CHT Gasket Probe

$120.00
The Cylinder Head Temperature (CHT) – Gasket Type (Washer) – You may install the probe on the upper or lower spark plug (the one that provides the best correlation with the other temperature probe). Due to the sparkplug location, the gasket probe may read 25’F higher (generally the sparkplug is the hottest part of the cylinder, which will cause this discrepancy).
  • 1 Thermocouple Type K CHT Gasket Probe

EGT Probe PN-M111

$120.00
Included with Probe: 1 Thermocouple type K probe 1 Stainless Steel Clamp Thimble 1 Stainless Steel Exhaust Seal Washer 1

CHT Bayonet Probe

$120.00
The Cylinder Head Temperature (CHT) – standard Bayonet – probe, has a captive 3/8-24 boss which is screwed into the base of the cylinder. The CHT port is predrilled by your engine manufacturer. The CHT probe has a screwdriver slot to facilitate tightening.
  • 1 Thermocouple Type K CHT Bayonet Probe

External GPS Antenna for EKPV

$115.00
The external GPS antenna connects to the EKP V power supply cable or the cockpit cradle via USB port.

TRIG TA50 – Compact GPS Antenna

Price range: $105.00 through $115.00
TA50 – COMPACT GPS ANTENNA This space saving WAAS antenna is perfect for gliders and light sport or experimental aircraft
Select options This product has multiple variants. The options may be chosen on the product page

Safety-Trim Dual Axis Wiring Harness

$106.69
Aircraft grade wiring harness for all Safety Trim single-axis models.   The wiring harness is 8ft long, color coded and utilizes mil-spec wire and connector terminations.   The wiring harness includes the recommended ON/OFF/Reverse switch.

Converter Connector Kit | Plastic, 4P, Solder, 10A | For LS03-05001-B

$103.44
The Converter Connector Kit (LS03-05026) is a plastic connector hood with the following accessories: back-shell, 4-40 hardware, 25 Pin d-sub,

IBBS STC Documents and Authorization Letter

$100.00
Includes all relevant STC documentation for the installation and use of the IBBS system under FAA AML STC SA04400NY and a copy of the authorization letter that provides sufficient evidence to use the STC to alter an aircraft, engine or propeller.