hartzell propeller inc. one propeller place piqua, ohio 45356...

HARTZELL PROPELLER INC.One Propeller PlacePiqua, Ohio 45356-2634 U.S.A.Telephone: 937.778.4200Fax: 937.778.4391

MANUAL REVISION TRANSMITTALManual 169 (61-00-69)

Propeller Owner's Manual and Logbook

REVISION 3 dated May 2014

Attached is a copy of Revision 3 to Hartzell Manual 169.

Page Control Chart for Revision 3:

Remove Insert Page No. Page No.COVER/INSIDE COVER COVER/INSIDE COVER

REVISIONS HIGHLIGHTS REVISIONS HIGHLIGHTS pages 5 thru 8 pages 5 thru 8

LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES pages 17 thru 20 pages 17 and 18

TABLE OF CONTENTS TABLE OF CONTENTS pages 21 thru 32 pages 19 thru 30

INTRODUCTION INTRODUCTION pages 1-1 thu 1-14 pages 1-1 thru 1-16 INSTALLATION AND REMOVAL INSTALLATION AND REMOVAL pages 3-1 thru 3-126 pages 3-1 thru 3-132

TESTING AND TESTING AND TROUBLESHOOTING TROUBLESHOOTING pages 4-1 thru 4-16 pages 4-1 thru 4-16

INSPECTION AND CHECK INSPECTION AND CHECK pages 5-3 thru 5-16 pages 5-3 thru 5-16 pages 5-19 thru 5-24 pages 5-19 thru 5-24

continued on next page

Page Control Chart for Revision 3 (continued):

Remove Insert Page No. Page No.

NOTE 1: When the manual revision has been inserted in the manual, record the information required on the Record of Revisions page in this manual.

NOTE 2: Pages distributed in this revision may include pages from previous revisions if they are on the opposite side of revised pages. This is done as a convenience to those users who wish to print a two-sided copy of the new revision.

MAINTENANCE PRACTICES MAINTENANCE PRACTICES pages 6-1 and 6-32 pages 6-1 and 6-28

Propeller Owner's Manual and Logbook

Hartzell Propeller Inc.One Propeller PlacePiqua, OH 45356 - 2634 U.S.A.Ph: 937 - 778 - 4200 (Hartzell Propeller Inc)Ph: 937 - 778 - 4379 (Product Support)937-778-4391 (Product Support Fax)

Steel Hub Reciprocating Propellers with Aluminum Blades

Two Blade Three Blade

HC-93Z20-1( )HC-93ZF-2( )HC-93Z20-2( )HC-93Z30-2( )

(B)HC-92( )F-1( )HC-92( )K-1( )(B)HC-92( )F-2( )HC-92( )K-2( )(B)HC-92( )F-3( )HC-92WF-5AHC-92( )F-8( )HC-92( )K-8( )

Manual No. 169 61-00-69Revision 3May 2014

Inside Cover Rev. 3 May/14

Propeller Owner's Manual169

61-00-69COVER

© 2000, 2005, 2009, 2014 - Hartzell Propeller Inc. - All rights reserved

Propeller Owner's Manual 169

61-00-69 REVISION HIGHLIGHTSPage 5

Rev. 3 May/14

REVISION 3 HIGHLIGHTS• COVER • Revised to match this manual revision• REVISION HIGHLIGHTS • Revised to match this manual revision• LIST OF EFFECTIVE PAGES • Revised to match this manual revision• TABLE OF CONTENTS • Revised to match this manual revision• INTODUCTION • Added a statement that the manual is accepted by the FAA. • Changed "Hartzell" to "Hartzell Propeller Inc." • Added the section "Inspection, Repair, and Overhaul" • Added the section "Safe Handling of Paints and Chemicals" • Added the section "Propeller Critical Parts" • Revised the section "Reference Publications" • Revised the section "Definitions" • Revised the section "Abbreviations" • Other minor formatting changes

• INSTALLATION AND REMOVAL • Changed "Hartzell" to "Hartzell Propeller Inc." • Added option for safety cable for mounting hardware • Revised Table 3-1, O-ring and Propeller Mounting Hardware

Identification • Revised the section "Pre-Installations" • Added Cautions about "Propeller Critical Parts" • Added Warnings about "Adhesives and solvents" • Revised the torque value for the governor mounting nuts • Revised the installation of the felt seal instruction in section

"Installing the 20 Spline HC-93Z20-1( ) Propeller Models" and section "Installing the 20 Spline HC-93Z20-2( ) Propeller Models"

• Other minor formatting changes

61-00-69 REVISION HIGHLIGHTS


Page 6 Rev. 3 May/14

TESTING AND TROUBLESHOOTING • Added Cautions about "Propeller Critical Parts" • Added wording for "a certified propeller repair station with the

appropriate rating" • Other minor formatting changes

INSPECTION AND CHECK • Added Cautions about "Propeller Critical Parts" • Revised the section "Pre-Flight Checks" • Added wording for "a certified propeller repair station with the

appropriate rating" • Other minor formatting changes

MAINTENANCE PRACTICES • Added Cautions about "Propeller Critical Parts" • Changed "Hartzell" to "Hartzell Propeller Inc." • Revised the section "Blade Repairs" • Added Warning about "Blade Repairs" • Revised Caution about shotpeened blades • Added wording for "a certified propeller repair station with the

appropriate rating" • Revised the section "Painting After Repair" • Other minor formatting changes

REVISION 3 HIGHLIGHTS


61-00-69 REVISION HIGHLIGHTSPage 7

Rev. 3 May/14

REVISION HIGHLIGHTS

1. IntroductionA. General

This is a list of current revisions that have been issued against this manual. Please compare it to the RECORD OF REVISIONS page to ensure that all revisions have been added to the manual.

B. Components(1) Revision No. indicates the revisions incorporated in this

manual.(2) Issue Date is the date of the revision.(3) Comments indicates the level of the revision.

(a) New Issue is a new manual distribution. The manual is distributed in its entirety. All the page revision dates are the same and no change bars are used.

(b) Reissue is a revision to an existing manual that includes major content and/or major format changes. The manual is distributed in its entirety. All the page revision dates are the same and no change bars are used.

(c) Major Revision is a revision to an existing manual that includes major content or minor content changes over a large portion of the manual. The manual is distributed in its entirety. All the page revision dates are the same, but change bars are used to indicate the changes incorporated in the latest revision of the manual.

(d) Minor Revision is a revision to an existing manual that includes minor content changes to the manual. Only the revised pages of the manual are distributed. Each page retains the date and the change bars associated with the last revision to that page.

61-00-69 REVISION HIGHLIGHTS


Page 8 Rev. 3 May/14

Revision No. Issue Date Comments Original July/00 New Issue Revision 1 Aug/05 Minor Revision Revision 2 May/09 Minor Revision Revision 3 May/14 Minor Revision

Rev. 3 May/14


61-00-69 LIST OF EFFECTIVE PAGES

Cover Cover/Back Cover Rev. 3 May/14

Message 1 thru 4 Original July/00

Revision Highlights 5 thru 8 Rev. 3 May/14

Record of Revisions 9 and 10 Original July/00

Record of Temporary Revisions 11 and 12 Original July/00

Service Documents List 13 and 14 Rev. 1 Aug/05

Airworthiness Limitations 15 and 16 Rev. 2 May/09

List of Effective Pages 17 and 18 Rev. 3 May/14

Table of Contents 19 thru 30 Rev. 3 May/14

Introduction 1-1 thru 1-16 Rev. 3 May/14

Description and Operation 2-1 thru 2-6 Original July/00

Description and Operation 2-7 Rev. 1 Aug/05




Description and Operation 2-16 thru 2-19 Rev. 1 Aug/05

Description and Operation 2-20 Original July/00



Description and Operation 2-26 thru 2-30 Rev. 1 Aug/05

Description and Operation 2-31 and 2-32 Original July/00



Installation and Removal 3-1 thru 3-132 Rev. 3 May/14

Testing and Troubleshooting 4-1 thru 4-16 Rev. 3 May/14

Inspection and Check 5-1 thru 5-2 Rev. 2 May/09

LIST OF EFFECTIVE PAGES

Chapter Page Revision Date

Rev. 3 May/14 61-00-69 LIST OF EFFECTIVE PAGES



Inspection and Check 5-9 Rev. 2 May/09



Inspection and Check 5-15 and 5-16 Rev. 3 May/14





Maintenance Practices 6-1 and 6-28 Rev. 3 May/14

Anti-ice and De-ice Systems 7-1 and 7-2 Rev. 2 May/09

Anti-ice and De-ice Systems 7-3 and 7-4 Rev. 1 Aug/05

Anti-ice and De-ice Systems 7-5 thru 7-8 Rev. 2 May/09

Records 8-1 thru 8-4 Original July/00

LIST OF EFFECTIVE PAGES

Chapter Page Revision Date

Rev. 3 May/14


61-00-69 TABLE OF CONTENTS

REVISION HIGHLIGHTS ............................................................... 5

RECORD OF REVISIONS ............................................................. 9

RECORD OF TEMPORARY REVISIONS .....................................11

SERVICE DOCUMENTS LIST ..................................................... 13

AIRWORTHINESS LIMITATIONS ................................................ 15

LIST OF EFFECTIVE PAGES ...................................................... 17

TABLE OF CONTENTS ................................................................ 19

INTRODUCTION ......................................................................... 1-1

1. Purpose .................................................................................. 1-3

2. Airworthiness Limits ................................................................ 1-3

3. AirframeorEngineModifications ............................................ 1-3

4.RestrictionsandPlacards ....................................................... 1-4

5. General ................................................................................... 1-4A.PersonnelRequirements ................................................... 1-4B.MaintenancePractices ....................................................... 1-5C. Continued Airworthiness .................................................... 1-7D.PropellerCriticalParts ....................................................... 1-7

6. ReferencePublications ........................................................... 1-8

7. Definitions ............................................................................... 1-9

8. Abbreviations ........................................................................ 1-13

9. HartzellProductSupport ...................................................... 1-14

10.WarrantyService .................................................................. 1-14

11.HartzellRecommendedFacilities ......................................... 1-15

DESCRIPTION AND OPERATION .............................................. 2-1

1. DescriptionofPropellerandSystems .................................... 2-3A.ConstantSpeed,Non-counterweighted, Non-FeatheringPropellers ................................................. 2-7B. Constant Speed, Counterweighted, Non-feathering Propellers ......................................................................... 2-11

TABLE OF CONTENTS Page

Rev. 3 May/14 61-00-69 TABLE OF CONTENTS


C.ConstantSpeed,FeatheringPropellers ........................... 2-17D. Constant Speed, Feathering and Reversing Propellers(ExternalBetaSystem) ................................... 2-21E.ConstantSpeed,FeatheringandReversingPropellers ... 2-27

2. ModelDesignation ................................................................ 2-32A.SteelHubPropellerModelIdentification .......................... 2-32B.AluminumBladeModelIdentification ............................... 2-33

3. Governors ............................................................................. 2-35A. Theory of Operation ......................................................... 2-35B. Governor Types ............................................................... 2-38C.IdentificationofHartzellGovernors .................................. 2-38

4. PropellerAnti-IceandDe-IceSystems ................................. 2-39A.PropellerAnti-IceSystem ................................................. 2-39B.PropellerDe-IceSystem .................................................. 2-40

INSTALLATION AND REMOVAL ................................................ 3-1

1. Tools,Consumables,andExpendables ................................. 3-5A.Tooling ................................................................................ 3-5B.Consumables ..................................................................... 3-5C.Expendables ...................................................................... 3-5

2. O-ringandPropellerMountingHardwareIdentification .......... 3-6

3. Pre-Installation ...................................................................... 3-10A.InspectionofShippingPackage ....................................... 3-10B.Uncrating .......................................................................... 3-10C.InspectionafterShipment ................................................ 3-10D.ReassemblyofaPropellerDisassembledforShipment .. 3-10

4. PropellerAssemblyInstallation ............................................. 3-11A.Precautions ...................................................................... 3-11B.O-ringandPropellerMountingHardwareIdentification ... 3-12C.InstallingtheFFlangePropellerModels BHC-92()F-1D1 ............................................................... 3-14


Rev. 3 May/14



D.InstallingtheFFlangePropellerModels HC-92()F-8() .................................................................. 3-22E.InstallingtheKFlangePropellerModels HC-92()K-1D,andHC-92()K-8() ................................... 3-28F. InstallingtheFFlangePropellerModels HC-92ZF-2()andHC-93ZF-2() ..................................... 3-34G.InstallingtheKFlangePropeller ModelsHC-92()K-2() ...................................................... 3-40H.InstallingtheFFlangePropellerModels (B)HC-92()F-3 ................................................................. 3-45I. InstallingtheFFlangePropellerModels BHC-92(W,Z)F-3(L)G ...................................................... 3-57J. InstallingtheFFlangePropellerModel HC-92WF-5A ................................................................... 3-65K.Installingthe20SplineHC-93Z20-1()PropellerModels 3-74L. Installingthe20SplineHC-93Z20-2()andthe30Spline HC-93Z30-2()PropellerModels ...................................... 3-81

5. Post-InstallationChecks ....................................................... 3-96

6. PropellerAssemblyRemoval ................................................ 3-97A.RemovingtheFFlangePropellerModels BHC-92()F-1D1 ............................................................... 3-97B.RemovingtheFFlangePropellerModels HC-92()F-8() .................................................................. 3-99C.RemovingtheKFlangePropellerModels HC-92()K-1D,andHC-92()K-8() ................................. 3-102D.RemovingtheFFlangePropellerModels HC-92ZF-2()andHC-93ZF-2() .................................... 3-105E.RemovingtheKFlangePropellerModels HC-92()K-2() ................................................................ 3-108F. RemovingtheFFlangePropellerModels (B)HC-92()F-3 ............................................................... 3-112G.RemovingtheFFlangePropellerModels BHC-92(W,Z)F-3(L)G ..................................................... 3-115H.RemovingtheFFlangePropellerModel HC-92WF-5A .................................................................. 3-120




I. Removingthe20SplinePropellerModels HC-93Z20-1() ............................................................... 3-125J. Removingthe20SplineHC-93Z20-2()andthe 30SplineHC-93Z30-2()PropellerModels .................. 3-128

TESTING AND TROUBLESHOOTING ....................................... 4-1

1. OperationalTests .................................................................... 4-3A.InitialRun-Up ..................................................................... 4-3B.StaticRPMCheck .............................................................. 4-4C.Post-RunCheck ................................................................. 4-4

2. PropellerIceProtectionSystems ........................................... 4-4A.ElectricDe-iceSystem ....................................................... 4-4B.Anti-iceSystem .................................................................. 4-5

3. Troubleshooting ..................................................................... 4-5A.IncorrectMaximumRPM(onGround) ............................... 4-5B. Hunting and Surging .......................................................... 4-6C. Engine Speed Varies with Airspeed ................................... 4-7D.LossofPropellerControl- HC-92()()-8()PropellerModels: ...................................... 4-9E.LossofPropellerControl-(B)HC-92()F-1(), HC-92()K-1(),HC-93Z20-1(),HC-92()()-2(), HC-93()()-2(),(B)HC-92()F-3(),and HC-92WF-5APropellerModels: ......................................... 4-9F. FailuretoFeatherorFeathersSlowly-HC-92()()-2(), HC-93()()-2(),andHC-92WF-5APropellerModels: ...... 4-10G.FailuretoUnfeather-HC-92()()-2(), HC-93()()-2(),andHC-92WF-5APropellerModels. ...... 4-10H.StartLocks(Anti-FeatherLatches)FailtoEngageon Shutdown-HC-9()()-2()()and HC-92WF-5APropellers: ................................................. 4-11I. Vibration ........................................................................... 4-12J. PropellerOverspeed ........................................................ 4-13


Rev. 3 May/14



K.PropellerUnderspeed ...................................................... 4-13L. OilorGreaseLeakage ..................................................... 4-14

INSPECTIONANDCHECK ......................................................... 5-1

1. Pre-FlightChecks ................................................................... 5-3

2. OperationalChecks ................................................................ 5-5

3. RequiredPeriodicInspectionsandMaintenance ................... 5-6A.PeriodicInspection ............................................................. 5-6B.PeriodicMaintenance ........................................................ 5-7C. Airworthiness Limitations ................................................... 5-7D.OverhaulPeriods ............................................................... 5-8

4. InspectionProcedures .......................................................... 5-10A.BladeDamage ................................................................. 5-10B.GreaseorOilLeakage ..................................................... 5-10C.Vibration ........................................................................... 5-12D.TachometerInspection ..................................................... 5-13E.BladeTrack ...................................................................... 5-15F. LooseBlades ................................................................... 5-15G. Corrosion ......................................................................... 5-16H. Spinner Damage .............................................................. 5-16I. ElectricDe-iceSystem ..................................................... 5-16J. Anti-iceSystem ................................................................ 5-16

5. SpecialInspections ............................................................... 5-19A. Overspeed ...................................................................... 5-19B.LightningStrike ................................................................ 5-20C.ForeignObjectStrike/GroundStrike ................................ 5-22D. Fire Damage or Heat Damage ......................................... 5-24

6. Long Term Storage ............................................................... 5-24




MAINTENANCE PRACTICES ..................................................... 6-1

1. Cleaning ................................................................................. 6-3A.GeneralCleaning ............................................................... 6-3B.SpinnerCleaningandPolishing ......................................... 6-3

2. Lubrication .............................................................................. 6-5A.LubricationIntervals ........................................................... 6-5B.LubricationProcedure ........................................................ 6-6C.ApprovedLubricants .......................................................... 6-9

3. CarbonBlockAssemblies ..................................................... 6-10A.Inspection ......................................................................... 6-10B.ReplacementofA-3026CarbonBlockUnitinthe A-3044CarbonBlockAssembly ...................................... 6-10C.InstallationoftheA-3044CarbonBlockAssembly .......... 6-11

4. BladeRepairs ....................................................................... 6-13A.RepairofNicksorGouges ............................................... 6-13B. RepairofBentBlades ...................................................... 6-15

5. Painting After Repair ............................................................. 6-16A.General ............................................................................ 6-16B.PaintingofAluminumBlades ........................................... 6-17

6. DynamicBalance .................................................................. 6-19A. Overview .......................................................................... 6-19B.InspectionProceduresBeforeBalancing ......................... 6-20C.PlacementofBalanceWeightsforDynamicBalance ...... 6-21

7. PropellerLowPitchSetting .................................................. 6-23A.LowPitchStop-AllPropellerModels ............................. 6-23B.Lowpitchmeasurementonpropellermodels HC-9()()()-2()(): ........................................................... 6-24C.Lowpitchmeasurementonpropellermodels (B)HC-9()()()-1()()andHC-92()()-8(): ....................... 6-24D.Lowpitchmeasurementonpropellermodels HC-92()()-3()andHC-92WF-5A. ..................................... 6-25


Rev. 3 May/14



E.AdjustingLowPitchAngle-PropellerModels BHC-92()f-3()()andHC-92WF-5A ............................... 6-25

8. HighPitch(MinimumRPM)Stop-Propellermodels HC-9()()()-1()()(),HC-92()()-3()(),and HC-92()()-8() ...................................................................... 6-28

9. FeatheringPitchStopAdjustment-PropellerModels HC-9()()-2()()andHC-92WF-5A ....................................... 6-28

10.StartLockAdjustment-Propellermodels HC-9()()-2()()andHC-92WF-5A ....................................... 6-28

11.PropellerIceProtectionSystems ......................................... 6-28

ANTI-ICE AND DE-ICE SYSTEMS ............................................. 7-1

1. Introduction ............................................................................. 7-3A.PropellerDe-iceSystem .................................................... 7-3B.PropellerAnti-iceSystem ................................................... 7-3

2. SystemDescription ................................................................. 7-4A.De-iceSystem .................................................................... 7-4B.Anti-iceSystem .................................................................. 7-5

3. De-iceSystemFunctionalTests ............................................. 7-5

4.Anti-iceSystemFunctionalTests ............................................ 7-5

5. De-iceandAnti-iceSystemInspections ................................. 7-6A.De-iceSystemInspections ................................................ 7-6B.Anti-iceSystemInspections ............................................... 7-6

6. De-iceandAnti-iceSystemTroubleshooting .......................... 7-6A.De-iceSystemTroubleshooting ......................................... 7-6B.Anti-iceSystemTroubleshooting ....................................... 7-7

RECORDS .................................................................................. 8-1

1. Introduction ............................................................................. 8-3

2. RecordKeeping ...................................................................... 8-3A. InformationtobeRecorded ................................................ 8-3




SteelHubUnit(ForSplinedShaft Mounting) ..................................................Figure 2-1 ............. 2-3

SplineShaftAttachment ................................Figure 2-2 ............. 2-4

FlangedAttachment.......................................Figure 2-3 ............. 2-5

ConstantSpeed,Nonfeathering,Non-counterweighted PropellerAssembly ....................................Figure 2-4 ............. 2-6

Constant Speed, Nonfeathering, Counterweighted PropellerAssembly ....................................Figure 2-5 ........... 2-10

ConstantSpeed,FeatheringPropellerAssembly (FlangedAttachment,ShortPiston) ..........Figure 2-6 ........... 2-14

ConstantSpeed,FeatheringPropellerAssembly (SplinedAttachment,ShortPiston) ...........Figure 2-7 ........... 2-15

ConstantSpeed,FeatheringPropellerAssembly (SplinedAttachment,LongPiston) ............Figure 2-8 ........... 2-16

Constant Speed, Feathering, and Reversing PropellerAssembly ....................................Figure 2-9 ........... 2-20

FundamentalElementsofaReversing System ......................................................Figure 2-10 ......... 2-22

ConstantSpeed,FeatheringandReversingPropeller Assembly(ExternalBetaSystem) .............Figure 2-11 ......... 2-26

Governor in Onspeed Condition ....................Figure 2-12 ......... 2-34

Governor in Underspeed Condition ...............Figure 2-13 ......... 2-34

Governor in Overspeed Condition .................Figure 2-14 ......... 2-34

Feathering Governor .....................................Figure 2-15 ......... 2-36

Synchronizer/Synchrophaser Governor ...................................................Figure 2-16 ......... 2-36

BHC-92()F-1D1PropellerAssembly.............Figure 3-1 ........... 3-13

InstallingFFlangePropelleronthe EngineFlange ...........................................Figure 3-2 ........... 3-15

LIST OF FIGURES Page

Rev. 3 May/14



DeterminingTorqueValueWhenUsing TorquingAdapter .......................................Figure 3-3 ........... 3-16

HC-92()()-1D,-8()Propeller Assembly ...................................................Figure 3-4 ........... 3-21

KFlangeInstallationon-1Propeller Models .......................................................Figure 3-5 ........... 3-25

InstallingKFlangePropelleronthe EngineFlange ...........................................Figure 3-6 ........... 3-27

HC-92ZF-2(),HC-92()K-2() PropellerAssembly ....................................Figure 3-7 ........... 3-32

HC-93ZF-2()PropellerAssembly .................Figure 3-8 ........... 3-33

KFlangeInstallationon-2Propeller Models .......................................................Figure 3-9 ........... 3-39

(B)HC-92()F-3PropellerAssembly ..............Figure 3-10 ......... 3-46

ToolforDecompressingExternal Beta System ..............................................Figure 3-11 ......... 3-47

HC-92WF-3InstallationonTSIO-520-C Engine .......................................................Figure 3-12 ......... 3-47

InstallationofBetaValve,Governor, andLinkage ...............................................Figure 3-13 ......... 3-49

CarbonBlockandBetaRing Clearance ..................................................Figure 3-14 ......... 3-50

CarbonBlockAssembly.................................Figure 3-15 ......... 3-50

AdjustingPropellerReverseControl System ......................................................Figure 3-16 ......... 3-53

BHC-92(W,Z)F-3(L)GPropeller Assembly ...................................................Figure 3-17 ......... 3-59

BHC-92(W,Z)F-3(L)GInstallation ..................Figure 3-18 ......... 3-60

HC-92WF-5APropellerAssembly ................Figure 3-19 ......... 3-66

HC-92WF-5AInstallation ...............................Figure 3-20 ......... 3-68




HC-93Z20-1()PropellerAssembly................Figure 3-21 ......... 3-76

InstallingPistonO-ringandFelt DustSeal ...................................................Figure 3-22 ......... 3-78

HC-93Z20-2A(1),-2B,-2C,-2D1 PropellerAssembly ....................................Figure 3-23 ......... 3-83

HC-93Z20-2C1PropellerAssembly ..............Figure 3-24 ......... 3-84

HC-93Z30-2EPropellerAssembly.................Figure 3-25 ......... 3-85

Piston-to-LinkArmAttachmentDetails ..........Figure 3-26 ......... 3-87

SpringAssembly-to-Cylinder AttachmentDetails ....................................Figure 3-27 ......... 3-89

FeatheringSpringAssembly..........................Figure 3-28 ......... 3-90

RearHubMountingPartson30-Spline ShaftPropeller ...........................................Figure 3-29 ......... 3-91

SafetyingtheShaftNutonaSplined ShaftPropeller ...........................................Figure 3-30 ......... 3-93

Reversing(Beta)Systemand Governing Hardware .................................Figure 3-31 ...... 3-117

DisconnectingtheBetaRing .........................Figure 3-32 ....... 3-123

CheckingBladeTrack....................................Figure 5-1 ........... 5-14

BladePlay .....................................................Figure 5-2 ........... 5-14

ReciprocatingEngineOverspeedLimits .......Figure 5-3 ........... 5-18

LubricationFitting ..........................................Figure 6-1 ............. 6-4

LubricationLabel ...........................................Figure 6-2 ............. 6-6

Repair Limitations ..........................................Figure 6-3 ........... 6-12

LocationofBalanceWeights .........................Figure 6-4 ........... 6-22

AdjustingLowPitchAngle .............................Figure 6-5 ........... 6-26


Rev. 3 May/14



O-ringandPropellerMountingHardware Identification ....................................Table3-1 ..................... 3-6

TorqueValuesTable ...............................Table3-2 ................... 3-17

Approved Paints .....................................Table6-1 ................... 6-19

LIST OF TABLES Page



(Thispageisintentionallyblank.)

INTRODUCTION 61-00-69Page 1-1

Rev. 3 May/14

Propeller Owner’s Manual169

INTRODUCTION - CONTENTS

1. Purpose ................................................................................. 1-3

2. Airworthiness Limits .............................................................. 1-3

3. AirframeorEngineModifications .......................................... 1-3

4. RestrictionsandPlacards ..................................................... 1-4

5. General ................................................................................. 1-4A.PersonnelRequirements ................................................... 1-4B.MaintenancePractices ....................................................... 1-5C. Continued Airworthiness .................................................... 1-7D.PropellerCriticalParts ....................................................... 1-7

6. ReferencePublications ......................................................... 1-8

7. Definitions ............................................................................. 1-9

8. Abbreviations ...................................................................... 1-13

9. HartzellPropellerInc.ProductSupport ............................... 1-14

10.WarrantyService ................................................................. 1-14

11. HartzellPropellerInc.RecommendedFacilities ................. 1-15


Rev. 3 May/14




Rev. 3 May/14


1. PurposeA. ThismanualhasbeenreviewedandacceptedbytheFAA.

Additionally,theAirworthinessLimitationsSectionofthismanualhasbeenapprovedbytheFAA.

CAUTION: KEEPTHISMANUALWITHTHEPROPELLER,ORWITHTHEAIRCRAFTONWHICHITISINSTALLED,ATALLTIMES.THELOGBOOKRECORD WITHIN THIS MANUAL MUST BE MAINTAINED,RETAINEDCONCURRENTLY,ANDBECOMEAPARTOFTHEAIRCRAFTANDENGINE SERVICE RECORDS.

B. Thismanualsupportsthefollowingtwoandthree-bladed,“9”typesteelhubreciprocatingpropellers:constantspeed,nonfeathering;constantspeed,feathering;andconstantspeed,feathering,andreversing.

C. Thepurposeofthismanualistoenablequalifiedpersonneltoinstall,operate,andmaintainaHartzellPropellerInc.propeller.Separatemanualsareavailableconcerningoverhaulproceduresandspecificationsforthepropeller.

D. Thismanualcoversdifferentdesigntypes.SamplehubandblademodelnumberswithineachdesignarecoveredintheDescriptionandOperationchapterofthismanual.NOTE: Allpropellermodelscoveredbythismanualuse

aluminumpropellerblades.

2. Airworthiness LimitsA. RefertotheAirworthinessLimitationssectionofthismanual

for Airworthiness Limits information.

3. AirframeorEngineModificationsA. Propellersareapprovedvibrationallyonairframeandengine

combinationsbasedontestsoranalysisofsimilarinstallations.Thisdatahasdemonstratedthatpropellerstresslevelsareaffectedbyairframeconfiguration,airspeed,weight,power,engineconfiguration,andflightmaneuvers.Aircraftmodificationsthatcaneffectpropellerstressinclude,butarenotlimitedto:aerodynamicchangesaheadoforbehindthepropeller,realignmentofthethrustaxis,increasingordecreasingairspeedlimits,increasingordecreasingweightlimits(lesssignificantonpistonengines),andtheadditionofapprovedflightmaneuvers(utilityandaerobatic).


Rev. 3 May/14


B. Enginemodificationscanalsoaffectthepropeller.Thetwoprimarycategoriesofenginemodificationsarethosethataffectstructureandthosethataffectpower.Anexampleofastructuralenginemodificationisthealterationofthecrankshaftordamperofapistonengine.Anychangetotheweight,stiffnessortuningofrotatingcomponentscouldresultinapotentiallydangerousresonantconditionthatisnotdetectablebythepilot.Mostcommonenginemodificationsaffectthepowerduringsomephaseofoperation.Someincreasethemaximumpoweroutput,whileothersimprovethepoweravailableduringhotandhighoperation(flatrating)oratoff-peakconditions.Examplesofsuchenginemodificationsinclude,butarenotlimitedto:changestothecompressor,powerturbine,orhotsectionofaturbopropengine;andonpistonengines,theadditionoralterationofaturbochargerorturbonormalizer,increasedcompressionratio,increasedRPM,alteredignitiontiming,electronicignition,fullauthoritydigitalelectroniccontrols(FADEC),ortunedinductionorexhaust.

C. Allsuchmodificationsmustbereviewedandapprovedbythepropellermanufacturerbeforeobtainingapprovalontheaircraft.

4. RestrictionsandPlacardsA. Thepropellerscoveredbythismanualmayhavea

restrictedoperatingrangethatrequiresacockpitplacard.Therestrictions,ifpresent,willvarydependingonthepropeller,blade,engine,and/oraircraftmodel.Reviewthepropellerandaircrafttypecertificatedatasheet(TCDS),PilotOperatingHandbook(POH),andanyapplicableAirworthinessDirectivesforspecificinformation.

5. GeneralA. PersonnelRequirements

(1) Inspection,Repair,andOverhaul(a)Compliancetotheapplicableregulatoryrequirements

establishedbytheFederalAviationAdministration(FAA)orforeignequivalentismandatoryforanyoneperformingoracceptingresponsibilityforanyinspectionand/orrepairand/oroverhaulofanyHartzellPropellerInc.product.


Rev. 3 May/14


(b) Personnelperformingmaintenanceonsteelhubpropellersareexpectedtohavesufficienttrainingandcertifications(whenrequiredbytheapplicableAviationAuthority)toaccomplishtheworkrequiredinasafeand airworthy manner.

B. MaintenancePractices(1) Thepropelleranditscomponentsarehighlyvulnerable

todamagewhiletheyareremovedfromtheengine.Properlyprotectallcomponentsuntiltheyarereinstalledon the engine.

(2) Neverattempttomovetheaircraftbypullingonthepropeller.

(3) Avoidtheuseofbladepaddles,ifpossible.Donotplacethebladepaddleintheareaofthede-icebootwhenapplyingtorquetoabladeassembly.Placethebladepaddleinthethickestareaoftheblade,justoutsideofthede-iceboot.Useonebladepaddleperblade.

(4) Useonlytheapprovedconsumables,e.g.cleaningagents,lubricants,etc.

(5) SafeHandlingofPaintsandChemicals(a) Alwaysusecautionwhenhandlingorbeingexposed

topaintsand/orchemicalsduringpropelleroverhaulandmaintenanceprocedures.

(b) Beforeusingpaintorchemicals,alwaysreadthemanufacturer’slabelonthecontainerandfollowspecifiedinstructionsandproceduresforstorage,preparation,mixing,andapplication.

(c) Refertotheproduct’sMaterialSafetyDataSheet(MSDS)fordetailedinformationaboutphysicalproperties,health,andphysicalhazardsofanychemical.

(6) Observeapplicabletorquevaluesduringmaintenance.


Rev. 3 May/14


(7) Before installing the propeller on the engine, the propeller must be statically balanced. New propellers are statically balanced at Hartzell Propeller Inc. Overhauled propellers must be statically balanced by a certified propeller repair station with the appropriate rating before return to service.NOTE: Dynamic balance is recommended, but may

be accomplished at the discretion of the operator, unless specifically required by the airframe or engine manufacturer. Dynamic balancing is to be accomplished in accordance with the procedures and limitations in Maintenance Practices chapter of this manual. Additional procedures may be found in the aircraft maintenance manual.

(8) As necessary, use a soft, non-graphite pencil or crayon to make identifying marks on components.

(9) As applicable, follow military standard NASM33540 for safety wire, safety cable, and cotter pin general practices. Use 0.032 inch (0.81 mm) diameter stainless steel safety wire, unless otherwise indicated.

(10) The airframe manufacturer’s manuals should be used in addition to the information in this manual due to possible special requirements for specific aircraft applications.

(11)If the propeller is equipped with an anti-ice system, applicable instructions and technical information can be obtained by contacting Hartzell Propeller Inc. Product Support at (937) 778-4379 (business hours are 8:00 a.m. through 5:00 p.m., United States Eastern Time).

(12) If the propeller is equipped with an ice protection system that uses components supplied by Hartzell Propeller Inc., applicable instructions and technical information for the components supplied by Hartzell Propeller Inc. can be found in the following publications, available on the Hartzell Propeller Inc. website at www.hartzellprop.com.(a) Hartzell Propeller Inc. Manual 180 (30-61-80)

- Propeller Ice Protection System Manual (b) Hartzell Propeller Inc. Manual 180 (30-61-81)

- Propeller Ice Protection System Component Maintenance Manual


Rev. 3 May/14


(c) HartzellPropellerInc.Manual182(61-12-82) -PropellerElectricalDe-iceBootRemovalandInstallationManual

(d) HartzellPropellerInc.Manual183(61-12-83) -PropellerAnti-icingBootRemovalandInstallationManual

(13)PropellericeprotectionsystemcomponentsnotsuppliedbyHartzellPropellerInc.arecontrolledbytheapplicableTCorSTCholder’sInstructionsforContinuedAirworthiness(ICA).

(14)Approvedcorrosionprotectionfollowedbyapprovedpaintmustbeappliedtoallaluminumblades.Forinformationconcerningtheapplicationofcorrosionprotectionandpaint,refertotheMaintenancesPracticeschapterofthismanual.Operationofbladeswithoutthespecifiedcoatingsandfinishes,e.g.,“polishedblades”isnot permitted.

C. Continued Airworthiness(1) OperatorsareurgedtokeepinformedofAirworthiness

informationviaHartzellPropellerInc.ServiceBulletinsandServiceLetterswhichareavailablefromHartzellPropellerInc.distributors,orfromtheHartzellPropellerInc.factorybysubscription.SelectedinformationisalsoavailableonHartzellPropellerInc.’swebsiteat www.hartzellprop.com.

D. PropellerCriticalParts(1) Thefollowingmaintenanceproceduresmayinvolve

propellercriticalparts.TheseprocedureshavebeensubstantiatedbasedonEngineeringanalysisthatexpectsthisproductwillbeoperatedandmaintainedusingtheproceduresandinspectionsprovidedintheInstructionsforContinuedAirworthiness(ICA)forthisproduct.

(2) NumerouspropellersystempartscanproduceapropellerMajororHazardouseffect,eventhoughthosepartsmaynotbeconsideredasCriticalParts.TheoperatingandmaintenanceproceduresandinspectionsprovidedintheICAforthisproductare,therefore,expectedtobeaccomplishedforallpropellersystemparts.


Rev. 3 May/14


6. ReferencePublicationsThefollowingpublicationscontaininformationvitaltotheairworthinessofthepropellermodelscoveredinthismanual:HartzellPropellerInc.ManualNo.105A-OverhaulManualHartzellPropellerInc.ManualNo.110-OverhaulManualHartzellPropellerInc.ManualNo.114B-OverhaulManualHartzellPropellerInc.ManualNo.127(61-16-27) - Spinner AssemblyMaintenanceHartzellPropellerInc.ManualNo.133C(61-13-33)-AluminumPropellerBladeMaintenanceManualHartzellPropellerInc.ManualNo.159(61-02-59) - ApplicationGuide-AlsoavailableontheHartzellPropellerInc.website at www.hartzellprop.comHartzellPropellerInc.ManualNo.165A(61-00-65)-IllustratedToolandEquipmentManual.

HartzellPropellerInc.ManualNo.180(30-61-80)-PropellerIceProtectionSystemManual-AlsoavailableontheHartzellPropellerInc.websiteatwww.hartzellprop.com.HartzellPropellerInc.ManualNo.181(30-60-81)-PropellerIceProtectionSystemComponentMaintenanceManual -AlsoavailableontheHartzellPropellerInc.websiteat www.hartzellprop.com.

HartzellPropellerInc.ManualNo.182(61-12-82)-PropellerElectricalDe-iceBootRemovalandInstallationManual-AlsoavailableontheHartzellPropellerInc.websiteat www.hartzellprop.com.

HartzellPropellerInc.ManualNo.183(61-12-83)-PropellerAnti-icingBootRemovalandInstallationManual-AlsoavailableontheHartzellPropellerInc.websiteatwww.hartzellprop.com.HartzellPropellerInc.ManualNo.202A(61-01-02) - Standard PracticesManual-Volumes1through11HartzellPropellerInc.ServiceLetterHC-SL-61-61Y-OverhaulPeriodsandServiceLifeLimitsforHartzellPropellerInc.AviationComponents-Propellers,Governors,andPropellerDamperAssemblies -AlsoavailableontheHartzellPropellerInc.websiteatwww.hartzellprop.com.


Rev. 3 May/14


7. DefinitionsAbasicunderstandingofthefollowingtermswillassistinmaintainingandoperatingHartzellPropellerInc.propellersystems.

Term Definition

Annealed ...................... softeningofmaterialduetooverexposuretoheat

BladeAngle .................. measurementofbladeairfoillocationdescribedastheanglebetweenthebladeairfoilandthesurfacedescribedbypropellerrotation

Brinelling ....................... adepressioncausedbyfailureofthematerialincompression.

Chord ............................ astraightlinedistancebetweentheleadingandtrailingedgesofanairfoil

ColdRolling .................. compressiverollingprocessthatprovides improved strength and resistancetofatigue

ConstantForce ............. aforcethatisalwayspresentinsomedegreewhenthepropellerisoperating

Constant Speed ............ apropellersystemwhichemploysagoverningdevicetomaintainaselectedengineRPM

Corrosion ...................... gradualmaterialremovalordeteriorationduetochemicalaction

Crack ............................ irregularlyshapedseparationwithinamaterial,sometimesvisibleasanarrowopeningatthesurface

Depression ................... surfaceareawherethematerialhasbeencompressedbutnotremoved

Distortion ...................... alterationoftheoriginalshapeorsizeofacomponent


Rev. 3 May/14


Term Definition

Erosion ......................... gradualwearingawayordeteriorationduetoactionoftheelements

Exposure ...................... leavingmaterialopentoactionoftheelements

Feathering .................... apropellerwithbladesthatmayberotatedtoapositionparalleltotherelativewind,thusreducingaerodynamicdrag

Gouge ........................... surfaceareawherematerialhasbeenremoved

HazardousPropeller ThehazardouspropellereffectsEffects ........................... aredefinedinTitle14CFRsection

35.15(g)(1)HorizontalBalance ....... balancebetweenthebladetipandthe

centerofthehubImpactDamage ........... damagethatoccurswhenthe

propellerbladeorhubassemblystrikes,orisstruckby,anobjectwhileinflightorontheground

MajorPropellerEffect ... ThemajorpropellereffectsaredefinedinTitle14CFRsection35.15(g)(2)

Nick .............................. removalofpaintandpossiblyasmallamountofmaterial

Onspeed ....................... conditioninwhichtheRPMselectedbythepilotthroughthepropellercontrolleverandtheactualengine(propeller)RPMareequal

Overhaul ....................... theperiodicdisassembly,inspection,repair,refinish,andreassemblyofapropellerassemblytomaintainairworthiness


Rev. 3 May/14


Term Definition

Overspeed .................... conditioninwhichtheRPMofthepropellerorengineexceedspredeterminedmaximumlimits;theconditioninwhichtheengine(propeller)RPMishigherthantheRPMselectedbythepilotthroughthepropellercontrollever

Overspeed Damage ..... damagethatoccurswhenthepropellerhubassemblyrotatesataspeedgreaterthanthemaximumlimitforwhichitisdesigned

Pitch .............................. sameas“BladeAngle”Pitting ............................ formationofanumberofsmall,

irregularlyshapedcavitiesinsurfacematerialcausedbycorrosionorwear

PropellerCriticalParts .. Apartonthepropellerwhoseprimaryfailurecanresultinahazardouspropellereffect,asdeterminedbythesafetyanalysisrequiredbyTitle14CFRsection35.15

Scratch ......................... sameas“Nick”SingleActing ................. hydraulicallyactuatedpropellerwhich

utilizesasingleoilsupplyforpitchcontrol

Synchronizing ............... adjustingtheRPMofallthepropellersofamulti-engineaircrafttothe same RPM

Synchrophasing ............ aformofpropellersychronizationinwhichnotonlytheRPMoftheengines(propellers)areheldconstant,butalsothepositionofthepropellersinrelationtoeachother

Underspeed .................. theconditioninwhichtheactualengine(propeller)RPMislowerthantheRPMselectedbythepilotthroughthepropellercontrollever


Rev. 3 May/14


VerticalBalance ............ balancebetweentheleadingandtrailingedgesofatwo-bladepropeller,withthebladespositionedvertically

VariableForce .............. aforcewhichmaybeappliedorremovedduringpropelleroperation.

Windmilling ................... therotationofanaircraftpropellercausedbyairflowingthroughitwhiletheengineisnotproducingpower.

Term Definition


Rev. 3 May/14


8. Abbreviations

Abbreviation Term

AMM ............................. AircraftMaintenanceManualAN ................................. AirForce-Navy(orArmy-Navy)AOG .............................. AircraftonGroundFAA ............................... FederalAviationAdministrationFT-Lb ............................ Foot-PoundICA ................................ InstructionsforContinued

AirworthinessID .................................. Inside DiameterIn-Lb ............................. Inch-PoundIPS ................................ InchesPerSecondLbs ................................ PoundsMIL-X-XXX .................... MilitarySpecificationMPI ............................... MajorPeriodicInspection(Overhaul)MS ................................ MilitaryStandardMSDS ........................... MaterialSafetyDataSheetOD ................................ Outside DiameterNAS .............................. NationalAerospaceStandardsNASM ........................... NationalAerospaceStandards,

Military N•m ............................... Newton-MetersPOH .............................. Pilot’sOperatingHandbookPSI ................................ PoundsperSquareInchRPM .............................. RevolutionsperMinuteTBO .............................. TimeBetweenOverhaulTC ................................. TypeCertificateTSN .............................. TimeSinceNewTSO .............................. TimeSinceOverhaulNOTE: TSN/TSOisconsideredasthetimeaccumulated

betweenrotationandlanding,i.e.,flighttime.


Rev. 3 May/14


9. HartzellPropellerInc.ProductSupportA. HartzellPropellerInc.isreadytoassistyouwithquestions

concerningyourpropellersystem.HartzellPropellerInc.ProductSupportmaybereachedduringbusinesshours(8:00a.m.through5:00p.m.,UnitedStatesEasternTime)at(937)778-4379.

B. Afterbusinesshours,youmayleaveamessageonour 24hourproductsupportlineat(937)778-4376.AOGsupportisalsoavailable24hoursperday,sevendaysperweekviathismessageservice.

C. Additionalinformationisavailableonourwebsiteat www.hartzellprop.comNOTE: WhencallingfromoutsidetheUnitedStates,dial

(001)beforedialingtheabovetelephonenumbers.

10. WarrantyServiceA. Ifyoubelieveyouhaveawarrantyclaim,itisnecessary

tocontactHartzell’sWarrantyAdministrator.HartzellPropellerInc.’sWarrantyAdministratorwillprovideyouwitha Warranty Applicationform.Itisnecessarytocompletethis form and return it to the Warranty Administrator for evaluationbefore proceeding with repair or inspection work.Uponreceiptofthisform,theWarrantyAdministratorwillprovideinstructionsonhowtoproceed.HartzellPropellerInc.Warrantymaybereachedduringbusinesshours (8:00a.m.through5:00p.m.),UnitedStatesEasternTime)at(937)-778-4379ortollfreefromtheUnitedStatesandCanadaat(800)942-7767.HartzellPropellerInc.WarrantyAdministrationcanalsobereachedbyfaxat (937)778-4391,[email protected]. NOTE: WhencallingfromoutsidetheUnitedStates,dial

(001)beforedialingtheabovetelephonenumbers.


Rev. 3 May/14


11. HartzellPropellerInc.RecommendedFacilitiesA. HartzellPropellerInc.recommendsusingHartzellPropeller

Inc.approveddistributorsandrepairfacilitiesforthepurchase,repairandoverhaulofHartzellPropellerInc.propellerassembliesorcomponents.

B. InformationabouttheHartzellPropellerInc.worldwidenetworkofaftermarketdistributorsandapprovedrepairfacilitiesisavailableontheHartzellPropellerInc.websiteatwww.hartzellprop.com.


Rev. 3 May/14



INSTALLATION AND REMOVAL 61-00-69Page 3-1

Rev. 3 May/14


INSTALLATION AND REMOVAL - CONTENTS

1. Tools, Consumables, and Expendables ................................. 3-5A. Tooling ................................................................................ 3-5B. Consumables...................................................................... 3-5C. Expendables ....................................................................... 3-5

2. O-ringandPropellerMountingHardwareIdentification .......... 3-6

3. Pre-Installation ...................................................................... 3-10A.InspectionofShippingPackage ....................................... 3-10B.Uncrating .......................................................................... 3-10C.InspectionafterShipment ................................................. 3-10D.ReassemblyofaPropellerDisassembledforShipment .. 3-10

4. Propeller Assembly Installation ............................................. 3-11A.Precautions....................................................................... 3-11B.O-ringandPropellerMountingHardwareIdentification.... 3-12C.InstallingtheFFlangePropeller ModelsBHC-92()F-1D1 ................................................... 3-14

D.InstallingtheFFlangePropeller ModelsHC-92()F-8() ...................................................... 3-22

E.InstallingtheKFlangePropellerModelsHC-92()K-1D andHC-92()K-8() ........................................................... 3-28

F.InstallingtheFFlangePropellerModelsHC-92ZF-2() andHC-93ZF-2() ............................................................ 3-34

G.InstallingtheKFlangePropeller ModelsHC-92()K-2() ...................................................... 3-40

H.InstallingtheFFlangePropeller Models(B)HC-92()F-3 ................................................... 3-45

I. InstallingtheFFlangePropellerModels BHC-92(W,Z)F-3(L)G ...................................................... 3-57

J.InstallingtheFFlangePropeller ModelHC-92WF-5A ........................................................ 3-65

K.Installingthe20SplineHC-93Z20-1() Propeller Models ............................................................. 3-74

L.Installingthe20SplineHC-93Z20-2()andthe30Spline HC-93Z30-2()PropellerModels ...................................... 3-81

INSTALLATION AND REMOVAL 61-00-69 Page 3-2

Rev. 3 May/14


INSTALLATION AND REMOVAL - CONTENTS(continued)5. Post-InstallationChecks ....................................................... 3-96

6. Propeller Assembly Removal ................................................ 3-97A.RemovingtheFFlangePropeller ModelsBHC-92()F-1D1 ................................................... 3-97

B.RemovingtheFFlangePropeller ModelsHC-92()F-8() ...................................................... 3-99

C.RemovingtheKFlangePropeller ModelsHC-92()K-1DandHC-92()K-8() ...................... 3-102

D.RemovingtheFFlangePropeller ModelsHC-92ZF-2()andHC-93ZF-2() ........................ 3-105

E.RemovingtheKFlangePropeller ModelsHC-92()K-2() .................................................... 3-108

F.RemovingtheFFlangePropeller Models(B)HC-92()F-3 ................................................... 3-112

G.RemovingtheFFlangePropellerModels BHC-92(W,Z)F-3(L)G ..................................................... 3-116

H.RemovingtheFFlangePropeller ModelHC-92WF-5A ....................................................... 3-120

I.Removingthe20SplinePropeller ModelsHC-93Z20-1() .................................................... 3-125

J.Removingthe20SplineHC-93Z20-2()andthe30Spline HC-93Z30-2()PropellerModels .................................... 3-128


Rev. 3 May/14


LISTOFFIGURES

BHC-92()F-1D1PropellerAssembly.............Figure3-1............ 3-13InstallingFFlangePropeller

ontheEngineFlange ..............................Figure3-2............ 3-15DeterminingTorqueValueWhen

Using Torquing Adapter ...........................Figure3-3............ 3-16HC-92()()-1D,-8()PropellerAssembly ........Figure3-4............ 3-21KFlangeInstallationon-1PropellerModels .Figure3-5............ 3-25InstallingKFlangePropelleronthe

EngineFlange .........................................Figure3-6............ 3-27HC-92ZF-2(),HC-92()K-2()Propeller

Assembly ................................................Figure3-7............ 3-32HC-93ZF-2()PropellerAssembly .................Figure3-8............ 3-33KFlangeInstallationon-2PropellerModels .Figure3-9............ 3-39(B)HC-92()F-3PropellerAssembly ...............Figure3-10.......... 3-46ToolforDecompressingExternal

Beta System ............................................Figure3-11 .......... 3-47HC-92WF-3InstallationonTSIO-520-C

Engine .....................................................Figure3-12.......... 3-47InstallationofBetaValve,Governor,

andLinkage ............................................Figure3-13.......... 3-49CarbonBlockandBetaRingClearance ........Figure3-14.......... 3-50CarbonBlockAssembly.................................Figure3-15.......... 3-50Adjusting Propeller Reverse Control System Figure3-16.......... 3-53BHC-92(W,Z)F-3(L)GPropellerAssembly.....Figure3-17.......... 3-59BHC-92(W,Z)F-3(L)GInstallation .................Figure3-18.......... 3-60HC-92WF-5APropellerAssembly ................Figure3-19.......... 3-66HC-92WF-5AInstallation ..............................Figure3-20.......... 3-68HC-93Z20-1()PropellerAssembly................Figure3-21.......... 3-76InstallingPistonO-ringandFeltDustSeal ....Figure3-22.......... 3-78HC-93Z20-2A(1),-2B,-2C,-2D1Propeller

Assembly ................................................Figure3-23.......... 3-83HC-93Z20-2C1PropellerAssembly ..............Figure3-24.......... 3-84HC-93Z30-2EPropellerAssembly.................Figure3-25.......... 3-85Piston-to-LinkArmAttachmentDetails ..........Figure3-26.......... 3-87SpringAssembly-to-CylinderAttachment

Details .....................................................Figure3-27.......... 3-89FeatheringSpringAssembly..........................Figure3-28.......... 3-90Rear Hub Mounting Parts on 30-Spline

ShaftPropeller ........................................Figure3-29.......... 3-91


Rev. 3 May/14


LISTOFFIGURES(continued)

LISTOFTABLES

SafetyingtheShaftNutonaSplined ShaftPropeller .......................................Figure3-30.......... 3-93

Reversing (Beta) System and Governing Hardware ..............................Figure3-31........3-114

DisconnectingtheBetaRing .........................Figure 3-32........ 3-121

O-ring and Propeller Mounting HardwareIdentification ........................... Table 3-1 ............... 3-6

Torque Values Table ...................................... Table 3-2 ............. 3-17


Rev. 3 May/14


1. Tools, Consumables, and ExpendablesThesteelhubreciprocatingpropellerscoveredinthismanualaremanufacturedwitheitheraflangemountingorasplinemounting.Theflangetypeorsplinetypeusedonaparticularpropellerinstallationisindicatedinthepropellermodelidentificationnumberstampedonthehub.Forexample,HC-92WK-2Bindicatesa“K” flange.HC-93Z20-2Aindicatesa“20”spline.RefertotheSteelHubModelIdentificationintheDescriptionandOperationchapterofthismanualforadescriptionofeachflangetype.Theflangemountedpropellerisshippedcompletelyassembled.Thesplinemountedpropellerisshippedwiththepistonremoved.Thefollowingtools,consumables,andexpendableswillberequiredforpropellerremovalorinstallation:A. Tooling

F Flange •Safetywirepliers(Alternate:Safetycabletool) •Torquewrench •Torquewrenchadapter(HartzellPropellerInc. P/N AST-2814)K Flange •Safetywirepliers(Alternate:Safetycabletool) •Torquewrench •Torquewrenchadapter(HartzellPropellerInc. P/NAST-2805)20 Spline •Safetywirepliers •Shaftnutwrench(HartzellPropellerInc.P/NBST-2910) 30 Spline •Safetywirepliers •Spannerwrench(HartzellPropellerInc.P/NBT461)or StrapWrench(P/N100923) •Shaftnutwrench(HartzellPropellerInc.P/NBST-2910)

B. Consumables•QuickDryStoddardSolventorMethyl-Ethyl-Ketone(MEK)

C. Expendables•0.032inch(0.81mm)StainlessSteelAircraftSafetywire(Alternate:0.032inch[0.81mm]aircraftsafetycableandassociatedhardware) •O-ringPropellertoengineseal-RefertoTable3-1.


Rev. 3 May/14


O-ring and Propeller Mounting Hardware Identification Table 3-1

Part Propeller Model Part No.

2. O-ringandPropellerMountingHardwareIdentification

Bolt/Stud, Mounting HC-92WK-2( ) A-1328-2(4)or A-1333 (2) HC-92ZF-2( ) A-1333-4 HC-92ZK-2(A)( ) A-1328 (4) or A-1315 (2) HC-92ZK-2B A-1328 (4) or A-1333 (2) HC-93ZF-2( ) B-6739H7A HC-92( )K-1D * NOTE BHC-92( )F-1D1 A-1328-2 HC-92WF-8( ) A-1333-4 HC-92( )K-8( ) * NOTE HC-92ZF-8D A-1333-4 (B)HC-92( )F-3 A-1328-1 BHC-92( )F-3(L)G A-2986 BHC-92WF-5A A-1328-1

DowelPins HC-92ZF-2() B-6138-8-8 HC-93ZF-2() B-6138-8-8 HC-92()F-8() B-6138-8-8 (B)HC-92()F-1D1 B-1344orB-6138-8-8 (B)HC-92()F-3 B-6138-8-8 BHC-92WF-3(L)G B-6138-8-9orB-6138-8-10 HC-92WF-5A B-6138-8-8

FeltDustSeal (B)HC-92()F-1D1 B-1843

HC-93Z20-1()() B-1843 HC-93Z20-2()() B-1843 HC-93Z30-2E B-1843

HC-93Z30-2B A-810

Gasket,Governor (B)HC-92()F-3 B-1104-() (GovernorandBetaValve) BHC-92(W,F)-3(L)G HC-92WF-5A

Nut,ForkRod HC-92()(F,K)-8() A-848orA-848-2 HC-92()K-1D A-848orA-848-2 (B)HC-92WF-1D1 A-848-2 HC-93Z20-1(A,B,C)(1) A-848-2

*NOTE: (2)A-1333+(2)A-1333-3orA-1333(underlugsofcollar)+(2)A-1333-6 orA-1333-2(underrodsofpiston)


Rev. 3 May/14


O-ring and Propeller Mounting Hardware Identification Table 3-1, Continued

Nut,Governor (B)HC-92()F-3 B-3808-5 (GovernorandBetaValve) BHC-92(W,F)-3(L)G HC-92WF-5A

Nut,PistonRod HC-93Z20-2()(1) B-3368 HC-93Z30-2() B-3368 HC-93ZF-2() B-3368Nut,Pitchchangerod HC-92Z()-2()(L) A-880-2 HC-93Z20-2()(1) A-880-1 HC-93Z30-2() A-880-1 HC-93ZF-2A A-880-2 HC-93ZF-2B A-880-1 (B)HC-92()F-3 A-880-2 BHC-92WF-3(L)G A-880-2 HC-92WF-5A A-880-2

Nut,Shaft/Hub HC-93Z20-2()(1) A-63-B HC-93Z20-1()(1) A-63-B HC-93Z30-2() B-1814

Nut,Castle(MountingStud) HC-92WF-3 A-2069-2

NutLock,Shaft HC-93Z30-2(B,C) A-1839 HC-93Z30-2E A-1839-1

O-ring,Bushing HC-B3Z30-2E C-3317-210-1

O-ring, Piston (BHC)-92()F-1D1 C-3317-343-1 HC-93Z20-2()(1) C-3317-343-1 HC-93Z20-1()(1) C-3317-343-1 HC-93Z30-2B C-3317-343-1 HC-93Z30-2E C-3317-347-1

O-ring,Pitchchangerod HC-92()(F,K)-2()(L) C-3317-024 HC-93Z20-2(A,B,D)(1) C-3317-116 HC-93Z20-2C1 C-3317-020 HC-93Z30-2() C-3317-020 HC-93ZF-2(A,B) C-3317-343-1 (B)HC-92()F-3 C-3317-024 BHC-92()F-3(L)G C-3317-024 HC-92WF-5A C-3317-230

O-ring,RearCone HC-93Z20-2()(1) C-3317-229 HC-93Z20-1()(1) C-3317-229 HC-93Z30-2() C-3317-111


INSTALLATION AND REMOVAL 61-00-69 Page3-8

Rev. 3 May/14



O-ring,Shaft HC-92()K-2()(L) C-3317-329 HC-92ZF-2(A,B) C-3317-228 HC-92WF-8() C-3317-228 HC-92WK-8() C-3317-329 HC-92()K-1D C-3317-329 HC-92ZF-8D C-3317-228 HC-92ZK-8() C-3317-329 (B)HC-92()F-1D1 C-3317-228 HC-93ZF-2(A,B) C-3317-228 (B)HC-92()F-3 C-3317-228 BHC-92()F-3(L)G C-3317-228 HC-92WF-5A C-3317-228

SafetyPin HC-93Z20-2()(1) A-847 HC-93Z20-1()(1) A-847

Screw,PistonRod HC-93Z20-2()(1) A-2037 HC-93Z30-2() A-2037

Shim HC-92()K-2()(L) B-1322 HC-92()K-1D B-1322 HC-92()K-8() B-1322

Spacer HC-93Z30-2() A-1819 (B)HC-92()F-3G(L) C-2987

SpinnerMountingPlate (B)HC-92WF-1D1 B-1344

Stud,Governor (B)HC-92()F-3 A-3147 (GovernorandBetaValve) BHC-92(W,F)-3(L)G HC-92WF-5A

Washer,ForkRod HC-92()(F,K)-8() A-965 HC-92()K-1D A-965 (B)HC-92WF-1D1 A-965 HC-93Z20-1()(1) A-965



Rev. 3 May/14




Washer,Mounting HC-92ZF-2() B-3851-0863 HC-92WF-8() B-3851-0863orA-1381 HC-92ZF-8D B-3851-0863orA-1381 (B)HC-92()F-3 A-1381 BHC-92( )F-3(L)G A-1381 BHC-92WF-5A A-1381 HC-92(W,Z)K-2 A-946 (locatedatcounter- bore under blade)

Washer,PistonRod HC-93Z20-2()(1) A-1444 HC-93Z30-2() A-1444


Rev. 3 May/14


3. Pre-InstallationA. InspectionofShippingPackage

(1) Examinetheexterioroftheshippingcontainerforsignsofshippingdamage,especiallytheboxendsaroundeachblade.Ahole,tear,orcrushedappearanceattheendofthebox(bladetips)mayindicatethatthepropellerwasdroppedduringshipment,possiblydamagingtheblades.

B. Uncrating(1) Placethepropelleronafirmsupport.(2) Removethebandingandanyexternalwoodbracing

fromtheshippingcontainer.(3) Removethecardboardfromthehubandblades.

CAUTION: DONOTSTANDTHEPROPELLERONABLADE TIP.

(4) Placethepropelleronapaddedsurfacethatsupportsthepropelleroveralargearea.Neverstandthepropelleron a blade tip.

(5) Onflangemountedmodels,removetheplasticdustcovercupfromthepropellermountingflange(ifinstalled).

C. InspectionafterShipment(1) Afterremovingthepropellerfromtheshippingcontainer,

examinethepropellercomponentsforshippingdamage.D. ReassemblyofaPropellerDisassembledforShipment

(1) Ifapropellerwasreceiveddisassembledforshipment,it must be reassembled by trained personnel in accordancewiththeapplicablepropellermaintenancemanual.


Rev. 3 May/14


4. Propeller Assembly InstallationA. Precautions

WARNING 1: DURINGENGINEINSTALLATIONORREMOVAL, USING THE PROPELLER TO SUPPORTTHEWEIGHTOFTHEENGINEISNOTAUTHORIZED.UNAPPROVEDINSTALLATION AND REMOVAL TECHNIQUESMAYCAUSEDAMAGETOTHEPROPELLERTHATMAYLEADTOFAILURERESULTINGINANAIRCRAFTACCIDENT.

WARNING 2: WHENINSTALLINGTHEPROPELLER,FOLLOWTHEAIRFRAMEMANUFACTURER’SMANUALSANDPROCEDURES,ASTHEYMAYCONTAINISSUESVITALTOAIRCRAFTSAFETYTHAT ARE NOT CONTAINED IN THIS OWNER’SMANUAL.

CAUTION: INSTRUCTIONSANDPROCEDURESINTHISSECTIONMAYINVOLVEPROPELLERCRITICALPARTS.REFERTOTHEINTRODUCTIONCHAPTEROFTHISMANUALFORINFORMATIONABOUTPROPELLER CRITICAL PARTS.

(1) Besurethepropellerisremovedbeforetheengineisremovedorinstalledintheairframe.

(2) Followtheairframemanufacturer’sinstructionsforinstallingthepropeller.Ifsuchinstructionsarenotintheairframemanufacturer’smanual,thenfollowtheinstructionsinthismanual;however,mechanicsmustconsiderthatthisowner’smanualdoesnotdescribeimportantproceduresthatareoutsideitsscope.Inadditiontopropellerinstallationprocedures,itemssuchasriggingandpreflighttesting,installationandadjustmentofde-iceequipment,andpropellersynchronizationdevicesarenormallyfoundintheairframemanufacturer’smanuals.


Rev. 3 May/14


B. O-ringandPropellerMountingHardwareIdentification(1) RefertoTable3-1forspecificpartnumbersofO-rings

andpropellermountinghardware,andpropellermodeleffectivity.


Rev. 3 May/14


BH

C-9

2( )F

-1D

1 Pr

opel

ler A

ssem

bly

Figu

re 3

-1

EngineFlangeH

ub

ShaftO-ringBulkheadUnit

Mou

ntin

g B

olt

SpinnerAttachmentB

olt

Spi

nner

Mou

ntin

g R

ing

Spi

nner

Mou

ntin

g P

late

Self-L

ockingHexNut

D-1340

Spi

nner

Dom

e


Rev. 3 May/14


C. InstallingtheFFlangePropellerModelsBHC-92()F-1D1RefertoFigure3-1.

WARNING: MAKESURETHESLINGISRATEDUPTO800LBS.(363KG)TOSUPPORTTHEWEIGHTOFTHEPROPELLERASSEMBLYDURING INSTALLATION.

CAUTION 1: INSTRUCTIONSANDPROCEDURESINTHISSECTIONMAYINVOLVEPROPELLERCRITICALPARTS.REFERTO THE INTRODUCTION CHAPTER OFTHISMANUALFORINFORMATIONABOUT PROPELLER CRITICAL PARTS.

CAUTION 2: WHENINSTALLINGTHEPROPELLERONTHEAIRCRAFT,DONOTDAMAGETHEICEPROTECTIONSYSTEMCOMPONENTS,IFAPPLICABLE.

(1) Withasuitablecranehoistandsling,carefullymovethepropellerassemblytotheaircraftenginemountingflangeinpreparationforinstallation.

WARNING: ADHESIVESANDSOLVENTSAREFLAMMABLEANDTOXICTOTHESKIN,EYES,ANDRESPIRATORYTRACT.SKINANDEYEPROTECTIONAREREQUIRED.AVOID PROLONGED CONTACT AND BREATHINGOFVAPORS.USESOLVENTRESISTANTGLOVESTOMINIMIZESKINCONTACTANDWEARSAFETYGLASSESFOREYEPROTECTION.USEINAWELLVENTILATEDAREAAWAYFROMSPARKSANDFLAME.READANDOBSERVEALLWARNING LABELS.

(2) CleantheengineflangeandpropellerflangewithQuickDryStoddardSolventorMEK.

(3) Pressfittwodowelpinsthroughtheholesinthepropellerflangetobeflushwiththepropellersideofthehubflange.RefertoTable3-1.

(4) InstallthespecifiedshaftO-ringontheengineshaft.RefertoTable3-1.


Rev. 3 May/14


Installing F Flange Propeller on the Engine FlangeFigure 3-2

TorqueWrench

WasherBolt

EngineFlange

PropellerFlange

O-ring

Dowel Pin

D-2999FTORQUE.PLT

NOTE:Iftorquewrenchadapterisused,usethecalculationinTable3-1todeterminecorrecttorquewrenchsetting.

TorqueWrenchAdapterHartzellP/NAST-2814


Rev. 3 May/14


(5) SlidethespinnermountingringontotheengineflangeOD.

CAUTION: USECARETOAVOIDSCRAPINGALUMINUMFROMTHEBOREOFTHERING. SCRAPINGS COULD BECOME WEDGEDBETWEENTHEFLANGESURFACES.

(6) Alignthespinnerbulkheadmountingholeswiththering(onthepropellersideofthering).

(7) Alignthespinnermountingplatewiththering(ontheenginesideofthering).

(8) Installthespinnerattachmentboltsandself-lockinghexheadnutstoholdthespinnerbulkhead,spinnermountingring,andspinnermountingplatetogether.

(9) Torquethespinnerattachmentboltsandself-lockinghexheadnutsto8to12Ft-Lb(10-16N•m).

Determining Torque Value When Using Torquing Adapter Figure 3-3

APS0212A

(actualtorquerequired)X(torquewrenchlength) Torquewrenchreading(torquewrenchlength)+(lengthofadapter) = toachieverequiredactual torque

= <

EXAMPLE:

StandardTorqueWrench

0.25foot(76.2 mm)

1.00foot(304.8mm)

Torquing Adapter

100Ft-Lb(136N•m)x1ft(304.8mm)1ft(304.8mm)+0..25ft(76.2mm)

80Ft-Lb(108N•m)

reading on torque wrenchwith3-inch(76.2mm)adapterforactualtorqueof100Ft-Lb(136N•m)

Thecorrectionshownisforanadapterthatisalignedwiththecenterlineofthetorquewrench.Iftheadapterisangled90degreesrelativetothetorquewrenchcenterline,thetorquewrenchreadingandactualtorqueappliedwillbeequal.


Rev. 3 May/14


Torq

ue V

alue

s Ta

ble

Tabl

e 3-

2

Prop

elle

r Mod

el

Mou

ntin

g B

olt

Torq

ue

HC-92W

K-1D**

A-1333

70-80Ft-Lb(81-95N•m

)*

HC-92Z

K-1D

A-1333

70-80Ft-Lb(81-95N•m

)*

BHC-92W

F-1D

1A-1328-2

70-80Ft-Lb(81-95N•m

)*

BHC-92Z

F-1D

1A-1328-2

70-80Ft-Lb(81-95N•m

)*

HC-92Z

F-1D

1A-1328-2

70-80Ft-Lb(81-95N•m

)*

HC-92W

K-2,-2B

A-1328andA-1333

70-80Ft-Lb(81-95N•m

)*

HC-92Z

K-2,-2A

,-2A

L,-2

B

A-1328andA-1333

70-80Ft-Lb(81-95N•m

)*

HC-92Z

F-2A

,-2B

A-1333-4

70-80Ft-Lb(81-95N•m

)*

BHC-92W

F-3

A-1328-1orA-1333-4

70-80Ft-Lb(81-95N•m

)*

BHC-92Z

F-3

A-1328-1orA-1333-4

70-80Ft-Lb(81-95N•m

)*

HC-92W

F-3

A-1328-1orA-1333-4

70-80Ft-Lb(81-95N•m

)*

HC-92Z

F-3

A-1328-1orA-1333-4

70-80Ft-Lb(81-95N•m

)*

BHC-92W

F-3G

,-3LG

A-2069-2StudNut

90Ft-L

b(122N•m

)*

BHC-92Z

F-3LG

A-2069-2StudNut

90Ft-L

b(122N•m

)*

HC-92W

F-5A

A-1328-1orA-1333-4

70-80Ft-Lb(81-95N•m

)*

HC-92W

F-8D

,-8E

A-1333-4

70-80Ft-Lb(81-95N•m

)*

HC-92Z

F-8D

A-1333-4

70-80Ft-Lb(81-95N•m

)*

HC-92W

K-8D

A-1333

70-80Ft-Lb(81-95N•m

)*

HC-92Z

K-8D

A-1333

70-80Ft-Lb(81-95N•m

)*

HC-92W

K-8L

A-1333

70-80Ft-Lb(81-95N•m

)*

HC-92Z

K-8L

A-1333

70-80Ft-Lb(81-95N•m

)*

HC-93Z

F-2A

,-2B

A-1328

70-80Ft-Lb(81-95N•m

)*


Rev. 3 May/14


HC-93Z

20-2A,-2A

1A-63B

HubNut

450Ft-Lb(610N•m

)*

HC-93Z

20-2C

A-63B

HubNut

450Ft-Lb(610N•m

)*

HC-93Z

20-2D1

A-63B

orB

-2063Nut

450Ft-Lb(610N•m

)*

HC-93Z

20-1A

A-63B

orB

-2063Nut

450Ft-Lb(610N•m

)*

HC-93Z

20-1A1

A-63B

orB

-2063Nut

450Ft-Lb(610N•m

)*

HC-93Z

20-1B1

A-63B

orB

-2063Nut

450Ft-Lb(610N•m

)*

HC-93Z

20-2C1

A-63B

ShaftNut

450Ft-Lb(610N•m

)*

HC-93Z

30-2B,-2E

B-1814Nut

600Ft-Lb(813N•m

)*

Spin

ner m

ount

ing

bolts

30-40Ft-Lb(41-54N•m

)*

Pist

on N

ut

A-880-1

120Ft-Lb(163N•m

)*

Low

-pitc

h st

op n

ut

A-848

20-22Ft-Lb(27-30N•m

)*

A-848-2

*

Torquetoleranceis±10percentunlessotherwisenoted.

**Exceptionstotorquevalueslistedinabovechart:H

C-92W

K-1Dw

heninstalledonaFoundBros.Centenial

100orTechnoimport-Torque=80-90Ft-L

b(108-122N•m

)*

NO

TE 1:

Torquevaluesarebasedonnon-lubricatedthreads.

NO

TE 2:

Spec

ified

torq

ues

take

into

acc

ount

the

run

on to

rque

of t

he fa

sten

ers.

No

adju

stm

ent

of th

e sp

ecifi

ed to

rque

is re

quire

d to

allo

w fo

r run

on

torq

ue.

Torq

ue V

alue

s Ta

ble

Tabl

e 3-

2, C

ontin

ued

Prop

elle

r Mod

el

Mou

ntin

g B

olt

Torq

ue


Rev. 3 May/14


(10)Alignthemountingholesanddowelpinsinthepropellerhubflangewiththemountingholesandthedowelpinholesintheengineflange.

CAUTION: MAKESURETHATCOMPLETEANDTRUESURFACECONTACTISESTABLISHEDBETWEEN THE PROPELLER HUB FLANGEANDTHEENGINEFLANGE.

(11)Slidethepropellerflangeontotheengineflange.(12)Alignthespinnermountingplateclearanceholeswith

theengineflangeclearanceholes.

CAUTION: NEWPROPELLERMOUNTINGBOLTSMUSTBEUSEDWHENINITIALLYINSTALLING A NEW OR OVERHAULED PROPELLER.

(13)Installthemountingboltswithwashers(ifapplicable)throughthespinnermountingplateandtheengineflangefromtherearandintothetappedholesinthepropellerflange.RefertoTable3-1andFigure3-1.NOTE: Forpropellerremovalsbetweenoverhaul

intervals,mountingboltsandwashersmaybereusediftheyarenotdamagedorcorroded.

(14)UseatorquewrenchwithatorquewrenchadapterHartzellPropellerInc.P/NAST-2814totorqueallmountingboltsinsequenceinaccordancewith Table3-2,TorqueValuesTable,Figure3-2,and Figure3-3todeterminethepropertorquevaluetowhichthetorquewrenchmustbeset.(a) Torquethemountingboltstohalfofthefinaltorque,

beginningwithanymountingbolt,andmovingclockwiseorcounterclockwiseuntilalltheboltsaretorqued.

(b) Finaltorquetheboltsinsequence,beginningwithanymountingbolt,andmovingclockwiseorcounterclockwiseuntilalltheboltsaretorqued.

(15)Safetyallmountingboltswith0.032inch(0.81mm)minimum diameter stainless steel wire or equivalent aircraftsafetycableandassociatedhardware(twoboltspersafety).


Rev. 3 May/14


(16)IfthepropellerisequippedwithaniceprotectionsystemthatusescomponentssuppliedbyHartzellPropellerInc.,applicableinstructionsandtechnicalinformationforthecomponentssuppliedbyHartzellPropellerInc.canbefoundinthefollowingpublicationsavailableontheHartzellPropellerInc.websiteatwww.hartzellprop.com.(a) HartzellPropellerInc.Manual180(30-61-80)

-PropellerIceProtectionSystemManual(b) HartzellPropellerInc.Manual181(30-60-81)

-PropellerIceProtectionSystemComponentMaintenanceManual

(c) HartzellPropellerInc.Manual182(61-12-82)-PropellerElectricalDe-iceBootRemovalandInstallation Manual



(18)Installthespinnerdomeasfollows:NOTE: ThefollowinginstructionsrelatetoHartzell

PropellerInc.spinnersonly.Insomecases,theairframemanufacturerproducedthespinnerassembly.Inthosecases,refertotheairframemanufacturer’smanualforspinnerinstallationinstructions.


Rev. 3 May/14


D-1334

HC

-92(

)( )-

1D,-8

( ) P

rope

ller A

ssem

bly

Figu

re 3

-4

EngineFlange

Hub

ShaftO-ring

BulkheadUnit

Mou

ntin

g B

olt

Spi

nner

Dom

e

Mou

ntin

g B

olt

MountingWasher

Spi

nner

Mou

ntin

g R

ing

“K”F

lange

“F”F

lange


Rev. 3 May/14


CAUTION 1: TOPREVENTDAMAGETOTHEBLADE AND BLADE PAINT, WRAP THEBLADESHANKSINSEVERALLAYERSOFMASKINGORDUCTTAPEBEFOREINSTALLINGTHESPINNERDOME.REMOVETHETAPEAFTERTHE SPINNER IS INSTALLED.

CAUTION 2: THESPINNERDOMEWILLWOBBLEIFNOTALIGNEDPROPERLY,ANDMAYAFFECTTHEBALANCEOFTHEPROPELLER.

(a) Carefullyslidethespinnerdomeoverthereassembled propeller.

(b) Attachthespinnerdometothespinnerbulkheadwiththesuppliedscrewsandwashers.

D. InstallingtheFFlangePropellerModelsHC-92()F-8()RefertoFigure3-4.


CAUTION 1: INSTRUCTIONSANDPROCEDURESINTHISSECTIONMAYINVOLVEPROPELLERCRITICALPARTS.REFERTOTHEINTRODUCTIONCHAPTEROFTHISMANUALFORINFORMATIONABOUTPROPELLER CRITICAL PARTS.




Rev. 3 May/14


WARNING: ADHESIVESANDSOLVENTSAREFLAMMABLEANDTOXICTOTHESKIN,EYES,ANDRESPIRATORYTRACT.SKINANDEYEPROTECTIONAREREQUIRED.AVOID PROLONGED CONTACT AND BREATHINGOFVAPORS.USESOLVENTRESISTANTGLOVESTOMINIMIZESKINCONTACTANDWEARSAFETYGLASSESFOREYEPROTECTION.USEINAWELLVENTILATEDAREAAWAYFROMSPARKSANDFLAME.READANDOBSERVEALLWARNING LABELS.

(2) CleantheengineflangeandpropellerflangewithQuickDryStoddardSolventorMEK.

(3) Pressfittwodowelpinsthroughtheholesinthepropellerflangetobeflushwiththepropellersideofthehubflange.RefertoTable3-1.

(4) InstallthespecifiedshaftO-ringontheengineshaft.RefertoTable3-1.

(5) Alignthemountingholesanddowelpinsinthepropellerhubflangewiththemountingholesandthedowelpinholesintheengineflange.NOTE: Thespinnerbulkheadisalreadyattachedtothe

propellersideofthepropellermountingflange.

CAUTION 1: USECARETOAVOIDSCRAPINGALUMINUMFROMTHEBOREOFTHERING. SCRAPINGS COULD BECOME WEDGEDBETWEENTHEFLANGESURFACES.

CAUTION 2: MAKESURETHATCOMPLETEANDTRUESURFACECONTACTISESTABLISHEDBETWEENTHEPROPELLERHUBFLANGEANDTHEENGINEFLANGE.

(6) Slidethepropellerflangeandspinnerbulkheadontotheengineflange.


Rev. 3 May/14


CAUTION: NEWPROPELLERMOUNTINGBOLTSMUSTBEUSEDWHENINITIALLYINSTALLING A NEW OR OVERHAULED PROPELLER.

(7) Installthemountingboltswithmountingwashersthroughtheengineflangefromtherearandintothetappedholesinthepropellerflange.RefertoTable3-1andFigure3-4.NOTE: Forpropellerremovalsbetweenoverhaul

intervals,mountingboltsandwashersmaybereusediftheyarenotdamagedorcorroded.

(8) UseatorquewrenchwithatorquewrenchadapterHartzellPropellerInc.P/NAST-2814totorqueallmountingboltsinsequenceinaccordancewith Table3-2,TorqueValuesTable,Figure3-2,and Figure3-3todeterminethepropertorquevaluetowhichthetorquewrenchmustbeset.(a) Torquethemountingboltstohalfofthefinaltorque,

beginningwithanymountingbolt,andmovingclockwiseorcounterclockwiseuntilalltheboltsaretorqued.

(b) Finaltorquetheboltsinsequence,beginningwithanymountingbolt,andmovingclockwiseorcounterclockwiseuntilalltheboltsaretorqued.

(9) Safetyallmountingboltswith0.032inch(0.81mm)minimum diameter stainless steel wire or equivalent aircraftsafetycableandassociatedhardware(twoboltspersafety).

(10)IfthepropellerisequippedwithaniceprotectionsystemthatusescomponentssuppliedbyHartzellPropellerInc.,applicableinstructionsandtechnicalinformationforthecomponentssuppliedbyHartzellPropellerInc.canbefoundinthefollowingpublicationsavailableontheHartzellPropellerInc.websiteatwww.hartzellprop.com.(a) HartzellPropellerInc.Manual180(30-61-80)

-PropellerIceProtectionSystemManual(b) HartzellPropellerInc.Manual181(30-60-81)

-PropellerIceProtectionSystemComponentMaintenanceManual


Rev. 3 May/14


K Flange Installation on -1 Propeller Models Figure 3-5

D-1334

Adapter Ring

Shim

Mounting Bolt

ShaftO-ringEngineFlange

Starter Ring Gear


Rev. 3 May/14


(c) HartzellPropellerInc.Manual182(61-12-82)-PropellerElectricalDe-iceBootRemovalandInstallation Manual



(12)Installthespinnerdomeasfollows:

CAUTION 1: TOPREVENTDAMAGETOTHEBLADE AND BLADE PAINT, WRAP THEBLADESHANKSINSEVERALLAYERSOFMASKINGORDUCTTAPEBEFOREINSTALLINGTHESPINNERDOME.REMOVETHETAPEAFTERTHE SPINNER IS INSTALLED.

CAUTION 2: THESPINNERDOMEWILLWOBBLEIFNOTALIGNEDPROPERLY,ANDMAYAFFECTTHEBALANCEOFTHEPROPELLER.

NOTE: ThefollowinginstructionsrelatetoHartzellPropellerInc.spinnersonly.Insomecases,theairframemanufacturerproducedthespinnerassembly.Inthosecases,refertotheairframemanufacturer’smanualforspinnerinstallationinstructions.

(a) Carefullyslidethespinnerdomeoverthereassembled propeller.

(b) Securethespinnerdometothespinnerbulkheadwiththesuppliedscrewsandwashers.


Rev. 3 May/14


Installing K Flange Propeller on the Engine FlangeFigure 3-6

TorqueWrenchAdapterHartzellP/NAST-2814

Torque Wrench

EngineFlange

Propeller Flange

O-ring

Shim

Starter Ring Gear

Mounting Bolt

W10298TORQUE.PLT

NOTE: Iftorquewrenchadapterisused,usethecalculationinTable3-1todeterminecorrecttorquewrenchsetting.


Rev. 3 May/14


E. InstallingtheKFlangePropellerModelsHC-92()K-1D andHC-92()K-8()RefertoFigure3-4.


CAUTION 1: INSTRUCTIONSANDPROCEDURESINTHISSECTIONMAYINVOLVEPROPELLERCRITICALPARTS.REFERTOTHEINTRODUCTIONCHAPTEROFTHISMANUALFORINFORMATIONABOUTPROPELLER CRITICAL PARTS.



WARNING: ADHESIVESANDSOLVENTSAREFLAMMABLEANDTOXICTOTHESKIN,EYES,ANDRESPIRATORYTRACT.SKINANDEYEPROTECTIONAREREQUIRED.AVOID PROLONGED CONTACT AND BREATHINGOFVAPORS.USESOLVENTRESISTANTGLOVESTOMINIMIZESKINCONTACTANDWEARSAFETYGLASSESFOREYEPROTECTION.USEINAWELLVENTILAT