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Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation and Maintenance ManualforProp De-Icing SystemsATA 30-60-02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsTABLE OF CONTENTSRRINTRODUCTIONINTRO-1SECTION I - DESCRIPTION AND OPERATION1A.B.12Prop De-Icing System ComponentsProp De-Icing System OperationSECTION II – INSTALLATION OF PROP DE-ICING SYSTEM 151920202431313334GeneralRemoval of Aircraft ComponentsModification of Aircraft ComponentsDe-Icer InstallationInstallation of Balance WeightsInstallation of Lead Strap Clamps or RestrainersInstallation of Rubber Restrainer StrapsQuick Disconnect System (QDS)Timer InstallationAmmeter, Switch, Circuit Breaker InstallationBrush Assembly Mounting Bracket InstallationSlip Ring InstallationPropeller Assembly InstallationBrush Assembly InstallationSystem WiringPost-Installation InspectionSECTION III PROP DE-ICING SYSTEM & COMPONENT MAINTENANCE35A.B.C.D.E.F.G.H.I.J.50-Hour Inspection100-Hour InspectionSlip Ring InspectionBrush Assembly InspectionTimer TestAmmeter TestWiringLightning Strike TestSystem TroubleshootingRepair Procedures35353639394141414148Typical Twin Engine De-Icing Systems SchematicDual Element Twin Engine De-Icing CycleSingle Element Twin Engine De-Icing CycleCounterweight Modification (Hartzell Compact Prop)Lead Configuration (Hartzell Compact Prop)Assembly & Wiring Details – Spinner Bulkhead (Hartzell Compact Prop)134666Figures12345678910111213Assembly & Wiring Details – Slip Ringer/Starter Ring Gear Assy (Hartzell Compact Prop)7Modified Balance Weight/Lead Strap Clamp Installation (4E1725)Lead Strap Clamp Installation (2E1063-4)Lead Strap Clamp Installation (2E1200-4)Nylon Tie Strap InstallationLead Strap Clamp Installation (3E1375)Restrainer Strap Installation (2E1290 & 2E1291)8999101030-60-02 Page TC1 of 2Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing 93031323334353637383940Lead Strap Clamp Installation (2E1285-1 & 2E1285-2)Lead Strap Clamp Installation (2E1087-3)Restrainer Strap InstallationTerminal Clamp Installation (3E1883-2 & 2E1848-1)Rubber Restrainer Strap Installation (2E1291 & 3E1470)Three Wire Normal Rotating Prop InstallationThree Wire Counter-rotating Prop InstallationTwo Wire Normal Rotating Prop InstallationTimer Mounting MethodsTypical Brush Assembly Mounting Bracket InstallationTypical Brush Assembly Mounting Bracket InstallationTypical Brush Assembly Mounting Bracket InstallationTypical Brush Assembly Mounting Bracket InstallationTypical Brush Assembly Mounting Bracket InstallationTerminal StripTerminal BlockLead Clip & Cable Clamp InstallationTerminal Strip VariationsSlip Ring Assembly Mounted on Spinner BulkheadSlip Ring Assembly Installation on Crankshaft or Prop Hub FlangeSlip Ring Assembly Installation on Crankshaft or Prop Hub FlangeTypical Slip Ring/Starter Ring Gear Assembly InstallationPositioning Spinner Adapter RingSlip Ring/Starter Ring Gear Assembly InstallationHose ClampsChecking Slip Ring Run-out (Alignment)Brush Alignment – ProjectionBrush Alignment – FaceAngular Brush Alignment AdjustmentAngular Brush Alignment 27282929303132323232TABLE OF CONTENTS414243Angular Brush Alignment AdjustmentEngine Firewall ConnectorMeasuring Slip Ring Minimum Dimension323437Component Groups Replaceable with QDSSlip Ring Minimum DimensionsTimer OperationTroubleshooting15384044Tables123430-60-02 Page TC2 of 2Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsINTRODUCTIONA.General1.2.This manual supersedes Goodrich Reports 68-04-712 and 70-04-700This manual provides installation, maintenance and repair information for Goodrich electrothermalpropeller de-icing systems and components installed on general aviation aircraft. Each system and itscomponents are uniquely designed for one application, although operation, installation, maintenanceand repair procedures may be common or similar. The Aircraft Manual (AMM) applicable to eachaircraft model contains specific information not included in this manual.Information about de-icing systems and/or components not manufactured by Goodrich must beobtained from the component or system approval holder.This manual is intended for use in conjunction with:3.4.- Applicable Aircraft and/or Prop Manufacturer manuals and instructions- Applicable Goodrich General Arrangement Drawing- Goodrich ATA 30-60-07 Removal & Installation Manual Electrothermal Prop De-Icers.- Goodrich Prop De-Icing Systems Replacement Parts List5.6.7.8.De-icing system installation, maintenance and repair must comply with FAA Advisory Circular 43 andsuperseding FAA releases. Safety wiring must be installed in accordance with C.A.R. Part 18 [Ref.C.A.R. 18.30-6(3)] and MS335440.Aircraft and/or prop manufacturers may modify a Goodrich de-icing system, making the instructions inthis manual incomplete or not applicable.For technical assistance call 1-800-334-2377 (United States, Canada and Puerto Rico) or330-374-3743/3706/2139 (other locations), or fax 330-374-2290.DefinitionsApproval HolderBrush AssemblyDrawingLong lead de-icerOptionalSlip Ring9.aircraft or prop manufacturer or modification house that holds a TypeCertificate or Supplemental Type Certificate for the prop de-icing system ona particular prop or aircraft.modular brush assembly or brush block assembly, except as specificallydistinguished. In this manual illustrations may depict either brush blockassemblies or modular brush assemblies, but are valid for both.applicable Goodrich General Arrangement Drawing.a de-icer without a separate de-icer wire harnesscomponent or procedure is not applicable to all de-icing systems.slip ring assembly or slip ring/starter ring gear assembly, except asspecifically distinguished.AbbreviationsAM Aircraft ManufacturerAMM Aircraft Maintenance ManualPM Propeller ManufacturerPMM Propeller Manufacturer’s ManualProp propeller or propeller assembly30-60-02 Page Intro 1 of 1Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsSECTION IDESCRIPTION AND OPERATIONPROP DE-ICING COMPONENTS AND SYSTEMA.Prop De-Icing System Components1.A prop de-icing system consists of the components shown in Figure 1, this page. Quantitydepends on application.2.Propeller De-Icing System Component Operationa.b.c.d.e.f.g.A prop de-icer is electrically heated, manufactured with special wire or foil, protected byfabric and rubber plies that resist oil, erosion and abrasion. One side has a dull, fabricimpressioned finish to provide good bonding surface.A wire harness may be used to electrically connect components. For example, a de-icerwire harness may connect de-icer leads to slip ring assembly leads.A slip ring and a brush assembly conduct electric power to the de-icers. The brushassembly, typically mounted on the engine, contains spring loaded brushes that contactrotating copper rings on the slip ring.A timer distributes power to the system in timed intervals in specific sequence.An ammeter is used to indicate system current flow. The ammeter has an internal orexternal shunt.A switch or circuit breaker/switch is used to cut power in case of overload. Somesystems include an extra circuit breaker between system and power supply.Some systems include additional components. Check AMM for complete systeminformation.30-60-02 SECTION I Page 1 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsB.Propeller De-Icing System Operation1.Electrically heated prop de-icers, combined with the centrifugal force of the rotating prop andairstream blast, remove accumulated ice. To conserve power and effectively remove ice, deicers are heated in timed intervals in specific sequence.Propeller de-icing systems differ in three areas:2.Number of engines:De-icer heating elements:Slip ring type:Single, twin, multipleSingle element has two leads (power & ground)Dual element has three leads (inboard, outboard & ground)Slip ring or slip ring/starter ring gear3.When the system is activated, power is cycled to the de-icers in timed intervals in specificsequence critical to effective ice removal. Sequence depends on number of de-icer elements andengines.Note:Typical heating interval is 34 seconds. Check AMM to confirm interval for your system. Thecycle may begin at any Phase, but the sequence remains the same.a. Dual element de-icer heating sequence, single engine aircraft:Phase 1:Phase 2:b.All outboard de-icer elements for specified intervalAll inboard de-icer elements for specified intervalDual element de-icer aircraft heating sequence, twin engine aircraft: (Figure 2, page 3)Note:Some twin engine aircraft have two independent timers that cycle power to de-icers on each propseparately as if there are two single engine systems.Note:The cycle may begin at any Phase, but the sequence remains the same.Phase 1:Phase 2:Phase 3:Phase 4:c.All outboard elements on 1st prop for specified intervalAll inboard elements on 1st prop for specified intervalAll outboard elements on 2nd prop for specified intervalAll inboard elements on 2nd prop for specified intervalSingle element de-icer heating sequence, single engine aircraft:Phase 1:Phase 2:All de-icers on for 90 seconds.All de-icers off for 90 seconds.d. Single element de-icer heating sequent, twin engine aircraft: (Figure 3, page 4)Phase 1:Phase 2:All de-icers on first prop heated for 90 secondsAll de-icers on second prop heated for 90 secondse. Check AMM for sequence on aircraft with three or more engines.30-60-02 SECTION I Page 2 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsFigure 2 – Dual Element Twin Engine De-Icing Cycle30-60-02 SECTION I Page 3 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsFigure 3 – Single Element Twin Engine De-Icing Cycle30-60-02 SECTION I Page 4 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsSECTION IIINSTALLATION OF PROP SYSTEM COMPONENTSNote:Read instructions entirely before proceeding, and follow in order provided.A.General1.Information provided is for initial system installation. Some procedures are not applicable forreplacement components or conversion kits. Refer to applicable manual for replacement orconversion.A de-icing system can be installed only on aircraft with sufficient electrical capacity for continuousprop de-icing system operation. Check AMM for required amperage, or perform electrical loadanalysis in accordance with FAA Advisory Circular 43.13-1, Chapter 11, Section 2 andsuperseding FAA releases, to determine if sufficient power is available.De-icing system installation affects weight and balance of prop. Consult AMM or PMM forspecific weight and balance information or calculate before proceeding.General information about component modification/removal necessary to install de-icing systemcomponents is provided. Check AMM for specific detail.2.3.4.CAUTION:Disconnect aircraft battery before proceeding.B.Removal of Aircraft Components1.2.3.Remove prop, and feather, if applicable, per PMM.Remove starter ring gear on aircraft so equipped; it will be replaced with slip ring/starter gearassembly.Remove engine cowling, nacelle cover, shroud, fairing, fuselage/interior panel as required.C.Modification of Aircraft Components1.Spinner bulkhead must be modified on aircraft so equipped. Using dimensions provided in AMM,lay out and drill required holes in spinner bulkhead. Lay out holes on a parallel plane to thespinner bulkhead plane of rotation, and drill perpendicular wire feed-through holes. Drill otherholes perpendicular to bulkhead surface, unless otherwise specified in AMM. Maintain tolerancesof /- .005” on decimals and /- 1/2 on radial locations when laying out and drilling holes onspinner bulkhead. In systems using a slip ring/starter ring gear assembly, the spinner adapterring may require modification. (Paragraph L3, Section II, page 27)It may be necessary to modify spinner dome by removal of material for clearance, and add rubberrestrainer straps to protect de-icer leads. Check AMM for applicability and instructions. Refer toGoodrich ATA 30-60-07 for rubber restrainer strap installation instructions. Engine cowling,shroud and baffle may require cut-outs for brush assembly installation. Check AMM for possiblemodification of other components.2.D.De-Icer Installation1.Install de-icers per Goodrich ATA 30-60-07. Refer to AMM or PMM, drawing or Goodrich PropRPL for location dimension.De-Icer Installation on Hartzell Compact Propa.Drill 9/32” diameter hole in counterweight and chamfer per Figure 4, page 6. File sharpcorners and apply zinc chromate paint to area.b.Install de-icers per Goodrich ATA 30-60-07. Slide 5/8” transflex tubing over de-icerleads. Insert de-icer wire harness through counterweight. Connect de-icer and wireharness leads, using window splice terminals (AMP 320559 or equivalent). Connectmatching leads – GND to GND, etc.2.30-60-02 SECTION II Page 5 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systemsc.d.Note:Form wires and install MS3367-1-0 tie strap in figure eight configuration as shown inFigure 5, this page. Tighten tie strap and slide tubing over coiled wires. InstallMS3367-2-0 tie straps loosely around counterweight and wire harness ¼” in from ends oftubing and assure position of tie strap buckles per Figure 6, this page & Figure 7, page7.Install .263 transflex tubing over de-icer wire harness up to counterweight then routeunder first tie strap per Figure 6, this page. Tighten both tie straps. Install terminals(AMP 32442 or equivalent) on wire harness.MS3367-1-9 & -2-9 tie straps shouldread MS3367-1-0 & -2-030-60-02 SECTION II Page 6 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsMS3367-2-0 tie strapsMS3367-0 tie strapbuckle locationE.Installation of Balance Weights1.Record number, type and location of balance weights installed on hub. Remove and saveweights and attaching parts. If balance weights are required over or under lead strap clamp, useAN960 washers for shims, trimmed to fit.It may be necessary to modify existing or install new balance weights to avoid interference withde-icer leads. Follow PMM for maximum number of balance weights, and check AMM formodification instructions.If mounting positions of balance weight and lead strap clamp coincide (Figure 8, page 8 &Figure 12, page 10), use longer screws for the extra thickness. Make sure there is threadengagement of 2-3 threads beyond nut and that screws do not bottom out or contact spinnerdome in any pitch position.2.3.30-60-02 SECTION II Page 7 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsF.Installation of Lead Strap Clamps or RestrainersCAUTION:Lead strap clamp must not squeeze leads tightly enough to cause damage, orenough tension to pull the de-icer loose. Excessive twisting of leads can result inbroken wires.A clamp or restrainer is required at the inboard end of a long lead de-icer to prevent loosening of de-icerby centrifugal force on the lead strap. Typical clamp and restrainer arrangements are shown in Figures8-18, pages 8-14. Use hardware provided in installation kit to attach clamp or restrainer through existingholes in hub. Secure de-icer or wire harness leads to clamp as shown in AMM or drawing.G.Installation of Rubber Restrainer StrapsRubber restrainer straps on a single prop must be located equidistant from hub to maintain prop balance(Figure 13, page 10 & Figure 18, page 14). Check AMM, PMM or drawing for correct dimension.30-60-02 SECTION II Page 8 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 9 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 10 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 11 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 12 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 13 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 14 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsH.Quick Disconnect System (QDS)1.The Goodrich QDS simplifies prop de-icer and wire harness installation, minimizing componentsand de-icer replacement turn time.QDS is available for HC-B3TN and HC-B4TN Hartzell Props. Table 1 , this page, shows groupsof components for which a QDS kit can be substituted.Reference Goodrich Service Newsletter 99-050 for QDS installation eligibility by prop and aircraftmodel.Reference Goodrich ATA #30-60-25 for QDS installation instructions.Reference Figures QDS1-QDS3, pages 16-18 for installation illustrations.2.3.4.5.TABLE 1 – COMPONENT GROUPS REPLACEABLE WITH QDSGroup A(3-wire normal rotating)Group B(3-wire counter E1601-53E1848-14E1889-2de-icer –orde-icer –andterminal clamp –andwire harness –orwire harnessde-icer –andterminal clamp –andwire harnessGroup C(6975-1 quick disconnect kit)Group D(2-wire normal cerwire harnesshardware kitde-icerwire harness –orwire harness30-60-02 SECTION II Page 15 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsFigure QDS1QDS installation for three wire normal rotatingprop installation (Group A, Table 1 page 15) andfor 6975-1 installation kits (Group C, Table 1,page 15)30-60-02 SECTION II Page 16 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsFigure QDS2QDS installation for three wire counter-rotating prop installation(Group B, Table 1, page 15)30-60-02 SECTION II Page 17 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsFigure QDS3QDS Installation for two-wire normal rotating prop installation(Group D, Table 1, page 15)30-60-02 SECTION II Page 18 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsI.Timer Installation1.Locate timer as specified in AMM. If not specified in AMM, check drawing for timer dimensionsand locate in appropriate available space. Timer leads must be at least 8” away from radio inputleads.Install timer per one of following methods (Figure 19, this page).a.Bulkhead – Use timer as template to locate holes for hardware and attach directly tobulkhead.b.Adjustable mounting plate – Use mounting plate as template over stringers or ribs tolocate hardware. Attach mounting plate and use timer as template to locate attachmenthardware. Attach timer to mounting plate. If mounting plate does not overlap timer casecompletely, use spacer washers between timer and plate.c.One piece mounting plate – Use mounting plate as template over stringers or ribs tolocate hardware. Attach timer to mounting plate.2.30-60-02 SECTION II Page 19 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsJ.Ammeter, Switch, Circuit Breaker InstallationCAUTION:Type and quantity of de-icers determine system current drain. Optionalcomponents such as ammeter, switch and circuit breaker, are designed to operateat that current. Only components specified for the aircraft can be used withoutaffecting de-icing system operation. Consult Goodrich Replacement Parts Listand/or AMM parts list before ordering replacement components.When optional components are specified, locate per FAA Part 23, Section 23.1321, and followingguidelines. Check AMM or drawing for dimensions and terminal size of optional components.1.2.Install ammeter in instrument panel. If an external shunt is used, install with 6” or shorter wirelength between ammeter and shunt . Install switch and ammeter near each other. If warningplacard required, install adjacent to switch in full view of pilot or as specified in AMM.Check AMM for circuit breaker mounting location.K.Brush Assembly Mounting Bracket InstallationRemove engine hardware and attach brush assembly mounting bracket using hardware provided.(Figures 20-24, pages 21-23) Remainder of brush assembly is installed after slip ring installation.30-60-02 SECTION II Page 20 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 21 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 22 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 23 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsL.Slip Ring Installation1.Install connecting hardware provided, usually terminal strip block, on modified spinner bulkhead.Figures 25-28, pages 24-25 show typical connections. Assure de-icer or wire harness leads aresecurely clamped. When directed by AMM, install rivnuts or grommets before installing terminalstrip or block.30-60-02 SECTION II Page 24 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 25 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems2.Slip Ring Assembly Installationa.Install slip ring assembly as specified in AMM per one of two installation methods below.i.ii.b.Feed slip ring leads through holes drilled in spinner bulkhead during modificationprocedure. (Paragraph C1, Section II, page 5) If specified in AMM, installrubber grommets. Secure slip ring assembly to bulkhead with appropriatehardware. Hand ream mounting holes for satisfactory alignment. Torque boltsfor snug fit. (Figure 29, this page)Position slip ring assembly on crankshaft or prop hub flange as specified in AMM(Figures 30 & 31, page 27).Slip Ring Assembly Wiringi.ii.Connect slip ring leads as specified in AMM, either directly to terminal strips,blocks or studs, or using slip ring wire harness.Connect de-icer or wire harness leads to terminal strips, blocks or studs, andhold in place with lead clips as specified in AMM. Leave no slack in de-icer orwire harness leads between terminals and clips, and secure leads as specified inAMM. Do not twist leads more than 180 when aligning.30-60-02 SECTION II Page 26 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems3.Slip Ring/Starter Ring Gear Assembly Installation (Figure 32, page 28)CAUTION:a.b.c.Before filing spinner adapter ring make sure spinner adapter ring is properlyaligned on slip ring/starter ring gear assembly by matching location of spinnerattaching nuts on spinner adapter ring flange.If there is a spinner adapter ring, remove it from original starter ring gear and positionover slip ring/starter ring gear assembly as it will be mounted.If slip ring is installed outside starter ring gear pulley, file spinner adapter ring as requiredfor a minimum 1/16” clearance between spinner adapter ring and slip ring terminals,making sure filed clearance areas have smooth and flowing radii. (Figure 33, page 29)If slip ring is installed inside pulley on starter ring gear, there should be no interferencebetween adapter ring and starter ring gear. Attach adapter ring to slip ring/starter ring30-60-02 SECTION II Page 27 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systemsd.e.Note:gear assembly with original bolts and finger tighten. (Bolts will be torqued later.) Installslip ring/starter ring gear assembly on crankshaft.If there is no adapter ring, there is a hub extension, and the slip ring/starter ring gearassembly is installed between the crankshaft flange and hub extension (Figure 34, page29). Secure hub extension and install prop per PMM or AMM.Slip Ring/Starter Ring Gear Assembly WiringBe sure to connect matching leads or matching studs and leads: GND to GND, etc. Do not twistde-icer or wire harness leads more than 180 when aligning to terminals. Secure de-icer or wireharness leads with lead clips, and install cushions (Figure 7, page 7 & Figure 32, this page),when specified in AMM. Leave no slack in leads between terminals and clips.i.ii.With a spinner adapter ring, de-icer or wire harness, leads connect to integralterminal studs (Figure 32, this page & Figure 33, page 29) or attached terminalstrips/blocks on slip ring/starter ring gear assembly, using adapter ringattachment bolts (Figures 25 & 26, page 24). With terminal strips/blocks, slip ring/starter ring gear assembly leads and deicer or wire harness leads both connect to strips/blocks. With integral terminal studs, de-icer or wire harness leads only connect tostuds using 10-12 inch-lbs. Torque to tighten nuts.If terminal strips, clips or other hardware are installed using same bolts thatattach adapter ring to slip ring/starter ring gear assembly, make sure there is 2-3thread engagement beyond nut. On aircraft with spinner bulkhead(s), a slip ringwire harness is installed on the slip ring/starter ring gear assembly terminalstuds, connects to de-icer or wire harness leads, is routed across hub extension,and connects to terminal strips or studs on modified spinner bulkhead (Figure33, page 29).30-60-02 SECTION II Page 28 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems30-60-02 SECTION II Page 29 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing Systems4.Hose ClampsIf there is a hub extension with slip ring or wire harness leads routed along the hub, hose clamps may beused to hold wiring against hub (Figure 34, page 29). If so, drill cap guards on hose clamps with No. 56drill as shown in Figure 35, this page. Drill both sides of cap guards in line with and near screw slotbase. Position clamps, spacers and cushions as applicable per AMM. Position worm screw housings180 opposite each other on hub extension. Do not place wire harness in tension when tighteningclamps. Torque worm screws to 35-55 inch-lbs. And safety wire.5.Slip Ring Run-out (Alignment)a.b.CAUTION:c.After installation, check slip ring alignment by attaching a dial indicator gauge to theengine and placing the pointer on the copper ring (Figure 36, page 31). Grasp propblade and rotate slowly, noting deviations of ring from true plane. Exert uniform push orpull on prop to make sure run-out reading is accurate. Total run-out reading must notexceed .0050” ( 0025”) for piston engines, or .0080” ( 0040”) for turbine engines.Additionally, run-out reading must not exceed .0020” within any 4” arc of slip ring travelfor either engine type.If slip ring/starter ring gear assembly is used, or if slip ring assembly is mounted betweencrankshaft flange and prop hub, and run-out reading is unacceptable, check for dirt onring gear mounting surfaces or slip ring holder and clean as required. If run-out readingis still unacceptable, return slip ring to Goodrich (through point of purchase) forevaluation.Torque adjustment/shim procedures cannot be used for slip rings mountedbetween crankshaft flange and prop hub.If slip ring is mounted on spinner bulkhead, and run-out reading is unacceptable, varytorque on attachment bolts within limits specified by PMM or AMM, or within standardlimits for bolts used. Most slip ring installations include a compression washerarrangement that allows proper ring adjustment by varying torque applied to attachinghardware (Figure 29, page 26).30-60-02 SECTION II Page 30 of 49Mar 20/02

Goodrich De-Icing & Specialty SystemsUniontown, OhioInstallation & Maintenance Manual for Electrothermal Prop De-Icing SystemsFigure 36 – Checking Slip Ring Run-outM.Propeller Assembly InstallationInstall spinner bulkhead and prop per PMM or AMM.N.Brush Assembly Installation1.Position brush assembly on mount

Installation & Maintenance Manual for Electrothermal Prop De-Icing Systems 30-60-02 Page Intro 1 of 1 Mar 20/02 INTRODUCTION A. General 1. This manual supersedes Goodrich Reports 68-04-712 and 70-04-700 2. This manual provides installation, maintenance and repair information for Goodrich electrothermal

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