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Continental C 125, C 135, C 145, O-300 aircraft engine overhaul manual Preview image 1
Continental C 125, C 135, C 145, O-300 aircraft engine overhaul manual Preview image 2
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Continental C 125, C 135, C 145, O-300 aircraft engine overhaul manual

Includes the following models

  • C 125
  • C 135
  • C 145
  • O-300 / Continental Motors

File specifications

File size: 58.21 MB
File type: PDF
Language: English

Printable: Yes
Estimated download time: 1.19 Minutes
$16.99 Instant Download

Product Information

Table of Contents

Section 1: Table of Specifications

  • Table of Limits

Section 2: Description and Principles of Operation

  • General Description
  • Cylinders and Valve Mechanism
  • Crankcase, Camshaft, Crankshaft, and Connecting Rods
  • Lubrication System
  • Cooling System
  • Fuel System
  • Ignition System

Section 3: Operating and Maintenance Instructions

  • Introduction, Inspection, and Preparation for Overhaul
  • Preservation of Engines for Storage
  • Preparation of Engines for Installation on Aircraft

Section 4: Pre-Overhaul Procedures

  • Disassembly, Cleaning, and Inspection
  • Removal of Engine from Aircraft
  • Preparation of Removed Engine for Overhaul
  • Disassembly Procedures

Section 5: Engine Overhaul Instructions

  • Cleaning and Inspection
  • Nondestructive Testing
  • Assembly Procedures
  • Final Assembly and Adjustment

Section 6: Accessories

  • Carburetor
  • Magneto
  • Generator
  • Starter

Section 7: Installation of Engine on Aircraft

  • Installation Instructions
  • Post-Installation Inspection
  • Engine Test Run

Section 8: Service Inspection and Associated Maintenance

  • General Service Inspections
  • Engine Operating Procedures
  • Periodic Inspections and Checks
  • Troubleshooting and Repair
  • Special Procedures

Section 9: Appendices

  • List of Tables
  • List of Illustrations

List of Tables

  • Table I: Characteristics and Dimensions
  • Table II: Cylinder and Valve Mechanism
  • Table III: Crankcase, Camshaft, Crankshaft, and Connecting Rods
  • Table IV: Lubrication System
  • Table V: Cooling System
  • Table VI: Fuel System
  • Table VII: Ignition System
  • Table VIII: Nondestructive Testing Limits
  • Table IX: Engine Assembly Torques
  • Table X: Carburetor Specifications
  • Table XI: Magneto Specifications
  • Table XII: Generator Specifications
  • Table XIII: Starter Specifications
  • Table XIV: Post-Overhaul Test Limits

Index of Illustrations

  • Three-Quarter Left Front View - O-300
  • Right Rear View - O-300
  • Right Rear View - O-300-A
  • O-300 Crankshaft Hydraulic Tappets
  • Cylinder with Rocker Box Removed
  • Typical Section Showing Gear Trains
  • Installation Drawings
  • Ignition Wiring Diagram for Scintilla
  • Ignition Wiring Diagram for Slick Magnetos
  • Right Magneto
  • Left Magneto
  • Accessory Drive
  • Preparation for Removal
  • Engine Removal from Aircraft
  • Disassembly Procedures
  • Inspection of Crankcase
  • Inspection of Crankshaft
  • Installation of Crankshaft
  • Assembly of Connecting Rods
  • Valve and Seat Grinding
  • Installation of Valve Mechanism
  • Installation of Cylinder Assemblies
  • Final Assembly Procedures
  • Installation on Aircraft
  • Post-Installation Inspections
  • Engine Test Run

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