATIONEU NEW ERA product series. Sourced from quality vendors, these bolts are manufactured to the US Army-Navy (AN) standard, predecessor to Mil-Spec (MS), superseded by the National Aerospace Standard (NAS). Commonly used in aviation for either tensile/shear load applications. Made from high-strength type 4037 or 8740 alloy steel or 431 Stainless Steel (CRES) and cadmium plated for superior corrosion resistance (compared to commercial grade zinc plated bolts) they are offered with shank drilled for cotter pin or undrilled for stop nut application, and with a drilled head for safety wire or without. Minimum Tensile Strength (Steel and CRES) - 125,000psi. The length of AN aircraft bolts is measured from under the head to the end of the shank. The "grip" is the unthreaded portion of the shank. Threads are pressed into the steel, not cut, thus maintaining strength throughout the entire shank. The surface under the head of AN bolts is designed to be a bearing surface to reduce non-uniform stress as the bolt is torqued thus reducing premature fatigue. The following letters are used in the product part  numbers.

"A" after the dash number for bolts with undrilled shank

"C"  for bolts made of 431 Stainless Steel (CRES)

"H" after the AN number for bolts with drilled head (eg. AN4H-15)

 AN3 through AN20 Series bolts are superseded by NASM3 through 20 Series. The part numbers in both series have not been changed. 

Specification Details:

AN3 through AN20 (REV. 12), Military Specification Sheet: Bolt -Machine, Aircraft [superseded by NASM3 through 20]. This specification covers aircraft machine bolts part numbers, AN3, AN4, AN5, AN6, AN7, AN8, AN9, AN10, AN14, AN16, AN17, AN18, and AN20. AN3 THRU AN20  is canceled and superseded by NASM3 THRU NASM20. The Part Identification Number (PIN) for AN3 THRU AN20 REV. 12 and the part number for NASM3 THRU NASM20 are identical. The part numbers have not been changed.

AN hex head bolts in different series are offered under AVIATIONEU NEW ERA product series. Sourced from quality vendors, these bolts are manufactured to the US Army-Navy (AN) standard, predecessor to Mil-Spec (MS), superseded by the National Aerospace Standard (NAS). Commonly used in aviation for either tensile/shear load applications. Made from high-strength type 4037 or 8740 alloy steel or 431 Stainless Steel (CRES) and cadmium plated for superior corrosion resistance (compared to commercial grade zinc plated bolts) they are offered with shank drilled for cotter pin or undrilled for stop nut application, and with a drilled head for safety wire or without. Minimum Tensile Strength (Steel and CRES) - 125,000psi. The length of AN aircraft bolts is measured from under the head to the end of the shank. The "grip" is the unthreaded portion of the shank. Threads are pressed into the steel, not cut, thus maintaining strength throughout the entire shank. The surface under the head of AN bolts is designed to be a bearing surface to reduce non-uniform stress as the bolt is torqued thus reducing premature fatigue. The following letters are used in the product part  numbers.

"A" after the dash number for bolts with undrilled shank

"C"  for bolts made of 431 Stainless Steel (CRES)

"H" after the AN number for bolts with drilled head (eg. AN3H-15)

 AN3 through AN20 Series bolts are superseded by NASM3 through 20 Series. The part numbers in both series have not been changed. 

Specification Details:

AN3 through AN20 (REV. 12), Military Specification Sheet: Bolt -Machine, Aircraft [superseded by NASM3 through 20]. This specification covers aircraft machine bolts part numbers, AN3, AN4, AN5, AN6, AN7, AN8, AN9, AN10, AN14, AN16, AN17, AN18, and AN20. AN3 THRU AN20  is canceled and superseded by NASM3 THRU NASM20. The Part Identification Number (PIN) for AN3 THRU AN20 REV. 12 and the part number for NASM3 THRU NASM20 are identical. The part numbers have not been changed.

MAGNUM aircraft rescue ballistic parachute systems 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.