- Compact Wheel Loader
- All
- Earthmoving Compactor
- All
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- All
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- Wheel Loader
- All
Introduction
Revision | Summary of Changes in SEBF8093 |
---|---|
13 | Updated boilerplate information, added clarity to Illustrations, tables, verbiage, and document layout. Corrected several Tolerances throughout this document. Added information for 20 part numbers. |
12 | Added 22 part numbers. |
11 | Added 3 part numbers. |
10 | Added 10 part numbers. |
© 2018 Caterpillar All Rights Reserved. This guideline is for the use of Cat dealers only. Unauthorized use of this document or the proprietary processes therein without permission may be violation of intellectual property law.
Information contained in this document is considered Caterpillar: Confidential Yellow.
This Reuse and Salvage Guideline contains the necessary information to allow a dealer to establish a parts reusability program. Reuse and salvage information enables Caterpillar dealers and customers to benefit from cost reductions. Every effort has been made to provide the most current information that is known to Caterpillar. Continuing improvement and advancement of product design might have caused changes to your product which are not included in this publication. This Reuse and Salvage Guideline must be used with the latest technical information that is available from Caterpillar.
For technical questions when using this document, work with your Dealer Technical Communicator (TC).
To report suspected errors, inaccuracies, or suggestions regarding the document, submit a form for feedback in the Service Information System (SIS Web) interface.
Canceled Part Numbers and Replaced Part Numbers
This document may include canceled part numbers and replaced part numbers. Use the Numerical Part Record (NPR) on the Service Information System Website (SIS Web) for information about canceled part numbers and replaced part numbers. NPR will provide the current part numbers for replaced parts.
Important Safety Information
Illustration 1 | g02139237 |
Work safely. Most accidents that involve product operation, maintenance, and repair are caused by failure to observe basic safety rules or precautions. An accident can often be avoided by recognizing potentially hazardous situations before an accident occurs. A person must be alert to potential hazards. This person should also have the necessary training, skills, and tools to perform these functions properly. Safety precautions and warnings are provided in this instruction and on the product. If these hazard warnings are not heeded, bodily injury or death could occur to you or to other persons. Caterpillar cannot anticipate every possible circumstance that might involve a potential hazard. Therefore, the warnings in this publication and the warnings that are on the product are not all inclusive. If a tool, a procedure, a work method, or operating technique that is not recommended by Caterpillar is used, ensure that it is safe for you and for other people to use. Ensure that the product will not be damaged or the product will not be made unsafe by the operation, lubrication, maintenance, or the repair procedures that are used.
Improper operation, lubrication, maintenance or repair of this product can be dangerous and could result in injury or death. Do not operate or perform any lubrication, maintenance or repair on this product, until you have read and understood the operation, lubrication, maintenance and repair information. |
Safety precautions and warnings are provided in this manual and on the product. If these hazard warnings are not heeded, bodily injury or death could occur to you or to other persons.
The hazards are identified by the safety alert symbol which is followed by a signal word such as danger, warning, or caution. Refer to Illustration 2 for an example of a “WARNING” Safety Alert Symbol.
Illustration 2 | g00008666 |
This safety alert symbol means:
Pay attention!
Become alert!
Your safety is involved.
The message that appears under the safety alert symbol explains the hazard.
Operations that may cause product damage are identified by "NOTICE" labels on the product and in this publication.
Caterpillar cannot anticipate every possible circumstance that might involve a potential hazard. The safety information in this document and the safety information on the machine are not all inclusive. Determine that the tools, procedures, work methods, and operating techniques are safe. Determine that the operation, lubrication, maintenance, and repair procedures will not damage the machine. Also, determine that the operation, lubrication, maintenance, and repair procedures will not make the machine unsafe.
The information, the specifications, and the illustrations that exist in this guideline are based on information which was available at the time of publication. The specifications, torques, pressures, measurements, adjustments, illustrations, and other items can change at any time. These changes can affect the service that is given to the product. Obtain the complete, most current information before you start any job. Caterpillar dealers can supply the most current information.
Summary
This guideline provides information, which aids in the determination of the reusability of the planetary carrier in the final drive.
This guideline provides the procedures necessary to determine the reusability of planetary final drives. Life will vary depending on application, load, lubrication, and environment.
This guideline contains the latest standards of engineering, which will help minimize owning and operating costs. A part is expected to reach the next Planned Component Rebuild (PCR) if the part meets the specifications within this guideline and the part is intended for a similar application. Use this guideline to determine whether a part should be reused. Do not install a part that is not reusable. During reconditioning, correct any condition that might have caused the original failure.
The dimensions and tolerances provided are to return a part / component to specification. The dimensional information alone is not solely used to condemn a part from reuse. Follow visual inspections and the "Crack Detection Methods" section for further guidance.
References
References | |
---|---|
Media Number | Publication Type & Title |
Channel1 | "Gear Tooth Inspection" |
https://channel1.mediaspace.kaltura.com/media/Gear+Tooth+Inspection/1_5ujdi5zp | |
"Why Reuse and Salvage Parts" | |
https://channel1.mediaspace.kaltura.com/media/Why+Reuse+and+Salvage+Parts/0_ae9rhu2z | |
PERJ1017 | Special Publication
"Dealer Service Tools Catalog" |
SEBF8163 | Reuse and Salvage Guidelines
"Procedures to Salvage Thrust Faces on Planetary Carriers" |
SEBF8187 | Reuse and Salvage Guidelines
"Standardized Parts Marking Procedures" |
SEBF8193 | Reuse and Salvage Guidelines
"Reusability of Drive Train Gears" |
SEBF8728 | Reuse and Salvage Guidelines
"Specifications for Inspection of Driveline Fasteners" |
SEBF9236 | Reuse and Salvage Guidelines
"Fundamentals of High Velocity Oxygen Fuel (HVOF) Spray for reconditioning Components" (1) |
SEBF9238 | Reuse and Salvage Guidelines
"Fundamentals of Arc Spray for reconditioning Components" (1) |
SEBF9240 | Reuse and Salvage Guidelines
"Fundamentals of Flame Spray for Reconditioning Components" (1) |
(1) | Only Cat dealers may utilize applications for Thermal Spray. The processes must be carried out within the facilities of the dealership. The dealership must maintain a clean environment and always use the correct equipment for all processes in each Thermal Spray Application. |
Service Advisories, Service Letters, and Technical Service Bulletins
The most recent Service Advisories, Service Letters, and Technical Service Bulletins that are related to this component should be reviewed before beginning work. Often Service Advisories, Service Letters, and Technical Service Bulletins contain upgrades in repair procedures, parts, and safety information which pertain to the components being repaired.
Tooling and Equipment
Note: The Tooling and Equipment in Table 3 is not an all inclusive list of Tooling required to perform every task within this document. Tooling needs may vary for scope of work to be performed for each specific rebuild.
Required Tooling and Equipment | ||
---|---|---|
Part Number | Description | Designation |
— (1) | Personal Protective Equipment (PPE) | Personal Protection |
— (2) | Clevis/ Shackle | Component
Repositioning and Movement |
— (2) | Lifting Eye Assemblies | Component
Repositioning and Movement |
— (2) | Tool (Cribbing) | Component
Repositioning and Movement |
— | Suitable Lifting Device | Component
Repositioning and Movement |
Telescoping Magnet | General Tooling | |
Automatic Tape Measure (1-inch X 26- ft)
|
Measurement
Checks |
|
Caliper
|
Profile
Measurement |
|
Tool
Rule |
Measurement
Checks |
|
Feeler Gauge
|
Thickness
Measurement Checks |
|
Tools (Micrometer)
Internal |
Internal
Measurement Checks |
|
Tool (Ruler)
|
Measurement
Checks |
|
Micrometers
External |
External
Measurement Checks |
|
or |
Instrument Group
Micrometer, Inside 2.00 - 12.00 inch |
Internal
Measurement Checks |
Instrument Group
Micrometer, Inside 50 - 300 mm |
||
Instrument Group
Micrometer, Outside 0.00 - 4.00 inch |
External
Measurement Checks |
|
Instrument Group
Micrometer, Outside 2.00 - 6.00 inch |
External
Measurement Checks |
|
Instrument Group
Micrometer, Outside - Digital |
External
Measurement Checks |
|
or |
Instrument Group
Micrometer, Inside |
Internal
Measurement Checks |
Instrument Group
Micrometer, Inside |
||
Tool (Level)
|
Level | |
—
and /or — |
GO/NO-GO Thread Gauge Set, Metric | Threaded Hole
Inspection |
GO/NO-GO Thread Gauge Set, SAE | ||
— (2) | Plastic Plug Assortment | Threaded Hole
Protection |
— (2) | Tap and Die Set | Threaded Hole
/ Restore |
File Metric | Threaded Shaft
/ Restore |
|
Disc (Coarse) | Surface
Preparation / De-burring |
|
Threaded Shaft | Surface
Preparation / De-burring |
|
Holder (Disc Pad) | Surface
Preparation / De-burring |
|
Grinding Wheel | Surface
Preparation / De-burring |
|
Grinding Wheel | Surface
Preparation / De-burring |
|
Abrasive Disc | Surface
Preparation / De-burring |
|
Abrasive Disc | Surface
Preparation / De-burring |
|
Grinding Wheel | Surface
Preparation / De-burring |
|
Wheel
(60 Grit) |
Surface
Preparation / De-burring |
|
Grinding Wheel (F-Grade)
(120 Grit) |
Surface
Preparation / De-burring |
|
Die Grinder
(Right Angle) |
Surface
Preparation / De-burring |
|
Brush
|
Surface
Preparation / De-burring |
|
Metal Marking Pen | Parts Marking | |
Polishing Stone | Gear Polishing | |
Brush | General Cleaning | |
Abrasive Material (Roll) | General Cleaning | |
Surface Reconditioning Pad (180 Grit) | General Cleaning | |
Towel | General Cleaning | |
— | Large Rubber Band | MOP Small Gear/
Spline Wear Inspection |
Tool Group
Gage Pins |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
— | Precision Gage Pins (4)
x |
Measurement
Between / MOP Gear/ Spline Wear Inspection |
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
Pin Set
|
Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
Tool (Magnet) (6) | Measurement
Between / MOP Gear/ Spline Wear Inspection |
|
— | Magnets | Measurement
Between / MOP Large Gear/ Spline Wear Inspection |
Seal Pick
Kit |
Gear/ Shaft
Step Inspection |
|
Comparison Gauge (Surface Texture) | Surface Texture
Tester |
|
Tool
Specimen |
Surface Texture
Tester |
|
Indicator
(Profilometer) |
Surface Texture
Tester |
|
Magnifying Glass | Visual Surface
Inspection (VT) |
|
Mirror (Telescoping) | Visual Surface
Inspection (VT) |
|
Flashing Lights Conversion Kit | Visual Surface
Inspection (VT) |
|
Light | Visual Surface
Inspection (VT) |
|
— (2) | Bright Incandescent Light | Visual Surface
Inspection (VT) |
— | Reflective Surface for Inspection | Visual Surface
Inspection (VT) |
Microscope (40-Power)
|
Crack/
Measurement Inspection |
|
Paper Towel | Liquid Penetrant
Testing (PT) |
|
Brush
Curved Handle Wire |
General Cleaning/
Liquid Penetrant Testing (PT) |
|
— | Developer | Liquid Penetrant
Testing (PT) |
— | Penetrating Oil | Liquid Penetrant
Testing (PT) |
— | Solvent Cleaner | General Cleaning/
Liquid Penetrant Testing (PT) |
Crack Detection Kit (Magnetic Particle) | Dry Magnetic
Particle Testing (MPT) |
|
— | Paint Pen | Dry Magnetic
Particle Testing (MPT) |
Lamp Group
Ultraviolet |
Wet Magnetic
Particle Testing (MPT) |
|
Fluid
Ultrasonic Wear Indicator |
Ultrasonic
Testing (UT) |
|
Tool Group(Ultrasonic) | Ultrasonic
Testing (UT) |
(1) | Refer to PERJ1017Special Publication, "Dealer Service Tools Catalog" for Personal Protective Equipment (PPE) part numbers suitable by geographic location and local safety standards. |
(2) | Refer to Special Publication, PERJ1017, "Dealer Service Tools Catalog" for suitable tooling. |
(3) | Available in the United States only. |
(4) | Minimum of two are required. |
(5) | Part of Tool Group |
(6) | For use with precision gage pins. |
Prepare the Area for Inspection
Personal injury can result when using cleaner solvents. To help prevent personal injury, follow the instructions and warnings on the cleaner solvent container before using. |
Personal injury can result from air pressure. Personal injury can result without following proper procedure. When using pressure air, wear a protective face shield and protective clothing. Maximum air pressure at the nozzle must be less than |
Illustration 3 | g03794147 |
Typical burr removal Tooling. (A) Die Grinder, Right Angle (B) Wheel Grinder, Group (C) Conditioning Discs, Disc pad Holder, and Threaded Shaft (D) Flapper Wheel |
- Before you inspect a part, clean the part thoroughly to ensure that all components are free from rust, oil, burrs, and debris prior to inspection. A surface irregularity can hide the indication of an unacceptable defect.
- Use a proper lifting device to provide safety to the operator. Also, use a proper lifting device to prevent damage to the part when you lift the part.
- During cleaning, do not damage machined surfaces.
- Do not use pressurized air to dry internal components. Compressed air has moisture and contaminants that can cause premature failure of internal components.
- Inspect all fasteners that have been removed, refer to SEBF8728, "Specifications for Inspection of Driveline Fasteners" for more information.
- Put hydraulic oil on all machined surfaces to prevent rust or corrosion if inspection is not done immediately after cleaning. Carefully store the parts in a clean container.
- Inspect all flange mating surfaces for fretting. Ensure that flange mating surfaces are true and free from raised material resulting from rust, nicks, and dents.
- Use appropriate thread taps to chase all threaded holes.
Standardized Parts Marking
Reference: , SEBF8187Reuse and Salvage Guidelines, "Standardized Parts Marking Procedures".
The code is a Cat standard and is used to record the history of a component. The code will identify the number of rebuilds and hours at the time of each rebuild. This information is important and should be considered for any decision to reuse a component.
Ensure that the mark is not covered by a mating part. Use a metal marking pen to mark the code onto the component.
NOTICE |
---|
Do not use numbering stamp punches to mark internal components. The impact from striking the stamp will cause an abnormal stress riser. The added stress riser may cause premature part failure. |
Illustration 4 | g06124077 |
DO NOT use numbering stamp punches to mark internal components. |
The procedure for marking components is a Cat standard. This code is helpful when the machine is sold into a different territory after the first rebuild. During an overhaul, the previous code of a part should never be removed.
Example 1
Illustration 5 | g03856853 |
Typical Example |
Illustration 5 shows code (1-15). The first number (1) indicates that the gear had been repaired once. The second number (15) indicates that there were 15,000 hours on the gear at the time of repair.
Example 2
Illustration 6 | g03748362 |
Example |
This coding can be used by all dealers and will help with identification at time of repair. Identification can be especially helpful if units that have been rebuilt are sold into different territories. As rebuilds are completed, the previous markings should be left on the component.
Illustration 6 shows code (1-12) and code (2-10). Code (2-10) represents the information from the second rebuild. The first number (2) indicates that the gear had been rebuilt twice. The second number (10) indicates that 10,000 hours accumulated on the gear between the first and second rebuild.
Note: Add the first and second rebuild hours to obtain the total number of hours for the gear in Illustration 6. In this example, the gear has a total of 22,000 hours.
Example 3
Illustration 7 | g03519882 |
Typical Example |
(A) Mark the planet pin on either end using a metal marking pen.
Final Drive Wheel Group Component Locations
Illustration 8 | g06320845 |
Typical Example of Final Drive Wheel Group - Without Brakes (1) Spindle (2) Wheel (3) Reaction Hub (4) Planetary Carrier (5) Planetary Gear (6) Planetary Shaft |
Illustration 9 | g06321222 |
Typical Example of Final Drive Wheel Group - With Brakes (1) Spindle (2) Wheel (3) Hub (4) Planetary Carrier (5) Planetary Gear (6) Planetary Shaft (7) Service Brake Group |
Measurement Techniques
NOTICE |
---|
Precise measurements shall be made when the component and measurement equipment are at |
Measurement Tooling Calibration
Outside Micrometers
Illustration 10 | g06208395 |
Typical example of calibrating outside micrometer (A). (A) Outside Micrometer |
Measurement Tooling include precision inside and outside diameter micrometers capable of measuring four decimal places in inches or three decimal places in millimeters. Measurement Tooling should be calibrated using gauge blocks certified to a national standard such as the National Institute of Standards and Technology (NIST).
Inside Micrometer
Illustration 11 | g06208411 |
Typical example of calibrating inside micrometer (B). (B) Inside Micrometer |
Bore Diameters
Illustration 12 | g06318221 |
Typical example of measuring bore Inside Dimension (ID) of a wheel. (A) Indicates the diameter of the bore. (B) Indicates the overall thickness of the material. |
Note: Measurements taken on the edge of a bore may not give an accurate measurement.
Take measurements at locations (A1), (A2), and (A3).
Then take measurements at locations (A4), (A5), and (A6).
To ensure adequate life of the components, this document contains precise tolerances for measurements taken on various features. Ensure that several sample measurements are taken at different locations on the same feature. Measure diameters of internal bores in six places to identify tapered and or oval conditions. Refer to Illustration 12.
Shaft and Journal Diameters
Illustration 13 | g06318222 |
Typical example of measuring an Outside Diameter (OD) Dimension of a spindle. (C) Indicates the diameter of the shaft. (D) Indicates the overall measurable length of the shaft journal. |
Take measurements at locations (C1), (C2), and (C3).
Then take measurements at locations (C4), (C5), and (C6).
To ensure adequate life of the components, this document contains precise tolerances for measurements taken on various features. Ensure that several sample measurements are taken at different locations on the same feature. Measure diameters of journals in six places to identify tapered and or oval conditions. Refer to Illustration 13.
Specification of the Pin Bore of the Planetary Carrier
Pin Bore Inspection
Bores will usually show a contact area from the shaft that may be worn slightly. The bore may also have damage from some broaching, fretting, adhesion, or impact. If any of the following conditions exist, the planetary carrier shall not be reused:
- The bore has a wear step that will stop a seal pick.
- The shaft has spun in the bore.
- The bore is elongated or cracked.
- Significant damage from some broaching or fretting is present in the bore.
- The pin bore exceeds the specifications for new parts.
Inspection Procedure
Complete the following steps to inspect the pin bore.
- Clean the pin bore thoroughly before inspecting.
Pin bores and pins can be cleaned with cleaner for parts and a surface reconditioning pad that will not remove metal.
- Visually inspect the bore for damage and wear.
Note: An adequate light source is necessary to inspect pin bores. An optical magnifier may also be used.
- Inspect the bore with a seal pick to detect any wear steps.
Refer to Table 5 for a summary of the specifications of the pin bores.
Reference: , SEBF8163Reuse and Salvage Guidelines, "Procedures to Salvage Thrust Faces on Planetary Carriers".
Summary of the Final Drive Planetary Carrier Pin Bore Tolerances
Illustration 14 | g06319011 |
Typical example of an internal planetary carrier with in bores on a dual plane. (A) Pin Bore |
Final Drive Internal Planetary Carriers Pin Bore Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
|||
---|---|---|---|---|
Part Number | Tolerance
(A) |
Measurement | Measurement | Measurement |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = |
(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Illustration 15 | g06319028 |
Typical example of an external planetary carrier with in bores on a dual plane. (B) Pin Bore |
Final Drive External Planetary Carriers Pin Bore Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
|||
---|---|---|---|---|
Part Number | Tolerance
(B) |
Measurement | Measurement | Measurement |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = | |
|
A1 = | A2 = | A3 = |
(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Illustration 16 | g06319051 |
Typical example of a planetary carrier with pin bores on a single plane. (C) Pin Bore |
Final Drive Planetary Carrier Pin Bore (Single Plane) Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
|||||
---|---|---|---|---|---|---|
Part
Number |
Fit
Limit (2) |
Tolerances
(C) |
Measurement | Measurement | Measurement | |
Minimum | Maximum | |||||
H8 | |
|
A1 = | A2 = | A3 = | |
— | Reference |
— | A1 = | A2 = | A3 = | |
H8 | |
|
A1 = | A2 = | A3 = |
(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
(2) | Limits and Fit Tolerances per ISO 286. |
Reusability of Gearing
Accurate inspection is critical for the life of any gear. The maximum life of any drive train can be obtained through proper inspection and repair procedures. If an unacceptable gear is reused, then there is a good possibility that the gear will fail. The gear that failed will destroy other components in the drive train. The technician that is inspecting should be familiar with all types of gear wear and damage. The most common reasons for gear failure are described in this guideline. Decisions regarding reuse and salvage of gears are aided in thorough inspections.
Note: Some gearing applications run in one direction. Thus wear should only occur on one side of the gear. If the inspection suggests that a gear is worn, then flipping the gear may be an option thus using the other side of the tooth. Most likely application of gear flipping will be to those gears that have symmetrical features.
Visual Inspections - Use the following general examples as a guide to inspect for the following common wear types, defects, critical part locations, and features:
- Abrasive & Adhesive Wear
- Uneven Wear Patterns
- Corrosion
- Cracks
- Wear Steps
- Fretting
- Scoring, Dings, Dents, or Other Damage
Reference: SEBF8193 Reuse and Salvage Guidelines, "Reusability of Drive Train Gears" for more detailed information regarding general gear inspection.
Reference: Channel1, "Gear Tooth Inspection" https://channel1.mediaspace.kaltura.com/media/Gear+Tooth+Inspection/1_5ujdi5zp for a video representation of general gear inspection.
Dimensional Checks - Refer to the "Measurement Techniques" section before dimensional checks are performed. Refer to each components illustration and table of dimensions and acceptable tolerances to inspect for excessive wear. In addition to these dimensional inspections, each part must also pass one of the Non-Destructive Testing (NDT) methods listed in the "Crack Detection Methods" section.
Gear Inspection Examples
Illustration 17 | g06085440 |
(A) Tooth Face
(B) Fillet Area |
Check fillet area (B) with a seal pick. Fillet area (B) must be free from notches or wear steps.
Note: If steps are found in the fillet area of a gear tooth, then DO NOT USE THE PART AGAIN.
Illustration 18 | g03427659 |
Typical example of a gear inspection using reflective paper. |
Utilize a clean, white piece of paper with a dull finish that to reflect light onto the face of each gear tooth during an inspection.
Illustration 19 | g06085442 |
Illustration of view through eye piece of a pocket microscope. |
If necessary use a microscope with light for enhanced view and to measure the defects. Refer to Tooling Table 3 for the part number.
Minor abrasive wear (C) may indicate that there is contamination in the gear case. Once the source of contamination has been found then, OK TO USE PART AGAIN.
Illustration 20 | g06033556 |
Typical example of a planetary gear with evidence of corrosion (D), OK TO USE THIS PART AGAIN. (D) Corrosion |
The presence of corrosion (D) may be due to contamination or as a result of the process used to clean the part. Identify the source of corrosion (D), then OK TO USE PART AGAIN.
Illustration 21 | g06033582 |
Typical example of spalling (E) on tooth face, DO NOT USE PART AGAIN. (E) Spalling |
Illustration 22 | g06033587 |
Typical example of pitting (F) on tooth surface, DO NOT USE PART AGAIN. (F) Pitting |
Illustration 23 | g03708114 |
Typical example of crack shown under Liquid Penetrant Testing (PT) of a gear, DO NOT USE THIS PART AGAIN. Refer to the "Liquid Penetrant Testing (PT)" section for testing instructions. |
Illustration 24 | g06085444 |
Typical example of cracks found using Wet Magnetic Particle Testing (MPT), DO NOT USE THIS PART AGAIN. Refer to the "Wet Magnetic Particle Testing (MPT)" section for testing instructions. |
Planetary Gear Bore Inspections
Illustration 25 | g03427695 |
Typical example of a planetary gear that requires further inspection of the bore. |
Illustration 26 | g06008970 |
Typical example of brinelling found during a planetary gear bore inspection, DO NOT USE THIS PART AGAIN. |
Inspect planetary gear bore for pitting, heat cracks, and brinelling. If pitting, heat cracks, or brinelling are found on the planetary gear bore then, DO NOT USE PART AGAIN.
Complete Steps 1 through 4 to inspect the planetary gear bore:
Illustration 27 | g06026642 |
Typical example of cleaning a planetary gear bore. After cleaning a planetary gear bore, OK TO USE THIS PART AGAIN. (G) Planetary gear bore before cleaning. (H) Planetary gear bore after cleaning. |
- Clean the planetary gear bore thoroughly before inspecting.
Note: Planetary gear bores can be cleaned with cleaner for parts and a nonmetallic pad for rubbing that will not remove metal.
- Visually inspect the planetary gear bore for damage and wear.
Note: An adequate light source is necessary to inspect planetary gear bore. An optical magnifier may also be used.
- Inspect the planetary gear bore with a seal pick to detect any wear steps.
- Perform Wet Magnetic Particle Testing (MPT). Refer to the "Wet Magnetic Particle Testing (MPT)" section for testing instructions.
Reusability of the Final Drive Planetary Gears
The planetary gears are heavily loaded in final drive. All gears must meet the given standards. Refer to Reuse and Salvage Guideline, SEBF8193, "Reusability of Drive Train Gears" for additional information on final drive gears.
Planetary Gear Bore Reusability
Planetary gears with bores that function as a bearing outer race require special attention to the presence of corrosion or damage from foreign materials.
Extreme Pressure (EP) lubricants can cause corrosion. These lubricants are not recommended for use in Caterpillar final drives.
Check the bores of all planetary gears for other surface defects (cracks, pits, and so on).
Refer to Table 7 for the tolerances for reusability of the final drive planetary gear bores.
Illustration 28 | g06322321 |
Typical example of stains on the surface of the gear bore. |
If stains can be removed from the gear bore surface with reconditioning pad, USE THIS PART AGAIN.
If pitting are found in the stained areas, then DO NOT USE GEAR AGAIN.
Illustration 29 | g06322341 |
Typical example of corrosion pitting on the gear bore. Due to surface pitting, DO NOT USE THIS PART AGAIN. The pitting will progress into spalling. |
Illustration 30 | g06322347 |
Wash board texture and appearance on surface of the gear bore is called "Brinelling", DO NOT USE THIS PART AGAIN. |
Summary of Final Drive Planetary Gear Bore Tolerances
Illustration 31 | g06318873 |
Typical example of planetary gear bore (D) measurement. (D) Bore |
Final Drive Planetary Gear Bore Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Reusability of Planetary Shafts
Illustration 32 | g06320721 |
Typical example of a slip fit shaft with minor fretting, OK TO USE THIS PART AGAIN. |
Fretting may occur on the contact surface of the shaft and carrier. Shafts can be reused if less than 50% of the contact width and 25% of the shaft diameter is affected. A shaft diameter in question should be measured and compared with the manufacturer's specifications.
Illustration 33 | g06319268 |
Fretting on a planetary shaft. |
If the shaft meets all other specifications, USE THIS PART AGAIN.
Refer to Table 8 for the dimensional tolerances for reusability of the planetary shaft.
Summary of the Planetary Shafts Tolerances
Illustration 34 | g06318906 |
Typical example of planetary shaft measurements. (E) Width (F) Length |
Planetary Shafts Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Illustration 35 | g06369426 |
Typical example of planetary shaft measurement of part number |
Planetary Shafts Tolerances
Part Number |
Record Actual Dimensions
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Illustration 36 | g06369452 |
Typical example of planetary shaft measurement of part number |
Planetary Shafts Tolerances
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Reference |
Final Drive Spindle Spline and Hub Reusability
General Guidelines for Inspection of Splines
The spindles and splines must be inspected prior to any repair. These splines are subject to high loads. This makes accurate inspection essential. Splines should be inspected immediately after removal. If the splines are not immediately inspected, hydraulic oil should be applied to each machined surface to prevent rust or corrosion. If spline on spindle is cracked, DO NOT USE AGAIN.
Always use proper lifting devices for the safety of the operator and to prevent damage to the machined surface. Personal protective Equipment (PPE) should be worn always for the operator's protection.
Signs of Potential Failure
The key element to analyzing damage on final drive splines is determining if the damage will progress to a failure before the next Planned Component Rebuild (PCR). The application and size of splines are important in determining if the damage will progress.
There are two typical signs of failure:
- Spline wear or fracture from misalignment
- Cracking from fatigue which could lead to fracture
Spline Wear and Misalignment
Spline wear is the result of relative motion between mating spline teeth. High loading, insufficient lubrication, vibration, and abrasive materials may result in wear. Typically, splines can be reused if less than a
There is normally a small amount of relative motion between mating spline teeth. Uneven contact patterns on teeth of the splines are the result of misalignment of one or both of the mating splines. The spline teeth will not fully engage if the teeth are misaligned. This means that only a portion of each tooth is carrying the full load. Misalignment of teeth causes high contact pressures on the portion of the tooth that carries the load. The damage on the surface that is caused by these conditions is spline wear and fretting. Misalignment can be identified by the uneven contact pattern on the spline teeth.
Misalignment of the spline can be caused by worn bearings, damaged bearings, bores of the carrier, faces of the carrier, or shafts. If any spline displays uneven contact patterns, be sure to check for misalignment and correct the problem.
Misaligned splines can be reused if the splines meet the specifications for reusability.
Cracks on Spline Teeth from Fatigue
Numerous broken spline teeth may be the result of failure from bending fatigue. The operational loads create tensile stress in the fillet on the loaded side of the tooth. With enough high loads and cycles, these stresses can cause cracks from fatigue. A crack from fatigue could cause a tooth to separate from the parent metal. Cracking can also occur between the root of the tooth and a bolt hole or inside diameter of the part.
Visual Inspection
Splines can be visually inspected. To ensure the best results, a magnifying glass and a strong light source such as sunlight are recommended. It can also be difficult to distinguish between small scratches and small cracks. If unable to determine scratches from hair line cracks, then perform Liquid Penetrant Testing (PT) or Wet Magnetic Particle Testing (MPT).
Ensure to inspect all spline. If damaged spline is found, all spline that mate to it and all splines that are 180° from the damaged spline should be reinspected for possible fatigue from bending. Refer to "Crack Detection Methods" section for Non-Destructive Testing (NDT) procedures.
If spline is damage from misalignment, then DO NOT USE AGAIN. Abnormal wear will not permit full tooth contact thus result in high contact pressures.
Illustration 37 | g01716065 |
Typical example of check spline for wear steps with a seal pick. |
If the splines stop the seal pick on the worn area, measure the splines before reusing. Generally, a
Typically spline can be reused if step measures less than
Normal Wear
If spline has no significant wear (J) steps, then OK TO USE THIS PART AGAIN.
Illustration 38 | g01240327 |
Internal spline with full contact and even wear, OK TO USE THIS PART AGAIN. |
Illustration 39 | g01240340 |
Spline shows signs of even loading and full contact, OK TO USE THIS PART AGAIN. |
Illustration 40 | g01240365 |
The spline has an external wear step, but the spline meets specifications for reusability. Corrosion from fretting is also apparent. This corrosion is due to lack of lubrication, OK TO USE THIS PART AGAIN. |
Wear Steps
Illustration 41 | g06122439 |
Typical example of an internal spline with significant wear (L) steps, DO NOT USE AGAIN. (L) Wear |
Illustration 42 | g06319105 |
Check the ends of location of the engagement of the splines. |
If wear steps are found on either external or internal splines, drag a seal pick across the step. If the wear step stops the pick and measures more than
Remember to check the ends of the location of the engagement of the splines. If splines are not worn evenly, DO NOT USE THE PART AGAIN. Check mating spline for alignment.
Corrosion and Pitting
Illustration 43 | g06324680 |
Typical example of corrosion from poor storage techniques, clean inspect for pitting. If excessive pitting, then DO NOT USE THIS PART AGAIN. |
Damage to Teeth
Illustration 44 | g06324678 |
Typical example of spline damage from poor handling, but no signs of cracking. Use a polishing stone to smooth any raised material from the indentation, OK TO USE THIS PART AGAIN. |
Illustration 45 | g06324674 |
Typical example of spline damage from poor handling with a sign of cracking. Use a polishing stone to smooth any raised material from the indentation. If evidence of crack after removal of raised material, then DO NOT USE THIS PART AGAIN. |
Illustration 46 | g01240382 |
A spline is cracked in the area of the root and the crack has progressed into the adjacent splines, DO NOT USE THIS PART AGAIN. |
Crack from Fatigue on Spindles
Illustration 47 | g06324684 |
Typical example of a crack extending from the spline into the bolt hole. The bolt hole is weakened and premature failure will result, DO NOT USE THIS PART AGAIN. |
Illustration 48 | g06324686 |
Typical example of a crack in the root of the spline tooth, DO NOT USE THIS PART AGAIN. |
Spline Wear Measurement Procedures
Internal Spline
Illustration 49 | g06321306 |
Typical wear step on an internal spline. |
Illustration 50 | g06075213 |
Typical example of taking an internal spline measurement. |
Illustration 51 | g06181320 |
(G) 1, (G) 2, and (G) 3 Measurement Locations |
The location of the gage pins at 60° intervals is critical to the formula. These three locations will provide information about the wear of the part. Refer to Illustration 51.
An inside micrometer must be positioned to measure the shortest distance points on the gage pins. This procedure will provide the measurement of the wear on the spline. The gage pin diameter for each individual part is determined by the size and pitch of the spline.
Calculate the average of the values taken from locations (G) 1, (G) 2, and (G) 3. The difference between the measurements will determine if there is an out of round condition caused by poor load distribution on the splines.
Place gage pins at 60° intervals on the planetary carrier. The location of the gage pins at 60° intervals is critical to the formula. These three locations will provide information about the wear of the part.
Steps 1 through 4 demonstrate an example of the process to calculation internal spline roundness. Provided is an example of performing spline reusability calculations of a reaction hub part number
- Take measurements at locations (G) 1, (G) 2, and (G) 3 between gage pins. Taken measurements are recorded in Table 11.
Show/hide table
Table 11 994 Wheel Loader Reaction Hub ( 137-8628 ) Internal Spline
Example of Recording 3 Measurements TakenLocation Measurements Taken G1 Ø 465.705 mm (18.3348 inch) G2 Ø 465.920 mm (18.3433 inch) G3 Ø 466.180 mm (18.3535 inch) - Add the measurements together to calculate the sum. The sum of the three measurements is
1397.805 mm (55.0316 inch) .Show/hide tableTable 12 994 Wheel Loader Reaction Hub ( 137-8628 ) Internal Spline
Example of Calculating Sum of 3 Measurements TakenMeasurement
LocationsCalculation SUM Total = G1, G2, and G3 G1 + G2 + G3 1397.805 mm (55.0316 inch) - Divide the sum of the measurements taken by 3 to calculate the average. The calculated average of
465.935 mm (18.3439 inch) is less than the reusability specification of466.167 mm (18.3530 inch) . In this example the internal spline is within the reusability specification and therefore passes this test, proceed to Step 4.If the internal spline is greater than the reusability specification, then DO NOT USE THE PART AGAIN.
Show/hide tableTable 13 994 Wheel Loader Reaction Hub ( 137-8628 ) Internal Spline
Example of Calculating Average of the 3 Measurements TakenLocation Calculations Results G1, G2, and G3 (G1 + G2 + G3) / 3
= AvgØ 465.935 mm (18.3439 inch) Refer to Specifications in Table 20. Reusability
SpecificationØ 466.17 mm (18.353 inch) Avg Specification Avg > Reusability Specification = Fail
Avg < Reusability Specification = PassAvg = Ø 465.935 mm (18.3439 inch) < than Reusability Specification ofØ 466.17 mm (18.353 inch)
Pass - The difference between the high measurement and the low measurement determines if the spline is round. Out-of-round or ovality can cause uneven load distribution on the splines. Calculate the difference between the high and the low measurement by subtracting the high measurement of
Ø 466.180 mm (18.3535 inch) from the low measurement ofØ 465.705 mm (18.3348 inch) . The difference between the high and low measurements determine if the spindle can be reused. The difference in this example is0.475 mm (0.0187 inch) .Maximum difference between the high measurement and the low measurement allowance of
0.47 mm (0.019 inch) and the actual difference of0.475 mm (0.0187 inch) is greater than the allowable maximum difference.If the maximum difference between the high measurement and the low measurement is greater than
0.47 mm (0.019 inch) the internal spline is considered to be out-of-round or oval shaped and not reusable, DO NOT USE THE PART AGAIN.Show/hide tableTable 14 994 Wheel Loader Reaction Hub ( 137-8628 ) Internal Spline
Example of Determining the Difference from the 3 Measurements TakenLocation Calculations Results G1 Low Ø 465.705 mm (18.3348 inch) G2 Mid Ø 465.920 mm (18.3433 inch) G3 High Ø 466.180 mm (18.3535 inch) G3 - G1 High and Low
Difference =0.475 mm (0.0187 inch) Refer to Specifications in Table 20. Maximum
Difference
Allowance0.47 mm (0.019 inch) Actual Difference (H - L) Maximum Difference Allowance Actual Difference < Maximum Difference Allowance = Fail
Actual Difference > Maximum Difference Allowance = PassActual Difference = 0.475 mm (0.0187 inch) < than Maximum Difference Allowance of0.47 mm (0.019 inch)
Fail
External Spline
Illustration 52 | g06321303 |
Typical wear step on an external spline. |
Illustration 53 | g06322365 |
Typical example of using a straight edge to measure a wear step on a spline tooth. |
If possible, use a straight edge and a feeler gauge to measure questionable spline wear.
Illustration 54 | g01716121 |
Typical example of a wear step. A |
Illustration 55 | g06075290 |
Typical example of taking a Measurement Over Pins (MOP). |
Illustration 56 | g06181327 |
(L) 1, (L) 2, and (L) 3 Measurement Locations |
The location of gage pins at 60° intervals is critical to the formula. These three locations will provide information about the wear of the part. Refer to Illustration 56.
Note: For odd splines take measurement as close to 180° from each gage pin as possible.
Place gage pins at 60° intervals on the spline. Take the measurements over gage pins that are located approximately 180° away from each other.
A micrometer must be positioned to measure the highest external points on the gage pins. This procedure will provide the measurement of the wear of the spline. The gage pin diameter for each individual part is determined by the size and pitch of the spline. Calculate the average from the values taken. The difference between the measurements will determine if there is an out of round condition caused by poor load distribution on the splines.
Steps 1 through 4 demonstrate an example of the process to calculation external spline roundness. Provided is an example of performing spline reusability calculations of a spindle part number
NOTICE |
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The spline must pass the roundness tests by meeting the reusability specification measurement over gage pins and the maximum difference between the high and low measurements to be reused again. |
- Take measurements at locations (L) 1, (L) 2, and (L) 3 over gage pins. Taken measurements are recorded in Table 15.
Show/hide table
Table 15 990 Series II Wheel Loader Spindle ( 131-1296 ) External Spline
Example of Recording 3 Measurements TakenLocation Measurements Taken L1 Ø 299.000 mm (11.7716 inch) L2 Ø 298.900 mm (11.7677 inch) L3 Ø 298.800 mm (11.7638 inch) - Add the measurements together to calculate the sum. The sum of the three measurements is
896.700 mm (35.3031 inch) .Show/hide tableTable 16 990 Series II Wheel Loader Spindle ( 131-1296 ) External Spline
Example of Calculating Sum of 3 Measurements TakenMeasurement
LocationsCalculation SUM Total = L1, L2, and L3 L1 + L2 + L3 896.700 mm (35.3031 inch) - Divide the sum of the measurements taken by 3 to calculate the average. The calculated average of
298.900 mm (11.7677 inch) is greater than the reusability specification of298.781 mm (11.7630 inch) . In this example the external spline is within the reusability specification and therefore passes this test, proceed to Step 4.If the external spline is less than the reusability specification, then DO NOT USE THE PART AGAIN.
Show/hide tableTable 17 990 Series II Wheel Loader Spindle ( 131-1296 ) External Spline
Example of Calculating the Average of 3 Measurements TakenLocation Calculations Results L1, L2, and L3 (L1 + L2 + L3) / 3
= AvgØ 298.900 mm (11.7677 inch) Refer to Specifications in Table 19. Reusability
SpecificationØ 298.781 mm (11.7630 inch) Avg Specification Avg < Reusability Specification = Fail
Avg > Reusability Specification = PassAvg = Ø 298.900 mm (11.7677 inch) > than Reusability Specification ofØ 298.781 mm (11.7630 inch)
Pass - The difference between the high measurement and the low measurement determines if the spline is round. Out-of-round or ovality can cause uneven load distribution on the splines. Calculate the difference between the high and the low measurement by subtracting the high measurement of
Ø 299.000 mm (11.7716 inch) from the low measurement ofØ 298.800 mm (11.7638 inch) . The difference between the high and low measurement determine if the spindle can be reused. The difference in this example is0.200 mm (0.0079 inch) .Maximum difference between the high measurement and the low measurement allowance of
0.30 mm (0.012 inch) and the actual difference of0.200 mm (0.0079 inch) is less than the allowable maximum difference.If the maximum difference between the high measurement and the low measurement is greater than
0.30 mm (0.012 inch) the external spline is considered to be out-of-round or oval shaped and not reusable, DO NOT USE THE PART AGAIN.Show/hide tableTable 18 990 Series II Wheel Loader Spindle ( 131-1296 ) External Spline
Example of Determining the Difference from the 3 Measurements TakenLocation Calculations Results L1 High Ø 299.000 mm (11.7716 inch) L2 Mid Ø 298.900 mm (11.7677 inch) L3 Low Ø 298.800 mm (11.7638 inch) L1 - L3 High and Low
Difference =0.200 mm (0.0079 inch) Refer to Specifications in 19. Maximum
Difference
Allowance0.30 mm (0.012 inch) Actual Difference (H - L) Maximum Difference Allowance Actual Difference > Maximum Difference Allowance = Fail
Actual Difference < Maximum Difference Allowance = PassActual Difference = 0.200 mm (0.0079 inch) < than Maximum Difference Allowance of0.30 mm (0.012 inch)
Pass
Methods of Securing Gage Pins
Illustration 57 | g06075262 |
Typical example of MOP. (N) Rubber Band (P) Gage Pins |
Note: Rubber band (N) can be used to secure gage pins (P) in place when taking measurements of external splines. Refer to Illustration 57.
Illustration 58 | g06124082 |
Typical example of a magnetizer/ demagnetizer. |
NOTICE |
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If gage pins are magnetized, then demagnetize after use. When a gage pin is magnetized, cuttings and iron powder will easily stick to the surface, thus precipitating wear. |
Gage pins can be magnetized to aid in taking measurements between or over gage pins. Ensure that gage pins are demagnetized after use and stored properly.
Spline Summary of Dimensions for Reusability
Illustration 59 | g06321299 |
Typical example of taking a Measurement Over Pins (MOP) (A) of spindle spline. (A) Measurement Over Pins (MOP) |
Spindle Spline Dimensions and Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Part Number | Gage Pin Diameter | Original Specification
Measurement Over Gage Pins |
Reusability Specification
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Maximum Difference
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Illustration 60 | g06321308 |
Typical example of taking a measurement between pins (B) of a reaction hub spline. (B) Measurement Between Pins |
Internal Reaction Hub Spline Dimensions and Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Assembly
Part Number |
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Number |
Gage Pin Diameter | Original Specification
Measurement Between Gage Pins |
Reusability Specification
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Maximum Difference
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Measurement |
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Illustration 61 | g06369821 |
Typical example of taking a measurement between pins (B) of a reaction hub spline. Note: Typical example of a reaction hubwithout bearing journal. (B) Measurement Between Pins |
Internal Reaction Hub Spline Dimensions and Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Part Number | Gage Pin Diameter | Original Specification
Measurement Between Gage Pins |
Reusability Specification
Measurement Between Gage Pins |
Maximum Difference
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Measurement |
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Illustration 62 | g06321309 |
Typical example of taking a Measurement Over Pins (MOP) (C) of a reaction hub spline. (C) Measurement Over Pins (MOP) |
External Reaction Hub Spline Dimensions and Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Assembly
Part Number |
Part
Number |
Gage Pin Diameter | Original Specification
Measurement Over Gage Pins |
Reusability Specification
Measurement Over Gage Pins |
Maximum Difference
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Measurement |
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Illustration 63 | g06369827 |
Typical example of taking a Measurement Over Pins (MOP) (C) of a reaction hub spline. Note: Typical example of a reaction hub without bearing journal. (C) Measurement Between Pins |
External Reaction Hub Spline Dimensions and Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Part Number | Gage Pin Diameter | Original Specification
Measurement Over Gage Pins |
Reusability Specification
Measurement Over Gage Pins |
Maximum Difference
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Wheel Bearing Bore and Bearing Journal Reusability
Illustration 64 | g06321257 |
Typical example of outboard bearing (8) placement variations. Note: The outboard bearing placement is on the spindle of the final drive wheel group on left versus the hub on the right. (1) Spindle (3) Hub (8) Outboard Bearing |
The placement of the outboard wheel bearings can be on the hub or spindle. Inspect the spindle and hub bearing journals and the bearing bores of the wheel for wear at each rebuild.
NOTICE |
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If the bearing journal or bore has significant wear, the bearings will fit loosely and will cause premature failure of the components. |
Bearing Journal and Bore Inspections
- Start with a visual inspect of all bearing journal and bores. Bearing bores and journals can be inspected with the naked eye. To provide the best results, a magnifying glass and a strong light source such as sunlight are recommended. Check each component for cracks, bruising, scratching, or spalling. It can also be difficult to distinguish between small scratches and small cracks. In these cases, perform Wet Magnetic Particle Testing (MPT) or Liquid Penetrant Testing (PT), refer to the "Crack Detection Methods" section.
- After passing visual/ Non-Destructive testing, then measure the bearing journal and bores to ensure that the component meets the criteria for reusability in Table 24 through Table 26.
- If any defects are present, DO NOT USE PART until the component is salvaged. The component can be used after performing the applicable salvage procedure.
Spindle and Hub Bearing Journal Wear Limits
The outboard bearings are positioned on the spindle in two different ways. The outboard bearings are positioned on the spindle, or the hub which is then mounted to the spindle. If the bearing is mounted to the hub, the spindle should still be checked for wear in locations where contact locations with the hub. If the spindle has wear characteristics, thermal spray may be used to salvage the spindle. Refer to the "References" section for applicable information regarding thermal spray. Refer to Table 24 for part number-specific outer diameter dimensions of spindles.
Spindle Bearing Journal Tolerances
Note: Refer to the "References" section for applicable information regarding thermal spray.
Illustration 65 | g06320902 |
Typical example of a spindle. (A) Bearing Journal (B) Spindle Journal |
Spindle Outside Diameter Tolerance (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Part Number | Tolerance
(A) |
Tolerance
(B) |
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Reaction Hub Bearing Journal Tolerances
Note: Refer to the "References" section for applicable information regarding thermal spray.
Illustration 66 | g06320923 |
Typical example of a reaction hub. (C) Bearing Journal |
The reaction hub shown in Illustration 66 is designed with a bearing journal (C). When inspecting this design, the hub and the spindle should be inspected and measured. The hub must meet specifications for new parts and the hub must have no abrasive wear or adhesive wear. If the reaction hub does not meet the required conditions, the hub can be reworked by use of thermal spray and machining. Refer to Table 25 for tolerances of reaction hub bearing journal.
Reaction Hub Bearing Journal Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Assembly
Part Number |
Part
Number |
Tolerance
(C) |
Measurement | Measurement | Measurement |
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Wheel Bearing Bore Tolerances
Determine the maximum allowable wear of the bore of the bearing cup of the wheel assembly with the following procedure:
- Measure the Inside Diameter (ID) of the bearing bores of the wheel. Refer to the "Measurement Techniques" section.
- Refer to Table 26 to verify that the measurement is within the specifications.
- If there is significant wear or the bore is not within the specifications, the wheel must be replaced or salvaged. To salvage the bore of the wheel, refer to the "References" section for applicable thermal spray options.
Illustration 67 | g06321589 |
Typical example of a wheel. (D) Inboard Bearing Bore (E) Outboard Bearing Bore |
Wheel Bearing Bore Tolerances (1) | Record Actual Dimensions
Refer to the "Measurement Techniques" section for the proper techniques and number of measurements to be taken. |
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Assembly
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Part
Number |
Inboard
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Outboard
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(1) | Note: The most current part number is identified in bold font when multiple part numbers are in a cell. |
Crack Detection Methods
NOTICE |
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Regardless of which crack detection method is used, it is important that the instructions furnished with the detection equipment are followed closely when checking any component. Failure to do so may cause inaccurate results or may cause injury to the operator and/or surroundings. |
There are five major crack detection methods or Non-Destructive Testing (NDT) listed in this section: Visual Surface Inspection (VT), Liquid Penetrant Testing (PT), Dry / Wet Magnetic Particle Testing (MPT), and Ultrasonic Testing (UT).
Crack detection methods or NDT is methods for testing components for cracks without damaging the component. VT, PT, Dry/ Wet MPT, and UT are methods recommended. There may be more than one acceptable crack detection method for the testing of a given part, although PT is the most versatile. For example, the PT method can be used when testing smooth machined components such as shafts, gear teeth, and splines, but using the Wet MPT is more accurate. Refer to Table 27 for advantages and disadvantages and Table 28 for standards and requirements for these NDT methods.
Crack Detection Methods Advantages vs. Disadvantages | ||
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Detection Method | Advantages | Disadvantages |
Visual Surface Inspection (VT) | - Least Expensive
- Detects most damaging defects. - Immediate Results - Minimum part preparation |
- Limited to surface-only defects.
- Requires inspectors to have broad knowledge of welding and fabrication in addition to Non-Destructive Testing (NDT). |
Liquid Penetrant Testing (PT) | - Inexpensive
- Minimal Training - Portable - Works on nonmagnetic material. |
- Least Sensitive
- Detects surface cracks only. - Rough or porous surfaces interfere with test |
Dry Magnetic Particle (MPT) | - Portable
- Fast/Immediate Results - Detects surface and subsurface discontinuities |
- Works on magnetic material only.
- Less sensitive than Wet Magnetic Particle Testing (MPT). |
Wet Magnetic Particle (MPT) | - More sensitive than Liquid Penetrant Testing (PT).
- Detects subsurface as much as |
- Requires power for light.
- Works on magnetic material only. - Liquid composition and agitation must be monitored. |
Ultrasonic Testing (UT) | - Most Sensitive
- Detects deep material defects. - Immediate Results - Wide range of materials and thickness can be inspected |
- Most Expensive
- Requires operator training and certification. - Surface must be accessible to probe |
Applicable Crack Detection Standards | |||
---|---|---|---|
Detection Method | Standard | Acceptance
Criteria |
Minimum
Required Personnel Qualifications |
Visual Surface Inspection (VT) | EN-ISO 5817
AWS D1.1 |
EN-ISO 5817 - Level B
AWS D1.1 - Table 6.1 |
EN-ISO 9712
ANSI-ASNT SNT-TC-1A |
Liquid Penetrant Testing (PT) | EN-ISO 3452
ASTM E165 |
EN-ISO 23277
AWS - D1.1 |
EN-ISO 9712
ANSI-ASNT SNT-TC-1A |
Magnetic Particle Testing (MPT) | EN-ISO 17638
ASTM E709 |
EN-ISO 23278 - Level 1
AWS D1.1 - Table 6.1 |
EN-ISO 9712
ANSI-ASNT SNT-TC-1A |
Ultrasonic Testing (UT) | EN-ISO 17640 - Level B
AWS D1.1 |
EN-ISO 11666 Technique 2 - Level 2
AWS D1.1 - Class A - Table 6.3 |
EN-ISO 9712
ANSI-ASNT SNT-TC-1A |
Visual Surface Inspection (VT)
Illustration 68 | g06124166 |
Example of Visual Surface Inspection (VT) Tooling (A) Flashlight (or adequate light source) (B) Magnifying Glass (C) Tape Measure (or other measuring device) (D) Inspection Mirror |
Refer to Tooling and Equipment Table 3 for part numbers.
Components and welds that are to be tested using PT, MPT, or UT shall first be subject to a Visual Surface Inspection (VT). VT is often the most cost-effective inspection method and requires little equipment as seen in Illustration 75. Personnel performing VT shall either be trained to a company standard or have sufficient experience and knowledge regarding the components being inspected. Personnel performing VT shall take routine eye exams.
Liquid Penetrant Testing (PT)
Personal injury can result from improper handling of chemicals. Make sure you use all the necessary protective equipment required to do the job. Make sure that you read and understand all directions and hazards described on the labels and material safety data sheet of any chemical that is used. Observe all safety precautions recommended by the chemical manufacturer for handling, storage, and disposal of chemicals. |
Materials and Equipment Required
Refer to Tooling and Equipment Table 3 for part numbers.
- Cleaner: Removes dirt before dye application and dissolves the penetrant making possible to wipe the surface clean.
- Penetration Oil: This solution is highly visible, and will seep into openings at the surface of a part with capillary action.
- Developer: Provides a blotting action, bringing the penetrant out of the discontinuities and providing a contrasting background to increase the visibility of the penetrating oil indications.
- Wire Brush: Removes dirt and paint.
- Cloth or Wipes: Use with cleaner and for other miscellaneous uses.
Procedure
- Preclean the area to be tested. Spray on cleaner/ remover to loosen any scale, dirt, or any oil. Wipe the area to be tested with a solvent dampened cloth to remove remaining dirt and allow the area to dry. Remove paint where there are visible cracks using paint remover or a wire brush.
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Illustration 70 g06084053 Typical example of applying penetrating oil to areas to be tested. - Apply penetrating oil by spraying to the entire area to be tested. Allow 10 to 15 minutes for penetrating oil to soak. After the penetrating oil has been allowed to soak, remove the excess penetrating oil with clean, dry wipe.
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Illustration 71 g06084060 Typical example of removing penetrating oil with a cloth. - The last traces of penetrating oil should be removed with the cleaner solvent dampened cloth or wipe. Allow the area to dry thoroughly.
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Illustration 72 g06084070 Typical example of applying the developer. - Before using developer, ensure that the developer is mixed thoroughly by shaking the container. Hold the container approximately
203 - 305 mm (8 - 12 inch) away from part. Apply an even, thin layer of developer over the area being tested. A few thin layers are a better application method than one thick layer.Show/hide tableIllustration 73 g03773759 Typical example of cracks found during Liquid Penetrant Testing (PT). - Allow the developer to dry completely for 10 to 15 minutes before inspecting for cracks. Defects will show as red lines in white developer background, refer to Illustration 73. Clean the area of application of the developer with solvent cleaner.
Illustration 69 | g06084048 |
Typical example of pre-cleaning the testing area. |
Dry Magnetic Particle Testing (MPT)
Materials and Equipment Required
Refer to Tooling and Equipment Table 3 for part numbers.
Illustration 74 | g06085930 |
(A) Indications shown by Dry Magnetic Particle Testing (MPT).
(B) Electromagnetic Yoke (C) Dry Powder Bulb |
- Dry magnetic powder shall be of high permeability and low retentively and of suitable sizes and shapes to produce magnetic particle indications. The powder shall be of a color that will provide adequate contrast with the background of the surface being inspected.
- Dry magnetic particles shall be stored in suitable containers to resist contamination such as moisture, grease, oil, non-magnetic particles such as sand, and excessive heat. Contaminants will manifest in the form of particle color change and particle agglomeration. The degree of contamination will determine further use of the powder.
- Dry magnetic powder shall be tested in accordance with ASTM E709 Section 18 (Evaluation of System Performance/Sensitivity) when not performing.
- Equipment should include a "U" shaped electromagnetic yoke made from highly permeable magnetic material, which has a coil wound around the yoke. This coil carries a magnetizing current to impose a localized longitudinal magnetic field into the part. The magnetizing force of the yoke is related to the electromagnetic strength and can be tested by determining the lifting power of a steel plate. The yoke shall have a lifting force of at least
4.5 kg (10 lbs) . - Check dry powder blower routinely to ensure that the spray is a light, uniform, dust-like coating of the dry magnetic particles. Blower should also have sufficient force to remove excess particles without disturbing those particles that are evidence of indications.
- All equipment shall be inspected at a minimum of once a year or when accuracy is questionable.
Procedure
- Ensure surface to be inspected is dry and free from oil, grease, sand, loose rust, mil scale, paint, and other contaminants.
- Apply the magnetic field using the yoke against the faces and inside diameter of each bore.
- Simultaneously apply the dry powder using the dry powder blower.
- Remove excess powder by lightly blowing away the dry particles.
- Continue around the entire circumference of each bore. Position the yoke twice in each area at 1.57 rad (90°) to ensure that multiple directions of the magnetic field are created.
- Observe particles and note if any clusters of particles appear revealing an indication.
- Record the size and shape of any discontinuities or indications found.
Wet Magnetic Particle Testing (MPT)
Materials and Equipment
Refer to Tooling and Equipment Table 3 for part numbers.
Illustration 75 | g06085937 |
(A) Indications shown by Wet Magnetic Particle Testing (MPT).
(B) Electromagnetic Yoke (D) Ultraviolet Lamp |
Illustration 76 | g06003178 |
Pear Shaped Centrifuge Tube |
- Wet magnetic particles are fluorescent and are suspended in a vehicle in a given concentration that will allow application to the test surface by spraying.
- Concentration:
- The concentration of the suspended magnetic particles shall be as specified by the manufacturer and be checked by settling volume measurements.
- Concentrations are determined by measuring the settling volume by using an ASTM pear shaped centrifuge tube with a
1 mL (0.034 oz) stem with0.05 mL (0.0017 oz) divisions, refer to Illustration 76. Before sampling, the suspension shall be thoroughly mixed to assure suspension of all particles, which could have settled. A100 mL (3.40 oz) sample of the suspension shall be taken and allowed to settle for 30 minutes. The settling volume should be between0.1 mL (0.0034 oz) and0.25 mL (0.0085 oz) in a100 mL (3.40 oz) sample. - Wet magnetic particles may be suspended in a low viscosity oil or conditioned water.
- The oil shall have the following characteristics:
- Low viscosity not to exceed
5 mm2/s (5 cSt) at any temperature at which the vehicle is to be used. - Low inherent fluorescence and be non-reactive.
- Low viscosity not to exceed
- The conditioning agents used in the conditioned water shall have the following characteristics:
- Impart good wetting characteristics and good dispersion.
- Minimize foaming and be non-corrosive.
- Low viscosity shall not exceed a maximum viscosity of
5 mm2/s (5 cSt) at38° C (100° F) . - Non-fluorescent, non-reactive, and odorless.
- Alkalinity shall not exceed a pH of 10.5.
- Equipment should include a "U" shaped electromagnetic yoke made from highly permeable magnetic material, which has a coil wound around the yoke. This coil carries a magnetizing current to impose a localized longitudinal magnetic field into the part. The magnetizing force of the yoke is related to the electromagnetic strength and can be tested by determining the lifting power of a steel plate. The yoke shall have a lifting force of at least
4.5 kg (10 lbs) .
Procedure
- Ensure surface to be inspected is dry and free from oil, grease, sand, loose rust, mil scale, paint, and any other contaminants.
- Apply the magnetic field using the yoke against the surface in the area to be inspected.
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Illustration 77 g03536210 - For case hardened and ground surfaces:
- Due to the sensitivity required to locate the grinding cracks, inspection of case hardened and ground surfaces require that the yoke is applied so that the magnetic field is 1.57 rad (90°) to the expected direction of the indications. Also, due to the increased sensitivity resulting when the yoke is energized, the yoke is not moved until the evaluation is completed in the first direction. An AC yoke shall be used. See Illustration 77 for an example of yoke placement.
- Visually inspect for indications of discontinuities using the proper illumination.
- Record the size and shape of any discontinuities found.
Ultrasonic Testing (UT)
Note: Crack depth cannot be accurately determined by UT, only full depth cracking can be consistently determined. For cracks that are not full depth, an indication of a partial depth cracks can be detected by an experienced technician. Refer to Table 28 for crack detection standards.
Refer to Tooling and Equipment Table 3 for part numbers.
- Ultrasonic Testing (UT) is a method of Non-Destructive Testing (NDT) using short ultrasonic pulse waves (with frequencies from 0.1-15 MHz up to 50 MHz) to detect the thickness of the object. Ultrasonic testing consists of an ultrasound transducer connected to a diagnostic machine and passed over the object being inspected.
- There are two methods of receiving the ultrasound waveform from the transducer: reflection and attenuation.
- Reflection - Ultrasonic pulses exit the transducer and travel throughout the thickness of the material. When the sound waves propagate into an object being tested, the waves return to the transducer when a discontinuity is discovered along the sonic path. These waves continue and reflect from the back surface of the material to project the thickness of the material.
- Attenuation - A transmitter sends ultrasound through one surface, and a separate receiver detects the amount that has reached it on another surface after traveling through the medium. Any discontinuities or other conditions within the medium will reduce the amount of sound transmitted, revealing the presence of the imperfections.