Reuse and Salvage Guideline for Cracks in Hydraulic Cylinder Rod Assemblies {0599, 0738, 5102, 7562} Caterpillar


Reuse and Salvage Guideline for Cracks in Hydraulic Cylinder Rod Assemblies {0599, 0738, 5102, 7562}

Usage:

794 AC HRT
Mining Truck
794 AC (S/N: HRT1-UP)
Off-Highway Truck/Tractor
794 AC (S/N: MN51-UP)
796 (S/N: HRZ1-UP)
MT4400D AC (S/N: MH41-UP)

Introduction

Table 1
Revision  Summary of Changes in M0098963 
00  New Document. 

© 2018 Caterpillar All Rights Reserved. This guideline is for the use of Caterpillar 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 guideline enables dealers and dealer customers to benefit from cost reductions made possible through an established parts reusability and salvage program. Every effort has been made to provide the most current information known to Caterpillar Inc. Since the company makes ongoing product changes and product improvements, this guideline must be used with the latest technical information. Using the latest technical information available from Caterpillar ensures that such changes and improvements are incorporated where applicable.

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 not include canceled part numbers and replaced part numbers. Use NPR on SIS for information about canceled part numbers and replaced part numbers. NPR will provide the current part numbers for replaced parts.

Important Safety Information



Illustration 1g02139237

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 the procedure is safe for you and for other people to use. Ensure that the product will not be damaged or be made unsafe by the operation, lubrication, maintenance, or the repair procedures that are used.

------ WARNING! ------

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 danger, warning, or caution. The "WARNING" safety alert symbol is shown below.



Illustration 2g00008666

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.

Safety

------ WARNING! ------

Sudden movement of the machine or release of oil under pressure can cause injury to persons on or near the machine.

To prevent possible injury, perform the procedure that follows before testing and adjusting the steering system.


------ WARNING! ------

Personal injury can result from hydraulic oil pressure and hot oil.

Hydraulic oil pressure can remain in the hydraulic system after the engine has been stopped. Serious injury can be caused if this pressure is not released before any service is done on the hydraulic system.

Make sure all of the attachments have been lowered, oil is cool before removing any components or lines. Remove the oil filler cap only when the engine is stopped, and the filler cap is cool enough to touch with your bare hand.


------ WARNING! ------

Rerodding, straightening, or welding any steering cylinder rod, bowl cylinder rod, or front suspension cylinder rod could result in injury or death. If any of these rods are broken or cracked, the rods must be replaced with a REMAN rod or a new rod. These rods can be ground and plated with chrome if the recommended Caterpillar process that is identified in this document is used.



NOTICE

Care must be taken to ensure that fluids are contained during performance of inspection, maintenance, testing, adjusting, and repair of the product. Be prepared to collect the fluid with suitable containers before opening any compartment or disassembling any component containing fluids.

Refer to Special Publication, PERJ1017, "Dealer Service Tool Catalog" for tools and supplies suitable to collect and contain fluids on Cat® products.

Dispose of all fluids according to local regulations and mandates.


Summary



Illustration 3g06359290
Piston Seal Groove Cracks

Some 431-5865 Rod As assembly tubes may exhibit cracking in the corners of the piston seal groove. These cracks require repair before the part may be placed back into service. This Reuse & Salvage Guideline will provide one method of salvage.

References

Table 2
Media Number  Title 
SEBF8072  Reuse and Salvage Guideline,"Inspection and Salvage of Hydraulic Cylinder Components" 
REHS2689  "Hydraulic Cylinder Honing" 
PECJ0003  "Hand Tools and Shop Supplies" 

Tooling and Equipment

Table 3
Required Tooling and Equipment 
Part Number  Description  Designation 
(1)  Clevis/ Shackle  Component
Repositioning
and Movement 
(1)  Lifting Eye Assemblies  Component
Repositioning
and Movement 
(1)  Tool (Cribbing)  Component
Repositioning
and Movement 
—  Suitable Lifting Device  Component
Repositioning
and Movement 
1U-7262  Telescoping Magnet  General Tooling 
1U-9367  Automatic Tape Measure
25.4 mm x 8 m
(1 inch x 26 ft) 
Measurement
Checks 
5P-3920  Tool
Rule
304.8 mm (12.00 inch) 
Measurement
Checks 
8H-8581  Feeler Gauge
0.038 - 0.635 mm
(0.0015 - 0.0250 inch) 
Thickness
Measurement
Checks 
367-9109  Caliper (Digital)
0 -150 mm
(0 - 6.0 inch) 
Measurement
Checks 
385-9422  Tools (Micrometer)
Internal
(2 - 24 inch) 
Internal
Measurement
Checks 
386-3364  Tool (Ruler)
1,000.0 mm (39.37 inch) 
Measurement
Checks 
423-4373  Caliper - Digital
0 - 200 mm (0 - 8 inch) 
Measurement
Checks 
431-4150  Micrometers
External
0 - 25 mm (0 - 1 inch) 
External
Measurement
Checks 
473-8688
or
473-8689 
Instrument Group
Micrometer, Inside
2.00 - 12.00 inch 
Internal
Measurement
Checks 
Instrument Group
Micrometer, Inside
50 - 300 mm
473-8690  Instrument Group
Micrometer, Outside
0.00 - 4.00 inch 
External
Measurement
Checks 
473-8691  Instrument Group
Micrometer, Outside
2.00 - 6.00 inch 
External
Measurement
Checks 
473-8692  Instrument Group
Micrometer, Outside - Digital
152.4 - 304.8 mm (6.00 - 12.00 inch) 
External
Measurement
Checks 
474-3709
or
474-3710 
Instrument Group
Micrometer, Inside
(8.00 - 32.00 inch) 
Internal
Measurement
Checks 
Instrument Group
Micrometer, Inside
200 - 800 mm
385-8484  Level
305 mm (12 inch) 
Level 
—  Straight Edge  Flatness/
Straightness
Checks 

and /or
— 
GO/NO-GO Thread Gauge Set, Metric  Threaded Hole
Inspection 
GO/NO-GO Thread Gauge Set, SAE
(1)  Plastic Plug Assortment  Threaded Hole
Protection 
(1)  Tap and Die Set  Threaded Hole
/ Restore 
1U-5516  Disc (Coarse)  Surface
Preparation
/ De-burring 
1U-5518  Threaded Shaft  Surface
Preparation
/ De-burring 
1U-5519  Holder (Disc Pad)  Surface
Preparation
/ De-burring 
4C-8514  Wheel
(2 x 1 inch)
(60 Grit) 
Surface
Preparation
/ De-burring 
4C-8515  Grinding Wheel (F-Grade)
(2 x 1 inch)
(120 Grit) 
Surface
Preparation
/ De-burring 
222-3076  Die Grinder
(Right Angle) 
Surface
Preparation
/ De-burring 
254-5319  Brush
76.2 x 50.8 mm
(3.00 x 2.00 inch) 
Surface
Preparation
/ De-burring 
9U-7377  Metal Marking Pen  Parts Marking 
Contact Sunnen  E-mail:
Sunnen@Sunnen.com
Website:
www.sunnen.com 
Cylinder Honing 
Cylinder Tube ID
Measurements
8T-5096  Tool Group
Dial Indicator 
Run-Out Checks 
5P-7414  Seal Pick
Kit 
Seal Removal 
237-5181  Respirator (2)  Grinding PPE 
6V-6035  Hardness Tester  Hardness Checks 
9A-1593  Comparison Gauge (Surface Texture)  Surface Texture
Tester 
453-5376  Tool - Specimen  Surface Texture
Tester 
448-3698  Indicator
(Profilometer) 
Surface Texture
Tester 
8S-2257  Magnifying Glass  Visual Surface
Inspection (VT) 
9U-6182  Mirror (Telescoping)  Visual Surface
Inspection (VT) 
9U-7231  Flashing Lights Conversion Kit  Visual Surface
Inspection (VT) 
4C-9442  Flashlight - Standard  Visual Surface
Inspection (VT) 
(1)  Bright Incandescent Light  Visual Surface
Inspection (VT) 
262-8390  Microscope (40-Power)
Pocket 
Crack/
Measurement
Inspection 
288-4209  Paper Towel  Liquid Penetrant
Testing (PT) 
1U-9915  Curved Handle Wire Brush  General Cleaning/
Liquid Penetrant
Testing (PT) 
—  Developer  Liquid Penetrant
Testing (PT) 
4C-4804  Penetrating Oil  Liquid Penetrant
Testing (PT) 
—  Solvent Cleaner  General Cleaning/
Liquid Penetrant
Testing (PT) 
263-7184  Crack Detection Kit (Magnetic Particle)  Dry Magnetic
Particle Testing
(MPT) 
—  Paint Pen  Dry Magnetic
Particle Testing
(MPT) 
459-0184  Lamp Group
Ultraviolet 
Wet Magnetic
Particle Testing
(MPT) 
(1) Refer to Special Publication, NENG2500, "Dealer Service Tool Catalog" for suitable tooling.
(2) For use in North and South America, with exception of Brazil.

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.

Welding Specifications

Table 4
Preheat 
Preheat Temp °C (min)  20 
Method  Flame 
Interpass Temp °C (min)  20 
Interpass Temp °C (max)  300 
Base Materials 
Group #  Material Spec  Thickness 
SAE 1026  Up to 25 mm (0.984 inch) 
Filler Materials Gas/Flux 
Process  GMAW 
Electrode  ER70S-3 
Size  1.2 mm (0.047 inch) 
Shielding Gas  90/10 (ArCO2
Flow Rate (CFH)  40 - 45 
Electrode Stickout  5/8–3/4 inch 
Technique 
Bead Type  Stringer Bead 
Initial/Interpass Cleaning  Chip/Brush 
Other Notes  Travel speed of positioner should reuslt in a quality 6 - 8 mm (0.236 - 0.315 inch) fillet weld in one pass. 12 mm (0.47 inch) fillet weld will be completed in 3 passes. 
Position 
Position of Groove  1G - Flat  Fillet  2F - Hor 
Vertical Progression  Up  Down   

Crack Repair

  1. If a defect has already been found, proceed to Step 3.


    Illustration 4g06355577
    Piston Seal Groove Location

  2. Inspect the piston seal groove for cracks in the corners. Refer to Illustration 4. Use VT/PT or VT/MPT for this purpose. If cracks are found proceed to Step 3.

  3. Machine off the piston portion of the tube. Turn the outside diameter to 274.00 + 0.00 -0.05 mm (10.79 + 0.00 -0.002 inch), for a length of 136.0 + 5.0 - 0.00 mm (5.354 + 0.197 - 0.00 inch) from the end.

  4. Re-inspect the tube to ensure the cracks have been machined off. If cracks remain, the tube is not usable and must be scrapped.


    Illustration 5g06355625

    Table 5
    Dimension  Ring 1  Ring 2 
    33.25 ± 0.25 mm (1.31 ± 0.01 inch)  69.75 ± 0.25 mm (2.75 ± 0.01 inch) 
    304.75 ± 0.25 mm (12.0 ± 0.01 inch)  304.75 ± 0.25 mm (12.0 ± 0.01 inch) 
    274.0 ± 0.05 mm (10.79 ± 0.002 inch)  274.0 ± 0.05 mm (10.79 ± 0.002 inch) 
    15° ± 0.50°  15° ± 0.50° 

  5. Machine two rings from a low carbon steel such as cold drawn SAE1026. Refer to Illustration 5 for ring sizes.


    Illustration 6g06359301
    Weld Locations and Sizes

    Table 6
    Ring 1  136.65 ± 0.25 mm (5.38 ± 0.01 inch) 
    Ring 2  11.8 ± 0.89 mm (0.46 ± 0.035 inch) 

  6. Slide the two rings over the machined outside diameter. Ring 1 should go on first, then Ring 2. The chamfered faces should be positioned to the inside, facing each other. The square end of each ring should face toward either end of the tube.

  7. Position Ring 2 11.8 ± 0.89 mm (0.465 ± 0.035 inch) from the end of the tube. Clamp the ring to hold it in position and secure in place with a 12 mm (0.472 inch) fillet weld at the left edge. Refer to Illustration 6. Follow Reuse and Salvage Guideline , SEBD0512, "Caterpillar Service Welding Guide".

  8. Position Ring 1 136.65 ± 0.25 mm (5.38 ± 0.01 inch) from the end of the tube. Clamp the ring to hold it in position. This will create a bevel groove weld joint with a root opening. Use a 16.00 mm (0.63 inch) weld with full penetration to secure the rings to the tube. Refer to Illustration 6. Follow Reuse and Salvage Guideline , SEBD0512, "Caterpillar Service Welding Guide".


    Illustration 7g06369143
    New Piston Machine Features
    (AE) Perpendicularity
    (AF) Concentricity

    Table 7
    Location  Dimension 
    254.038 ± 0.038 mm (10.0015 ± 0.0015 inch) 
    279.3175 ± 0.0445 mm (10.9967 ± 0.00175 inch)(1)
    279.3745 ± 0.0255 mm (10.99897 ± 0.001 inch)(2) 
    135.125 ± 0.25 mm (5.32 ± 0.01 inch) 
    88.9 ± 0.25 mm (3.50 ± 0.01 inch) 
    65.02 ± 0.25 mm (2.56 ± 0.01 inch) 
    7.925 mm (0.312 inch) 
    38.42 ± 0.0635 mm (1.51 ± 0.0025 inch) 
    9.64 ± 0.0635 mm (0.38 ± 0.0025 inch) 
    3.2 µm (0.126 µin) Surface Texture 
    38.42 ± 0.0635 mm (1.51 ± 0.0025 inch) 
    9.65 mm (0.38 inch) 
    1.524 mm (0.06 inch) x 45° 
    R 0.381 mm (0.015 inch) 
    15° 
    1.6 µm (0.063 µin) Surface Texture 
    Ø 302.768 ± 0.05 mm (11.9 ± 0.002 inch) 
    Ø 264.236 ± 0.025 mm (10.403 ± 0.001 inch) 
    4.83 mm (0.19 inch) 
    16.0 ± 0.25 mm (0.63 ± 0.01 inch) 
    44.45 mm (1.75 inch) 
    R 4.85 ± 0.05 mm (0.191 ± 0.002 inch) 
    0.127 mm (0.005 inch) 
    0.051 mm (0.00201 inch) 
    AA  15° 
    AB  Ø 282.13 ± 0.0635 mm (11.11 ± 0.0025 inch) 
    AC  Ø 278.51 ± 0.127 mm (10.965 ± 0.005 inch) 
    AD  Ø 298.30 ± 0.05 mm (11.744 ± 0.002 inch) 
    Notes:  All radii to be 1.5 ± 0.5 mm (0.06 ± 0.02 inch), including in the seal groove corners. 
    (1) Before Plating
    (2) After Plating

  9. Machine the outside of the new piston to the dimensions shown in Illustration 7. Pay attention to the surface finish on the sealing groove.

    Note: The new piston seal groove shall have a radius of 1.5 ± 0.5 mm (0.059 ± 0.0197 inch) in the corners.

  10. Finish hone the bore to a surface finish of Ra = 0.1 - 0.3 microns and a bore size of 254.0 + 0.08 -0.00 mm (1.00 + 0.003 - 0.00 inch). Refer to Reuse and Salvage Guideline , REHS2689, "Hydraulic Cylinder Honing".

  11. Re-inspect all machined dimensions.

  12. Perform any other needed repairs to the tube such as chrome plating or polishing the outside diameter. Refer to Reuse and Salvage Guideline, SEBF8072, "Inspection and Salvage of Hydraulic Cylinder Components" for more salvage procedures.

Acceptance Criteria

Table 8
Defect Name  ISO 6520 Defect Reference No.  Remarks  Defect Limit 
Cracks-
Longitudinal, Transverse, Radiating, Crater, Disconnected, Branching 
1011, 1012, 1013, 1014, 1015, 1023, 1024, 1031, 103, 1034, 1045, 1046, 1047, 1051, 1053, 1054, 1061, 1063, 1064  Not permitted 
Crack - Transverse  1021  Hard surface welds only  Permitted 
Crack - Transverse  1021  Joining welds  Not Permitted 
Porosity  2011, 2012, 2014, 2017  Maximum Diameter for a single pore  1.0 mm (0.04 inch) 
Maximum pores in any 300 mm (11.8 inch) length of weld 6.0 mm (0.24 inch) 
Maximum number of pores in any 50 mm (2.0 inch) of weld length for welds less than 300 mm (11.8 inch) in length 1.0 mm (0.04 inch) 
Clustered Porosity  2013  Maximum length of cluster in any weld  3.0 mm (0.12 inch) 
Elongated Cavities  2015  Maximum height or width  3.0 mm (0.12 inch) 
Maximum length for any single discontinuity, and 25 mm (0.98 inch) 
Maximum length in any weld 10% of weld length 
Elongated Cavities  2016  Maximum Dimension of any single cavity  3.0 mm (0.12 inch) 
Maximum total length of affected area in any weld 10% of weld length to not exceed 25 mm (0.98 inch) 
Shrinkage Cavities  2021, 2024, 2025  Maximum diameter or length  1.0 mm (0.04 inch) 
Slag or Flux Inclusions  3011, 3012, 3014, 3021, 3022, 3024  Maximum height or width  1.0 mm (0.04 inch) 
Maximum length for any single discontinuity, and 25 mm (0.98 inch) 
Maximum length in any weld 10% of weld length 
Oxide Inclusions  3031, 3032, 3033  Maximum height or width  1.0 mm (0.04 inch) 
Maximum length for any single discontinuity, and 25 mm (0.98 inch)
Maximum length in any weld 10% of weld length
Puckering (Oxide Inclusion - Aluminum)  3034  Not permitted 
Metallic Inclusion  3041, 3041, 3043  Not permitted 
Lack of Fusion  4011, 4012, 4013  Visual (breaking the surface)  Not permitted 
Subsurface maximum height or width 1.0 mm (0.04 inch)
Subsurface maximum length for any single discontinuity, and 25 mm (0.98 inch)
Maximum length in any weld 10% of weld length
Lack of Penetration  402, 4021  Maximum reduced penetration  10% of nominal penetration not to exceed 1.0 mm (0.04 inch) 
Maximum allowed total length of reduced penetration 10% of weld length
Undercut  5011, 5012, 5013, 5014, 5015  Maximum depth measured from plate surface - any length  0.5 mm (0.02 inch) 
Excess Weld Metal - Groove Weld Reinforcement (Convexity)  502  Any length   
Weld face width 5.0 mm (0.20 inch) or less 1.0 mm (0.04 inch)
Weld face width over 5.0 mm (0.20 inch) but less than 10 mm (0.39 inch) 1.5 mm (0.06 inch)
Weld face width 10 mm (0.39 inch) to 20 mm (0.79 inch) 2.0 mm (0.08 inch)
Weld face width over 20 mm (0.79 inch) but less than 30 mm (1.18 inch) 3.0 mm (0.12 inch)
Weld face width 30 mm (1.18 inch), and over 4.0 mm (0.16 inch)
Excess Weld Metal - Fillet Weld Convexity  503  Convexity affects weld toe angle, reducing fatigue life  90° 
Weld toe angles of 135° and more are better
Defect limits expressed as minimum toe angles allowed
Excess penetration  5041, 5042, 5043  Without drawing limitation  2.0 mm (0.08 inch) (Any length) 
With "melt-thru" and "flush" weld symbols 1.0 mm (0.04 inch) (Any length)
With "melt-thru" and "grind flush" weld symbols Not permitted (after grinding)
Incorrect Weld Toe  505  When IE2995 (NEEDS EXPLAINING) applies (expressed as a weld toe radius rather than a toe angle)  3.0 mm (0.12 inch) minimum radius 
Overlap  5061, 5062  Expressed as minimum toe angle  90° 
Fillet Weld Leg Size - Undersize  Applies to either weld leg measured independent of the other 
Maximum undersize 1.0 mm (0.04 inch)
Maximum length of undersize weld 10% of total weld length if at least 10% of total weld length is at least 1.0 mm (0.04 inch) over nominal size. Otherwise, no undesize length is permitted
Fillet Weld Leg Size - Oversize  Applies to either weld leg measured independent of the other  +25% (max 3.0 mm (0.12 inch)
Maximum oversize
Conformance to design - Fillet weld leg sizes may be oversized (within defect limitations or beyond) without correction provided the excess does not interfere with satisfactory end use of the component (i.e. distortion, fit-up interference, etc.)
Fillet Weld - Linear Length when specified at less than the length of the joint  Weld size </= 6.5 mm (0.25 inch)  ± 6.5 mm (0.25 inch) 
Weld size > 6.5 mm (0.25 inch) ± 12.5 mm (0.49 inch)
Fillet Weld Throat Size - Undersize  5213  Nominal Size (.7 x Leg Size) not inclusive of penetration beyond the weld root  Not permitted 
Weld crater only - maximum undersize 2.0 mm (0.08 inch) MAX - and not to exceed 20% of specified throat, not inclusive of penetration beyond the weld root (.7 x Leg Size)
Incompletely Filled Groove Weld  511  Careful consideration needs to be given when plate mismatch is apparent  Not permitted 
Weld depth must be maintained as minimum
Root Concavity on Open Root Groove Welds  515, 5013  Maximum depth measured from plate surface or tube inner surface - any length  0.5 mm (0.02 inch) 
Poor Restart (Tie-In)  5171, 5172  Measured in terms of excess weld metal (Fillet weld convexity) or overlap on groove welds, lack of fusion, or insufficient throat 
Excess weld metal on fillet welds, defect limits expressed as minimum toe angles allowed 90°
Overlap on groove welds, defect limits expressed as minimum toe angles allowed
Lack of fusion - Visual maximum length per restart 3.0 mm (0.12 inch)
Insufficient weld throat Not permitted
Stray Arc Strike  601  Not permitted 
Slag Residue  615  SMAW, SAW, FCAW, GMAW  Not permitted 
GTAW Silicon residue permitted unless removal specified by drawing note

Table 9
Defect Name  ISO 6520 Defect Reference No.  Remarks  Defect Limit 
Combined Discontinuities  Total maximum combined length of all imperfections in a weld, expressed as a percent of total weld length  15% 
(No single type of imperfection can exceed the limits for that single type of imperfection)

Visual Surface Inspection (VT)



Illustration 8g06124166
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, or MPT 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 8. 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)

------ WARNING! ------

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.

  • Penetrating 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



    Illustration 9g06103795
    Typical example of pre-cleaning the testing area.

  1. 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.


    Illustration 10g06103803
    Typical example of applying penetrating oil to areas to be tested.

  2. Apply penetrant by spraying to the entire area to be tested. Allow 10 to 15 minutes for penetrant to soak. After the penetrating oil has been allowed to soak, remove the excess penetrating oil with clean, dry wipe.


    Illustration 11g06103816
    Typical example of removing penetrating oil with a cloth.

  3. The last traces of penetrating oil should be removed with the cleaner solvent dampened cloth or wipe. Allow the area to dry thoroughly.


    Illustration 12g06103820
    Typical example of applying the developer.

  4. Before using developer, ensure that the developer is mixed thoroughly by shaking the container. Hold the container approximately 203 - 305 mm (8.0 - 12.0 inch) away from the testing area. Apply an even, thin layer of developer over the testing area. A few thin layers are a better application method than one thick layer.


    Illustration 13g06084042
    Typical example of cracks found during Liquid Penetrant Testing (PT).

  5. Allow the developer to dry completely for 10–15 minutes before inspecting for cracks. Defects will show as red lines in white developer background, refer to Illustration 13. Clean the area of application of the developer with solvent cleaner.

Dry Magnetic Particle Testing (MPT)

Materials and Equipment Required

Refer to Tooling and Equipment Table 3 for part numbers.



Illustration 14g06085930
(A) Indications shown by Dry Magnetic Particle Testing (MPT).
(B) Electromagnetic Yoke
(C) Dry Powder Bulb

  1. 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.

  2. 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.

  3. Dry magnetic powder shall be tested in accordance with ASTM E709 Section 18 (Evaluation of System Performance/Sensitivity) when not performing.

  4. 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).

  5. 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.

  6. All equipment shall be inspected at a minimum of once a year or when accuracy is questionable.

Procedure

  1. Ensure surface to be inspected is dry and free from oil, grease, sand, loose rust, mil scale, paint, and other contaminants.

  2. Apply the magnetic field using the yoke against the faces and inside diameter of each bore.

  3. Simultaneously apply the dry powder using the dry powder blower.

  4. Remove excess powder by lightly blowing away the dry particles.

  5. 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.

  6. Observe particles and note if any clusters of particles appear revealing an indication.

  7. 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 15g06085937
(A) Indications shown by Wet Magnetic Particle Testing (MPT).
(B) Electromagnetic Yoke
(D) Ultraviolet Lamp


Illustration 16g06003178
Pear Shaped Centrifuge Tube

  1. 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.

  2. Concentration:

    1. The concentration of the suspended magnetic particles shall be as specified by the manufacturer and be checked by settling volume measurements.

    2. Concentrations are determined by measuring the settling volume by using an ASTM pear shaped centrifuge tube with a 1 mL (0.034 oz) stem with 0.05 mL (0.0017 oz) divisions, refer to Illustration 16. Before sampling, the suspension shall be thoroughly mixed to assure suspension of all particles, which could have settled. A 100 mL (3.40 oz) sample of the suspension shall be taken and allowed to settle for 30 minutes. The settling volume should be between 0.1 mL (0.0034 oz) and 0.25 mL (0.0085 oz) in a 100 mL (3.40 oz) sample.

    3. Wet magnetic particles may be suspended in a low viscosity oil or conditioned water.

    4. 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.

    5. 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) at 38° C (100° F).

      • Non-fluorescent, non-reactive, and odorless.

      • Alkalinity shall not exceed a pH of 10.5.

  3. 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

  1. Ensure surface to be inspected is dry and free from oil, grease, sand, loose rust, mil scale, paint, and any other contaminants.

  2. Apply the magnetic field using the yoke against the surface in the area to be inspected.


    Illustration 17g03536210

  3. 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 17 for an example of yoke placement.

  4. Visually inspect for indications of discontinuities using the proper illumination.

  5. Record the size and shape of any discontinuities found.

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