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Jabiru Aircraft
Pty Ltd
Instruction & Maintenance Manual
Jabiru 2200 Aircraft Engine
Hydraulic Valve Lifter Models
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REVISION
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Dated : June 2010
Issued By: DPS
Page: 42 of 116
L:\files\Manuals_For_Products\Engine_Manuals\Transition\JEM2204-9_I&M_unsigned.docx
No.
Operation
Tools Required
-
Rods will need to be heated
-
Big End Bolts are Discarded on Removal
Hot Air Gun
Rags
45
Remove Rod Bearing Inserts
Note
- visually inspect for marks and scratches
- keep matched to their seat
-
46 Remove Camshaft Gears. Discard Camshaft
Bolts. Remove welsh plug in rear of camshaft.
-
7.5
2200 ENGINE OVERHAUL
Inspection and Assembly of Sub-Assemblies
a)
Sub-Assembly A - Crankshaft, Prop Mount and Con Rods.
b)
Sub-Assembly B - Crankcase and Camshaft.
c)
Sub-Assembly C - Pistons, Cylinders and Cylinder Heads.
d)
Sub-Assembly D - Sump and Oil Pump
e)
Sub-Assembly E - Flywheel, Ignition Coils and Alternator
f)
Sub-Assembly F - Gear Case
g)
Fuel Pump and Carburettor
h)
Final Assembly of Sub-assemblies
i)
Run In: Engines can be run in statically using suitable mount structure and very
large specially constructed air ducts or in the airframe in flight with extreme care.
Run In program can be found at the end of the build sheets (see also early run
notes section).
j)
Overhaul: The overhaul of any engine is an exacting science. Approved Jabiru
service centres as well as Jabiru can provide this service.