Operating instructions
Table Of Contents
- 1 Introduction
- 2 General Description
- 3 Special Tools and Equipment
- 4 Disassembly
- 5 Cleaning, Repair and Replacement
- 6 Inspection
- Definitions
- Magnetic Particle Inspection
- Critical New Part Dimensions
- Fluorescent Particle Inspection
- Dimensional Inspection
- Protective Coatings
- Crankcase Inspection
- Crankshaft Inspection
- Camshaft Inspection
- Connecting Rod Inspection
- Gear Inspection
- Piston Inspection
- Cylinder Inspection
- Inspection Chart
- Crankcase Stud Heights
- Mag Particle Inspection Procedures
- Table of Limits
- Torque Specifications
- General Torques
- Table of Limits Chart
- 7 Assembly of Subassemblies
- 8 Final Assembly and Test
- 9 IO-520-M
- 10 IO-520-BB, CB and MB

3-1
SECTION III
SPECIAL TOOLS AND EQUIPMENT
3-1. It is advisable to have an engine
transportation stand (Figure 3-4) on which the
engine can be inverted so certain parts can be
removed or installed easily.
3-2. The tool in Figure 3-1 is used for installing
the needle bearing in the starter adapter. This tool
can be manufactured locally in accordance with the
dimensions specified.
3-3. For replacing an outer sleeve on the ignition
harness, use a Thomas and Betts Crimping Tool,
No. WT-217.
3-4. For removing and replacing crankshaft blade
and counterweight bushings use Borrough’s Tool
No. 4965.
NOTE
Special tools for Aircraft Engine in
general and the IO-520 in particular can
be purchased from the Borrough’s Tool
and Equipment Corporation 2429 North
Burdick Street, Kalamazoo, Michigan
49007.
FIGURE 3-1. STARTER ADAPTER BEARING INSTALLER
FIGURE 3-2. CRANKSHAFT BLADE AND DAMPENER FIGURE 3-3. PISTON RING COMPRESSOR,
BUSHING REMOVER AND REPLACER BORROUGHS NO. 5201