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Electronics International CGR-30C User Manual

Electronics International CGR-30C
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Primary Glass Panel Engine MonitorPrimary Glass Panel Engine Monitor
Primary Glass Panel Engine MonitorPrimary Glass Panel Engine Monitor
Primary Glass Panel Engine Monitor
CGR-30CCGR-30C
CGR-30CCGR-30C
CGR-30C
Installation InstructionsInstallation Instructions
Installation InstructionsInstallation Instructions
Installation Instructions
II 10291301
Electronics International Inc. Electronics International Inc.
Electronics International Inc. Electronics International Inc.
Electronics International Inc.
®®
®®
®
Rev: B, 5/11/15*
63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com 63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com
63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com 63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com
63296 Powell Butte Hwy • Bend, OR 97701 • (541) 318-6060 • Buy-EI.com
Model #:Model #:
Model #:Model #:
Model #:
S/N:S/N:
S/N:S/N:
S/N:
You must read this manual before installing or operating the instrument. This
manual contains warranty and other information that may affect your decision
to install this product and/or the safety of your aircraft.
The CGR-30C is a FAA Approved Primary Replacement
for Engine and Aircraft System Instruments

Table of Contents

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Electronics International CGR-30C Specifications

General IconGeneral
BrandElectronics International
ModelCGR-30C
CategoryMonitor
LanguageEnglish

Summary

Important Safety and Installation Notices

System Overview

System Description

Details the four major components of the CGR-30C installation: CGR Display, EDC-33P, Probes, and Wiring.

Operational Overview

Explains how the CGR system measures and displays engine/aircraft functions using probes and the EDC.

Installation Overview

Outlines the general steps for installing the CGR-30 system, including panel mounting and wiring.

Hardware Installation

Important Information and Initial Checkout

Crucial pre-installation checks, warranty review, and FAA approvals for installing the CGR-30 system.

Install the CGR Display

Guidance on mounting the CGR display unit in the aircraft instrument panel, ensuring proper fit and visibility.

Install the Temperature Probes

Instructions for installing various temperature probes (EGT, TIT, CHT, Oil Temp, Carb Temp, OAT).

Install the Pressure Transducers

Procedures for mounting and connecting pressure transducers for Manifold Pressure, Gyro Vacuum, Oil, and Fuel pressure.

Install the Shunt (for Amps)

Details on installing an external shunt for accurate amperage measurement and its connection to the system.

Install the Fuel Flow Transducer

Instructions for mounting the fuel flow transducer in the fuel line for accurate fuel flow measurement.

Install the EI P-300C Fuel Level Probes

Guidance on installing capacitive fuel level probes, including connection to the EDC.

Install the EI P-300M Fuel Level Sender

Instructions for installing the magnetic float fuel level sender and its interface with the EDC.

Install the Resistive Fuel Level Module (RFLM-4-X)

Details on installing the RFLM module to interface resistive fuel level sensors with the EDC.

Install the Voice Alarm Control Panel (OEM Only)

Instructions for installing the AV-17CP Control Panel for voice alarms.

Install the Intensity Control Pot CP-1A (Optional)

Guidance on installing the CP-1A for controlling backlight intensity.

Install the Master Warning (red) and Caution (yellow) Lights

Instructions for mounting and connecting master warning and caution lights.

Install the EDC-33P

Procedure for mounting the Engine Data Converter (EDC-33P) and connecting its harnesses.

Install EDC Wire Harnesses and Route Wires

Attach the three EDC 37-pin Wire Harnesses to the EDC

Securing the EDC 37-pin wire harnesses to the EDC unit using supplied mounting screws.

Connect the EDC Harness to the Temperature Probes

Routing and connecting EDC harness cables to the appropriate temperature probes.

Connect the EDC Harness to the Pressure Transducers

Routing and connecting EDC harness cables to the appropriate pressure transducers.

Connect the EDC Harness to the Fuel Flow Transducer

Routing the fuel flow cable from the EDC harness to the Fuel Flow Transducer.

Connect the EDC Harness to the Existing Capacitive Fuel Level System

Connecting the EDC harness to an existing capacitive fuel level system.

Connect the EDC Harness to the EI P-300C Capacitive Fuel Level Probes

Routing EDC harness wires to EI P-300C capacitive fuel level probes.

Connect the EDC Harness to the EI P-300M Magnetic Fuel Level Senders

Routing EDC harness wires to EI P-300M magnetic fuel level senders.

Connect the EDC Harness to the RPM Signals

Connecting the EDC harness to RPM signals from magnetos or electronic ignition.

Set up the EDC for a 4 or 6-Cylinder Engine

Configuring the EDC for 4 or 6-cylinder engines using a strap on the bottom connector.

Install CGR Wire Harness and Route Wires

Attach the CGR 25-pin D-sub Connector to the CGR

Securing the CGR 25-pin D-sub connector to the CGR display unit.

Connect the EDC 5V-Serial Output Wire to the CGR 5V-Serial Input Wire

Connecting the EDC serial data output to the CGR serial input.

Connect the CGR Harness to the Master Warning and Caution Lights

Routing and connecting the CGR harness to the master warning and caution lights.

Connect the CGR Harness to the Voice Alarm Control Panel (OEM Only)

Connecting the CGR harness to the AV-17CP Control Panel for voice alarms.

Connect the CGR Harness to Power and Ground

Connecting the CGR harness to the aircraft's main bus and ground.

Mandatory System Setup and Checkout

Power-On Checkout

Performing initial system checks after powering up the CGR unit.

Ground Run Checkout

Verifying proper operation of all CGR functions with the engine running on the ground.

First Flight Checkout

Conducting checks during and after the first flight to ensure proper function and safety.

Installation Data

Instructions for Continued Airworthiness (ICA)

Information on maintenance requirements and procedures for ensuring continued airworthiness.

Airworthiness Limitations

FAA-approved maintenance requirements and operational limitations for the CGR-30 system.

Troubleshooting

CGR or EDC Problem

Diagnosing issues related to the CGR display or the Engine Data Converter (EDC).

Pressure Problem with one Function

Troubleshooting inaccurate or zero readings for a single pressure function.

Temperature Problem on all Channels

Diagnosing issues affecting all temperature channels simultaneously.

Temperature Problem with one Function

Troubleshooting inaccurate or zero readings for a single temperature function.

RPM Problem

Diagnosing inaccurate, jumpy, or zero RPM readings, often related to isolator issues.

Fuel Flow Problem

Troubleshooting inaccurate, jumpy, or zero fuel flow readings, including K-factor and transducer issues.

Amp Problem

Diagnosing inaccurate, jumpy, or zero amperage readings, typically related to wiring or fuses.

Resistive Fuel Level Problem

Troubleshooting issues with resistive fuel level sensors and their interface module (RFLM).

Capacitive Fuel Level Problem

Diagnosing inaccurate or zero readings from capacitive fuel level probes.

Technical Data

Specifications / Features

Detailed specifications, functions, and features of the CGR-30P and CGR-30C systems.

Error Messages

Explanation of common error messages displayed by the CGR system.

Input Configuration

Details the input channels available for the EDC-33P and EDC-33T-XX models.

Amps

Technical specifications and input details for amperage measurements.

Fuel Flow

Technical specifications and input details for fuel flow measurements.

Temperature

Technical specifications and input details for temperature measurements.

Resistive Fuel Level

Technical specifications and input details for resistive fuel level measurements.

Capacitive Fuel Level

Technical specifications and input details for capacitive fuel level measurements.

Pressure

Technical specifications and input details for pressure measurements.

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