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Flybox Avionics ⏳ Available on Backorder

Eclipse NG IFIS

Part No / SKU: 701002
£3,423.00 inc. VAT
📦 Backorder Item

This item is currently out of stock but is available to backorder. Placing your order reserves your position in our next incoming shipment from the manufacturer. We will keep you notified with delivery updates when able.

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Flybox Flagship Glass Cockpit

Flybox Eclipse NG MFD / IFIS (Integrated Flight & Engine System)

The Flybox Eclipse NG MFD / IFIS is the definitive all-in-one avionics system engineered for Ultralight, Light Sport (LSA), and Experimental aircraft. Designed to act as the primary operational hub in modern glass cockpits, it pairs a complete Primary Flight Display (PFD) on the left with a dedicated, full-scale Engine Information System (EIS) on the right—combining air data, AHRS, engine pressures, all-cylinder CHT/EGT, fuel computers, and airframe status into a single sleek panel display.

Display Mode PFD (Left) + EIS (Right)
Panel Cutout 170.0 × 116.0 mm
Pneumatic Ports 3x (Pitot, Static & MAP)
Engine Senders Full CON2 & CON3 Sockets

Comprehensive Engine & Airframe Management

The right half of the Eclipse NG MFD / IFIS permanently organizes your complete powerplant telemetry into clean visual zones:

01

Power & Pressures

Continuous large numerical and arc readouts for Engine RPM, Manifold Absolute Pressure (MAP in inHg via rear brass barb), Oil Pressure (bar or psi), and Fuel Delivery Pressure with customisable limit arcs.

02

All-Cylinder CHT & EGT

Multi-column vertical bargraph displaying up to 6x Cylinder Head Temperatures and 6x Exhaust Gas Temperatures simultaneously, featuring automatic peak detection and delta spread tracking for mixture leaning.

03

Fuel Reserves & Flow Computer

Monitors up to 3 individual fuel tank levels (Left, Main, Right) via capacitive or resistive senders, paired with dual pulse flow inputs for live burn rates, endurance time-to-empty, and GPS nautical reserve projection.

04

Airframe Controls & Status

Includes real-time on-screen indicators for elevator trim position, flap potentiometer setting, three landing gear status lights, bus voltage, current draw, and an intelligent pre-takeoff engine readiness monitor.


Technical Specifications

Outer Bezel Dimensions 188.50 mm Wide × 136.10 mm High
Panel Cutout Dimensions 170.00 mm Wide × 116.00 mm High (with 3.50 mm corner radii)
Chassis Depth 45.30 mm (Body) / 99.10 mm (Total depth including rear D-Sub connectors & harness clearance)
Operating Voltage & Current 10 V – 30 V DC (approx. 0.5 A typical current consumption)
Pneumatic Inputs 3x Barbed ports: Pitot (Dynamic), Static, and Manifold Absolute Pressure (MAP)
Engine Senders Harness (CON2) 37-Pin D-Sub: Oil P/T, Fuel P, Coolant T, OAT, 3x Fuel Tanks, 2x Flow, Trim, Flaps
Thermocouple Harness (CON3) 25-Pin D-Sub: Up to 6x CHT + 6x EGT channels (ungrounded K-Type or J-Type)
Digital Communication Busses CAN1 (Autopilot & Flybox network) • ECU CAN (Rotax 912iS/915iS telemetry)
Video & Audio Interfaces 3x Composite PAL video inputs • Intercom audio line-out for spoken voice warnings
Alarm Annunciation 2x Master Alarm outputs (NPN open-collector, max 500 mA)
Housing Construction CNC-machined solid aluminium case with rear cooling heatsink • -20°C to +70°C
Installation Advisory: Ensure at least 2 cm of clearance around the instrument casing and heatsink for convective airflow. The main power ground (CON1 Pin 2) should be connected directly to the engine block via the shortest possible path. Thermocouple wires connecting to CON3 must be crimped into the supplied D-Sub contacts and never soldered.
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User & Installation Manual
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Technical Inquiry for Eclipse NG IFIS

Confirm wiring loom compatibility, panel depths, or kit lead times with our engineering team.