Continental IO-470 Series Aircraft Engine Operator Manual

Operator's manual for the Continental IO-470 series aircraft engine covering specifications, operating procedures, and maintenance.


Continental IO-470 Series Aircraft Engine Operator Manual - cover page
Brand
Continental Motors
Category
Motor
Document type
User Manual
Language
English
Pages
48
File format
PDF
File size
2.3 MB
Published
03 October, 2026
Updated
03 October, 2026
MD5 checksum
5A3A7A5EC7889F48034DFB2C4AA778A4

About this manual

This manual provides pilots and maintenance mechanics with essential information for operating and inspecting the Continental IO-470 series aircraft engine. It includes specifications, operating instructions, and guidance on daily and periodic inspections.

The document also contains fuel injector service procedures, performance charts, and troubleshooting tips, while directing users to the appropriate overhaul manuals for extensive repairs.

What's inside

  • Foreword
  • Specifications
  • Operating Instructions
  • Inspection and Maintenance
  • Fuel Injector Service and Maintenance
  • Performance Curves
  • Troubles and Repairs

Specifications

Number of Cylinders6
Cylinder Bore5 inches
Piston Stroke4 inches
Total Displacement471 cu.in.
Compression Ratio8.6:1
Rated Maximum Continuous Brake Horsepower250 bhp
Rated Maximum Continuous Speed2600 RPM
Oil Pressure (cruising)30‑60 psi
Oil Pressure (idle, minimum)10 psi
Oil Sump Capacity12 US quarts
Maximum Oil Consumption at Rated Power0.15 lbs/bhp/hr
Maximum Oil Temperature Allowable225 °F
Maximum Cylinder Head Temperature460 °F

Frequently asked questions

How many cylinders does the IO-470 engine have?

The IO-470 engine has six cylinders.

What is the recommended cruising oil pressure range?

The recommended oil pressure during cruising is 30 to 60 psi.

What is the rated maximum continuous brake horsepower?

The engine is rated for a maximum continuous brake horsepower of 250 bhp.

What is the minimum oil temperature for take‑off?

The minimum oil temperature for take‑off is 75 °F.

Download PDF (2.3 MB)

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