INSTRUCTION AND MAINTENANCE MANUAL FOR JABIRU 2200 ...

Jabiru Aircraft Pty LtdInstruction & Maintenance ManualJabiru 2200 Aircraft EngineHydraulic Valve Lifter Models9.14 Subassembly H – Component Assembly ProcedureFinal AssemblyNo. Details Sign Sign DateH1 Apply Loctite 515 to crankcase halves;lubricate where necessaryH2 Locate camshaft and crankshaft incrankcase halfStage Stage Inspection Pre-joining Crankcase3H3 Locate crankcase half over crankshaft andcamshaftH4 Tension front (2) and rear (2) studsH5 Fit oil pump assembly and front sealhousingH6 Place all through bolts in crankcaseH7 Fit piston and cylinder assemblies andcheck circlipsStage Stage Inspection Piston/Circlips4H8 Tension the cylinder base studs to 25 ft.lbsthen 30 ft.lbsH9 Fit sumpH10 Fit heads to cylinder torque 12 ft.lbs / 24ft.lbsH11 Fit push rod and valve gear. Set gap to0.10” (0.25mm)H12 Check camshaft timing DEGREESH13 Fit fuel pumpH14 Fit engine mount plate and gearboxhousingH15 Fit flywheel alternator mount plate andignition coils and leadH16 Fit carby assemblyH17 Fit exhaust systemI hereby certify that the subassembly has been completed using the approved proceduresand data; and is fit for installation.Signed: _______________Date: ____________For Jabiru Aircraft Pty LtdProduction Certificate #444128Notes:This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled.REVISION 0 1 2 3 4 5 6 7 8 9 Dated : June 2010 Issued By: DPS Page: 94 of 116L:\files\Manuals_For_Products\Engine_Manuals\Transition\JEM2204-9_I&M_unsigned.docx