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Lycoming IO-390-D Series User Manual

Lycoming IO-390-D Series
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© 2020 Avco Corporation. All Rights Reserved.
Engine Installation and Operation Manual
IO-390-D Series
March 2020
Part No. IOM-IO-390-D Series

Table of Contents

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Lycoming IO-390-D Series Specifications

General IconGeneral
Number of Cylinders4
Compression Ratio8.7:1
Ignition SystemDual Magneto
Engine TypeHorizontally Opposed, Air-Cooled
Displacement390 cubic inches (6.4 L)
Bore5.125 in (130.2 mm)
Maximum Power210 hp at 2700 RPM
Fuel TypeAvgas 100LL
Fuel SystemInjection
Oil Capacity8 quarts (7.6 L)
TBO (Time Between Overhaul)2000 hours
AspirationNormally Aspirated
CoolingAir-cooled

Summary

Record of Revisions

Service Document List

List of Figures

List of Tables

Abbreviations and Acronyms

Introduction

Scope of this Manual

Details the manual's coverage, including installation, operation, and fuels.

Compliance Requirements

Explains adherence to regulations and service document supersessions.

Warning, Cautions, and Notices

Defines safety advisory message conventions used in the manual.

System Description

Cylinders

Describes the four cylinders and their components.

Crankcase

Details the crankcase construction and its role in the engine.

Ignition System

Explains the ignition system components, including spark plugs and harness.

Fuel Injection System

Outlines the fuel manifold, injectors, nozzles, and pump.

Lubrication System

Describes the wet sump, oil pump, filter, and lines.

Cylinder Number Designations

Identifies cylinder numbering and firing order.

Engine Reception and Lift

Acceptance Check

Verifies engine serial and model numbers against documentation.

Lift the Engine

Instructions for safely lifting the engine using proper equipment.

Requirements for Engine Installation

Step 1. Prepare the Engine

Details preparation for new, rebuilt, or stored engines.

Prepare a Stored Engine for Installation

Procedures for depreservation of engines stored for extended periods.

Step 2. Supply Interface Items

Lists optional equipment and requirements for airframe preparation.

Step 6. Make Electrical Interface Connections

Connecting electrical interfaces for engine operation.

Engine Installation

Step 1. Install the Engine on Mounts

Procedures for mounting the engine securely to the airframe.

Step 8. Connect Fuel Lines

Connecting fuel lines, ensuring no contamination or leaks.

Step 11. Add Oil

Procedures and precautions for adding engine oil.

Step 12. Engine Pre-Oil Procedure

Critical steps to circulate oil before initial start to prevent damage.

Field Run-In

Ground Operational Test

Steps for conducting the ground operational test.

Engine Initiation

Warranty Requirement

Emphasizes adherence to manual specifications for warranty.

Step 1. Pre-Flight Inspection for Engine Initiation

Checklist for pre-flight checks before engine initiation.

Step 2. Engine Start

Detailed procedure for starting the engine.

Step 5. Break-In/Flight Test/50-Hour Operation

Process for seating piston rings and stabilizing oil consumption.

Engine Operation

Step 1. Pre-Flight Check

Pre-flight checks before starting the engine for routine operation.

Step 2. Engine Start

Routine procedure for starting the engine.

Step 4. Engine Operation

Procedures for normal engine operation, including in-flight.

Fuel Mixture Leaning

Guidance on leaning the fuel mixture for performance and economy.

Engine Conditions

Apply Heat to a Cold Engine

Procedures for pre-heating engines in cold weather.

Cold Weather Engine Start

Recommended procedures for starting engines in cold weather.

Overspeed

Actions to take if the engine operates above its rated RPM.

Low Oil Pressure During Flight

Procedures for handling low oil pressure during flight.

Engine Preservation and Storage

Engine Corrosion and Prevention

Measures to prevent corrosion on engines not in frequent use.

Engine Preservation Guidelines - 31 to 60 Days

Procedures for preserving engines stored for 31-60 days.

APPENDIX A ENGINE SPECIFICATIONS AND OPERATING LIMITS

APPENDIX B PERFORMANCE DATA

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