TM 55-2835-208-232-14 DISASSEMBLE COMBUSTOR ASSEMBLY2-14INITIAL SETUPGeneral Safety Instructions:Applicable Configurations:Tools:RubberAllEngine Repairman’s Tool KitNSN 5180-00-323-4944GlovesNSN 8415-00-266-8677Eye ProtectionMaterials:NonePersonnel Required:68B Aircraft Powerplant RepairerEquipment Condition:Off APU TaskRemove combustor section(Task 2-13)When handling combustor assembly internalparts that have been exposed to fuels con-taining tetra-ethyl lead, ensure that the byproduct (poisonous lead oxide) is not in-haled or taken into the body through cuts orother external openings. If accidental ex-posure occurs, drench affected area withlarge amounts of clear water, and obtainim-mediatemedicalattention.Gloves and gog-gles shall be worn at all times when handlingcontaminated parts.1.2.3.4.Place combustor assembly on clean worksurface with exhaust end down.Removelockwire(E16) from bolts (1)and discard.Remove four (4) combustor locating bolts(1) and liftcombustorliner(2)outofcombustor housing (3)Remove and discard six packings (4)from combustor liner (2)FOLLOW-ON MAINTENANCE:NoneEND OF TASK2-30Change 4
Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business