INSTRUCTION AND MAINTENANCE MANUAL FOR JABIRU 2200 ...

More documents

Recommendations

Info

Jabiru Aircraft Pty LtdInstruction & Maintenance ManualJabiru 2200 Aircraft EngineHydraulic Valve Lifter Models‣ Use 2.2 litres of W100 oil for normal operation or W80 oil for cold weather operation.Shell also manufacture a multigrade oil Aeroshell 15W50 which is particularly suited foroperations in cold climates.CAUTION: UNDER NO CIRCUMSTANCES USE AUTOMOTIVE OIL IN THIS ENGINE.Use only oils which are designed for Air Cooled Aero Engines.‣ Some brands of automotive oils have been shown to cause very rapid cylinder wear.This will not be covered under Jabiru’s Limited, Express warranty.‣ Operate engine only on AVGAS 100LL or highest octane available MOGAS (Minoctane 95 RON). Failure to do so could result in engine damage and void Jabiru’sLimited Express Warranty.CAUTION:USE OF OIL/FUEL ADDITIVES VOIDS JABIRU’S LIMITED, EXPRESS WARRANTYThis 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: 80 of 116L:\files\Manuals_For_Products\Engine_Manuals\Transition\JEM2204-9_I&M_unsigned.docx
Jabiru Aircraft Pty LtdInstruction & Maintenance ManualJabiru 2200 Aircraft EngineHydraulic Valve Lifter Models9 Service Documentation9.1 Subassembly A – Component Assembly ProcedureCrankshaft, Propeller Mount Flange & ConrodsStage 1No. Details Sign Sign DateA1 Inspect for Burrs, Oil Holes,Chamfers; Clean Crankshaft,Conrods and PropellerMount PlateA2 Inspect Oil Holes and InsertWelch PlugsA3 Measure Crankshaft (refer toGoods Inwards InspectionSheet)A4 Inspect and MeasurePropeller Mount FlangeA5 Inspect and MeasureConrods (refer to GoodsInwards Inspection Sheet)A6 Mount Propeller MountFlange to crankshaft; UseLoctite 620, Torque to30ft.lbs / Lockwire 3A7 Fit the Conrods to theCrankshaft; Use Loctite 620on the bolts and torque to18ft.lbsA8 Stage Inspection ofAssembly –Conrods/CrankshaftI 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:3 For std prop flange length onlyThis 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: 81 of 116L:\files\Manuals_For_Products\Engine_Manuals\Transition\JEM2204-9_I&M_unsigned.docx
Page 1 and 2:
INSTRUCTION AND MAINTENANCE MANUALF
Page 3 and 4:
Jabiru Aircraft Pty LtdInstruction
Page 5 and 6:
Page 7 and 8:
Page 9 and 10:
Page 11 and 12:
Page 13 and 14:
Page 15 and 16:
Page 17 and 18:
kWkWNmNmJabiru Aircraft Pty LtdInst
Page 19 and 20:
Page 21 and 22:
Page 23 and 24:
Page 27 and 28:
Page 29 and 30: Jabiru Aircraft Pty LtdInstruction
Page 79: Jabiru Aircraft Pty LtdInstruction
show all

INSTRUCTION AND MAINTENANCE MANUAL FOR JABIRU 2200 ...

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?