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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: 94 of 116
L:\files\Manuals_For_Products\Engine_Manuals\Transition\JEM2204-9_I&M_unsigned.docx
9.14 Subassembly H
– Component Assembly Procedure
Final Assembly
No.
Details
Sign
Sign
Date
H1
Apply Loctite 515 to crankcase halves;
lubricate where necessary
H2
Locate
camshaft
and
crankshaft
in
crankcase half
Stage
3
Stage Inspection Pre-joining Crankcase
H3
Locate crankcase half over crankshaft and
camshaft
H4
Tension front (2) and rear (2) studs
H5
Fit oil pump assembly and front seal
housing
H6
Place all through bolts in crankcase
H7
Fit piston and cylinder assemblies and
check circlips
Stage
4
Stage Inspection Piston/Circlips
H8
Tension the cylinder base studs to 25 ft.lbs
then 30 ft.lbs
H9
Fit sump
H10
Fit heads to cylinder torque 12 ft.lbs / 24
ft.lbs
H11
Fit push rod and valve gear. Set gap to
0.10” (0.25mm)
H12
Check camshaft timing DEGREES
H13
Fit fuel pump
H14
Fit engine mount plate and gearbox
housing
H15
Fit flywheel alternator mount plate and
ignition coils and lead
H16
Fit carby assembly
H17
Fit exhaust system
I hereby certify that the subassembly has been completed using the approved procedures
and data; and is fit for installation.
Signed: _______________
Date: ____________
For Jabiru Aircraft Pty Ltd
Production Certificate #444128
Notes: