Eight Cylinder EGT w/TIT Kit – 2 1/2″ Clamp Probes
Eight Cylinder EGT with Turbine Inlet Temperature Kit and 2 1/2" Clamp Probes
The ET208T is a full color EGT instrument that provides simultaneous, real-time display of all eight cylinders and turbine inlet temperature. This kit includes eight 2 1/2" clamp type probes and one bayonet turbine inlet temperature Type-K ungrounded thermocouple probe, all connectors and installation hardware.
Exhaust gas and turbine inlet temperature functionality is TSO'd and meets the temperature accuracy requirements of SAE AS8005 for a Class IIa (+/- 1%) instrument. Functional displays include:
- Real-time eight cylinder and turbine inlet temperature display
- Menu select option for fast selection of display type
- Automated rich-of-peak (ROP) leaning function
- Automated lean-of-peak (LOP) leaning function
- Single cylinder and turbine inlet temperature monitoring while retaining graphic indications for all cylinders
- Graphic trend analysis and viewing of all cylinders and turbine inlet simultaneously
The ET208TP3 is TSO'd and STC'd as a primary replacement instrument under all flight conditions (day/night VFR and IFR).
Rolls-Royce® Spark Igniter Lead Assembly
CH53351 LEAD: SPARK IGNITER,ASSEMBLY
xCruze 100/110 Autopilot for Experimental Aircraft
tailBeacon | ADS-B Out, WAAS GPS
Fuel Flow Transducer | 7-90 GPH, Hall Effect, Straight Pick-up
Fuel Flow Transducer | 7-90 GPH, Hall Effect, Right Angle Pick-up
TRANSDUCER FUEL FLOW/160GPH/ST PICK UP
The transducer is a device that converts the mechanical motion of a spinning turbine into an electronic signal that is read by the fuel computer. The magnetic pick-up assembly detects the spinning turbine and counts the revolutions. This produces a series of pulses that is transmitted to the fuel computer. The computer uses the pulse frequency to calculate the fuel flow over time. The Shadin Avionics Company Incorporated-designed fuel flow transducer can be used in conjunction with all of our fuel totalizer units and fuel/airdata computers.
TRANSDUCER/70GPH W/ST PICK-UP + False
The transducer is a device that converts the mechanical motion of a spinning turbine into an electronic signal that is read by the fuel computer. The magnetic pick-up assembly detects the spinning turbine and counts the revolutions. This produces a series of pulses that is transmitted to the fuel computer. The computer uses the pulse frequency to calculate the fuel flow over time. The Shadin Avionics Company Incorporated-designed fuel flow transducer can be used in conjunction with all of our fuel totalizer units and fuel/airdata computers.
Nine Cylinder CHT 12mm Ring Kit
Nine Cylinder CHT Kit with 12mm Ring Probes
The CT209 is a full color CHT instrument that provides simultaneous, real-time display of all nine cylinders. This kit includes nine ungrounded 12mm ring thermocouple probes, all connectors and installation hardware.
Cylinder head temperature functionality is TSO'd and meets the temperature accuracy requirements of SAE AS8005 for a Class IIa (+/- 1%) instrument. Functional displays include:
- Real-time nine cylinder temperature display
- Single cylinder temperature monitoring while retaining graphic indications for all cylinders
- Graphic trend analysis and viewing of all cylinders simultaneously
- Programmable shock cooling monitor and indication
The CT209R2 is TSO'd and STC'd as a primary replacement instrument under all flight conditions (day/night VFR and IFR).
Nine Cylinder CHT 14mm Ring Kit
Nine Cylinder CHT Kit with 14mm Ring Probes
The CT209 is a full color CHT instrument that provides simultaneous, real-time display of all nine cylinders. This kit includes nine ungrounded 14mm ring thermocouple probes, all connectors and installation hardware.
Cylinder head temperature functionality is TSO'd and meets the temperature accuracy requirements of SAE AS8005 for a Class IIa (+/- 1%) instrument. Functional displays include:
- Real-time nine cylinder temperature display
- Single cylinder temperature monitoring while retaining graphic indications for all cylinders
- Graphic trend analysis and viewing of all cylinders simultaneously
- Programmable shock cooling monitor and indication
The CT209R4 is TSO'd and STC'd as a primary replacement instrument under all flight conditions (day/night VFR and IFR).
