Differential Housing Components for Wheel Loaders, Articulated Trucks, Wheel Tractors, Compactors, Integrated Toolcarriers, and Motor Graders {3258, 3284} Caterpillar


Differential Housing Components for Wheel Loaders, Articulated Trucks, Wheel Tractors, Compactors, Integrated Toolcarriers, and Motor Graders {3258, 3284}

Usage:

44 06W
Articulated Truck
All
Integrated Toolcarrier
All
Landfill Compactor
816 (S/N: 57U1-UP)
816B (S/N: 15Z1-UP)
816F (S/N: 5FN1-UP; BMR1-UP)
816K (S/N: LT61-UP; SLL1-UP)
826B (S/N: 58U1-UP)
826C (S/N: 87X1-UP)
826G (S/N: 7LN1-UP)
826G Series II (S/N: AYH1-UP)
826K (S/N: 2L31-UP; 2T61-UP)
836G (S/N: BRL1-UP; 7MZ1-UP)
836K (S/N: T6X1-UP; L6Z1-UP)
Motor Grader
All
Soil Compactor
815 (S/N: 91P1-UP; 15R1-UP)
815B (S/N: 17Z1-UP)
815F (S/N: BKL1-UP; 1GN1-UP)
815K (S/N: SL91-UP; T1Y1-UP)
825B (S/N: 43N1-UP)
825G (S/N: 6RN1-UP)
825G Series II (S/N: AXB1-UP)
825K (S/N: 2L91-UP; 2T91-UP)
835 (S/N: 44N1-UP)
Wheel Dozer
814 (S/N: 90P1-UP; 14R1-UP)
814B (S/N: 16Z1-UP)
814F (S/N: BGF1-UP; 9DM1-UP)
814K (S/N: LW41-UP; T1Z1-UP)
824 (S/N: 29G1-UP)
824B (S/N: 36H1-UP)
824C (S/N: 85X1-UP)
824G (S/N: 4SN1-UP)
824G Series II (S/N: AWW1-UP)
824K (S/N: 2T21-UP; 2L41-UP)
834 (S/N: 43E1-UP)
834B (S/N: 7BR1-UP; 92Z1-UP)
834G (S/N: BPC1-UP; 6GZ1-UP)
834K (S/N: TW41-UP; L4Y1-UP)
844 (S/N: BBN1-UP; 2KZ1-UP)
844H (S/N: BTW1-UP)
844K (S/N: M4R1-UP; K4Y1-UP)
854G (S/N: AMP1-UP; A4W1-UP; 1JW1-UP)
854K (S/N: 2211-UP; KK61-UP; RM61-UP; H9K1-UP; H8M1-UP)
Wheel Loader
All
Wheel Tractor-Scraper
All

Introduction

Table 1
Revision  Summary of Changes in SEBF8119 
24  Added new serial number prefixes for New Product Introduction (NPI). 
23  Added new serial number prefixes for New Product Introduction (NPI).
Updated copyright date to 2018.
Added 1 part number. 
22  Removed sleeving verbiage. 
21  Added 7 part numbers. 
20  Added 8 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 NPR on SIS for information about canceled part numbers and replaced part numbers. NPR will provide the current part numbers for replaced parts.

Summary

The contents of this guideline discuss the reusability of components of the differential housing for differentials. The contents also provide dimensions of diameters to reuse bearing journals. Additional instructions for the salvage of repairable components will be contained in future individual guidelines. Differential housing assemblies can be salvaged by metal spraying pinion bores, bearing journals, axle bores, bearing shoulders, ring gear mounting faces, and split faces. Bolt hole damage and distortion in the flange half can be repaired by sleeving the bolt holes. The repair procedure in this guideline provides a method to salvage differential housings.

Several conditions can cause damage. For example, the differential housing bores can be damaged by foreign material or component failure. Damage to the differential housing can occur from bearing or gear failures. These failures can cause the bores of the housing to become elongated. Damage to the differential housing can also occur when subjected to extreme axial loads.

This guideline identifies the various areas that can be salvaged using the metal spray. The metal spray operation must be followed by precision machining and using dimensions provided in this guideline.

Differential housings that meet these salvage guidelines and specifications can be expected to perform normally in the same application. Never install a part that this guideline indicates cannot be used again. Before installing a used or reconditioned part, correct any condition that may have caused the original wear.

If you need dimensional information for a component that is not yet available or to report suspected errors, inaccuracies, or suggestions regarding the document, submit a form for feedback in the Service Information System (SIS Web) interface. Examples of gear wear are provided in this publication, but much more detailed description and information for analysis can be found in publication Reuse and Salvage Guideline, SEBF8193, "Reusability of Drive Train Gears".

This guideline contains the latest standards of engineering, which will help minimize owning and operating costs. A part can be expected to reach the next Planned Component Repair if the part meets the specifications in this guideline and if the part is used in the same application.

Do not operate or perform any lubrication, maintenance, or repair on this product until you have understood the operation, lubrication, maintenance, and repair information. If a part has met the specification in this guideline, the part can be expected to give normal performance until the next overhaul. The conditions apply when the part is used in the same application.

If this guideline shows a part that is not reusable, do not install the part. During reconditioning, correct any conditions that might have caused the original failure.

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 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.

------ 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 such as 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.

Service Letters and Technical Information Bulletins


NOTICE

The most recent Service Letters and Technical Information Bulletins that are related to this component shall be reviewed before beginning work. Often Service Letters and Technical Information Bulletins contain upgrades in repair procedures, parts, and safety information that pertain to the parts or components being repaired.


References

Table 2
References 
Media Number  Publication Type & Title 
SEBF8187  Reuse and Salvage Guideline , "Standardized Parts Marking Procedures" 
SEBF8193  Reuse and Salvage Guideline , "Reusability of Drive Train Gears" 
SEBF8227  Reuse and Salvage Guideline , "Salvage of Differential Housing Assembly used on 785, 789, and 793 Off-Highway Trucks" 
SEBF8728  Reuse and Salvage Guideline , "Specifications for Inspection of Drive-line Fasteners" 
SEBF9236  Reuse and Salvage Guideline , "Fundamentals of HVOF Spray for Reconditioning Components" 
SEBF9238  Reuse and Salvage Guideline, SEBF9238, "Fundamentals of Arc Spray for Reconditioning Components" 
SEBF9240  Reuse and Salvage Guideline , "Fundamentals of Flame Spray for Reconditioning Components" 

Tooling and Equipment


NOTICE

Failure to follow the recommended procedure or the specified tooling that is required for the procedure could result in damage to components.

To avoid component damage, follow the recommended procedure using the recommended tools.


Table 3 contains the items that are needed to complete the repair procedures in this guideline.

Table 3
Tooling and Equipment 
Part Number  Description 
1U-5512  Polishing Cloth / Emery Cloth 
1U-5519  Disc Pad Holder 
1U-5516  Discs (Coarse) 
1U-9918  Wire Brush 
1P-3537  Dial Bore Gauge Kit 
4C-4804  Penetrant 
4C-4805  Developer 
4C-8515  Flapper Wheel
(2" x 1" 120 grit) 
4C-8521  Wheel Adapter 
5P-1720  Seal Pick 
7M-7456  Bearing Mount Compound 
8S-2257  Eye Loupe 
8T-7765  Surface Reconditioning Pad 
9A-1593  Surface Texture Comparison Gauge 
9U-7377  Metal Marking Pen 
170-5903  Gear Inspection Stand 
222-3074  Die Grinder 
222-3076  Right Angle Die Grinder 
238-8244  White LED Pen Light 
263-7184  Crack Detection Kit 
269-3123  Blue LED Pen Light 
288-4209  Paper Towel 
367-9109  Digital Caliper 6 Inch 
385-9422  Inside Micrometer Set
2-24 inch 
448-3697
or
448-3698 
Profilometer
Bluetooth Feature 
Profilometer
Non-Bluetooth Feature
459-0184  UV Light Kit 
473-8688
or
473-8689 
Inside Micrometer Set
2-12 inch 
Inside Micrometer Set
50-300 mm
473-8690  Outside Electronic Micrometer Set
0-4 inch 
473-8691  Outside Electronic Micrometer Set
2-6 inch 

Preparation Before Inspection

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

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.


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

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 205 kPa (30 psi) for cleaning purposes.




Illustration 3g03721203
Typical burr removal tooling.
(A) Right Angle Die Grinder
(B) Die Grinder
(C) ( D) ( E) Conditioning Discs, Disc Pad Holder, and Threaded Shaft
(F) ( G) Flapper Wheels

  • Clean all surfaces for inspection before you inspect the part. Make sure that you remove all debris, paint, and oil.

  • When you move parts that require cleaning, always use a proper lifting device. This device must protect the part from damage. For the safety of the operator, all lifting devices must be inspected before use.

  • During cleaning, do not damage machined surfaces.

  • Use pressurized air to dry parts.

  • If the bore cannot be inspected immediately after cleaning, put hydraulic oil on all machined surfaces to prevent rust or corrosion. Carefully store the parts in a clean container.

  • Use appropriate thread taps to chase all threaded holes.

Preheat the base metal to a minimum of 21 °C (70 °F). Maintain the minimum temperature throughout the welding process.

Clean the area that will be welded. Make sure that the substances that follow are removed from the area that will be welded.

  • Oil

  • Grease

  • Paint

  • Dirt

All components need thoroughly cleaned prior to inspection to be sure that no damage is hidden by oil or dirt. Use a wash tank or a coarse bristle brush with a mild petroleum-based solvent. Be sure that the solvent does not have any water contamination. Also, never use a chlorinated solvent. Water or chlorine can cause corrosion on the surface from pitting. Pits cause areas of highly concentrated stress that are called stress raisers to occur. These areas are more likely to result in component failure.

The 8S-2257 Eye Loupe As and 5P-1720 Seal Pick are useful in the close inspection of irregularities on the surface of the component. Use a dye penetrant or other suitable equipment to check all components for cracks, and scrap any cracked parts. Emery cloth or abrasive sheets are used to remove surface rust, light fretting, or nicks from handling. When inspection is completed, be sure to maintain the cleanliness of all acceptable differential components and protect the components from moisture. If necessary, clean the parts again before reassembly.

Standardized Parts Marking Procedure

Reference: Refer to Reuse And Salvage Guideline, SEBF8187, "Standardized Parts Marking Procedures" for additional information regarding marking procedures.

The code is a Cat standard and is used to record the history of a gear. The code will identify the number of rebuilds and hours at the time of each rebuild. This information is important for any decision to reuse a gear. The information should be considered when deciding whether to reuse a gear. The information should be utilized for locating the cause of a failure.

The mark should be on the sides of planetary gears and sun gears. The mark should not be covered by a mating part. Use a Metal Marking Pen to mark the code onto the gear.


NOTICE

Do not use a numbering stamp punches set to mark internal parts. The impact from striking the stamp will cause an abnormal stress riser. The added stress riser may cause the part to fail prematurely.


The procedure for marking gears 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 4g03649157

Illustration 4 shows code (1-15). The first number (1) indicates that the component had been rebuilt once. The second number (15) indicates that there were 15,000 hours on the component at the time of rebuild.

Example 2



Illustration 5g03649151

Illustration 5 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 component had been rebuilt twice. The second number (10) indicates that 10,000 hours accumulated on the component between the first and second rebuild.

Note: To obtain the total number of hours for the component in Illustration 5, add first and second rebuild hours. In this example the component has a total of 22,000 hours.

Metal Spray

Metal spray is an acceptable method of restoring a surface to the original size. Each step in the procedure is critical in achieving the desired coating, bond, and surface finish. Refer to Reuse and Salvage Guideline, SEBF9236, "Fundamentals of HVOF Spray for Reconditioning Components", Reuse and Salvage Guideline, SEBF9238, "Fundamentals of Arc Spray for Reconditioning Components" and Reuse and Salvage Guideline, SEBF9240, "Fundamentals of Flame Spray for Reconditioning Components" for metal spray repair procedures.

Ring Gear and Pinion

On most machines, the ring and the pinion are serviced separately. However, if the ring and the pinion are a matched set, damage to either gear requires the installation of a new set.

Pitting of the Teeth

Start of Active Profile

If pitting of the teeth occurs on the ring gear and the pinion, the result is normally a line of small pits at the SAP (Start of Active Profile). The pitting starts first on the pinion, and then on the ring gear. See Illustration 7 through Illustration 9.



Illustration 6g03782670
Profile of gear tooth
(1) Start of Active Profile (SAP)
(2) Pitch line


Illustration 7g01363842
Slight indication of pitting at the SAP.

USE THE GEAR AGAIN



Illustration 8g01367967
Slight indication of pitting at the SAP.

USE THE GEAR AGAIN



Illustration 9g03782673
Slight indication of pitting at the SAP.

USE THE GEAR AGAIN

Pitch Line

Do not reuse gears with any pitting around the pitch line.

Sensor Gear



Illustration 10g03782675

Differential Spider Gears, Side Gears, and Pinions

Surfaces of the thrust face must be free of smearing, grooves, corrosion from pitting and any other mechanical damage that could act as a cutting edge against the bearing.



Illustration 11g01234759
The thrust face has shallow grooves.

DO NOT USE THE GEAR AGAIN



Illustration 12g01234768
Stains from rusting.

USE THE GEAR AGAIN

Part can be reused after removing the rust with a fine abrasive cloth.



Illustration 13g01234825
The thrust face has been grooved by abrasive particles.

DO NOT USE THE GEAR AGAIN



Illustration 14g01234832
The thrust face has been pitted by corrosion.

DO NOT USE THE GEAR AGAIN

Spider Shaft

No wear is permitted on spider shafts.

Differential Housing

Visually determine if the differential housing can be salvaged. Damage to machined bolt holes in the flange area may be repaired by enlarging the hole and installing a sleeve.



Illustration 15g03704110
Inspect all areas indicated by arrows for wear, dents, nicks, and other types of damage.

  • Check bolt hole depth using the bolt without the washer. The bolt must go completely through both parts with sufficient clearance for locknut, washer, and nut.

  • Check the housing for cracks.Do Not Use Again, If the housing is cracked.

  • Check housing for heat damage and distortion.

  • Check bore and outside diameter bearing surfaces for wear. If worn beyond recommended specification, repair the damage before using again.

Mounting Faces

Movement between the halves of the differential housing and between the ring gear and the housing causes the pieces to fret. Fretting refers to the wearing and transferring of metal between the pieces. Any parts that show fretting up to the amount in Illustration 16 can be reused after all high spots are removed. Face off the surface and build up the surface by thermal spray if the damage is deeper. Contact dealer support for dimensions for given parts.



Illustration 16g01234839
The damage from fretting on the mounting surface is not excessive. The damage from fretting on the mounting surface must not be more than the amount of damage that is shown here.

Use the differential housing again.

Bore of the Spider Shaft

Some fretting is permitted in this bore. See Illustration 17 for a typical example of acceptable fretting. The bores which are machined in the mounting face of the case may show fretting or wear beyond this point. The bores may then be built up using thermal spray and re-bored. This is done together with the mounting faces. Call Dealer Support to obtain this dimension for given housings.



Illustration 17g01234842
Typical example of acceptable fretting.

Use the differential housing again.

Side Gear and Pinion Thrust Faces

Do not reuse a housing if the thrust bearing has worn into the housing more than 0.5 mm (0.02 inch). See Illustration 18. No welding on the ductile iron differential half and surfaces that are worn beyond the maximum amount can only be metal sprayed.



Illustration 18g03782677
The thrust face does not have more than 0.5 mm (0.02 inch) wear.

Use the differential housing again.

The component is acceptable to be reused if the thrust face does not have more than 0.5 mm (0.02 inch) of wear.

Locating Dowel for the Thrust Bearing

Do not reuse a housing if the locating dowel is loose. See Illustration 19. Loose dowels will break during operation, which will permit the thrust bearing to turn. Housings with worn dowel holes can be salvaged by drilling a new hole in the other half of the housing or by boring the worn hole, plugging the hole with a steel rod, and drilling a new hole in the original location.



Illustration 19g01234855
Housing with loose locating dowel.

Use the differential housing again.

The hole for the locating dowel must be relocated or repaired to be reused.

Support Bearing Journals

The maximum amount of wear that is permitted on the outside diameter of the bearing journals that support the differential housing is shown in Table 4. Journals that are worn beyond this amount can be salvaged with metal spray. Bearings that will be used on journals that are smaller than the new diameter must be installed using 7M-7456 Bearing Mount Compound. Wear on the thrust face up to 0.25 mm (0.010 inch) can be machined. Thrust surfaces that are worn beyond 0.25 mm (0.010 inch) can be built up with welding or thermal spray and can be re-machined to the original dimensions that are provided in the charts.



Illustration 20g01234859
Excessive wear on the bearing journal that supports the differential housing.

Use the differential housing again.

The bearing journal that supports the differential housing must be repaired.



Illustration 21g03782678
Typical group for the differential housing.
(3) Flange
(4) Bearing journal on the plain end
(5) Bearing journal on the flange end

Table 4
Diameter of the Bearing Journal that Supports the Differential Housing 
Part Number  Part Description  Dimension 
6S-3026,
6S-7582 
differential case  75.044 ± 0.013 mm (2.9545 ± 0.0005 inch) 
4E-0699,
4E-0885 
differential housing  75.038 ± 0.015 mm (2.9543 ± 0.0006 inch) 
8R-6619,
9C-5348,
109-4717,
118-5025,
191-3576,
218-0766,
237-9201,
237-9202 
differential case  75.051 ± 0.015 mm (2.9548 ± 0.0006 inch) 
7V-2188,
9V-4330 
differential case  75.050 ± 0.015 mm (2.9547 ± 0.0006 inch) 
8R-2538,
9C-8161,
103-2010,
138-1612,
143-9513,
206-9670 
differential case  75.040 ± 0.015 mm (2.9543 ± 0.0006 inch) 
365-1300,
365-1301,
365-1302 
housing  80.00 ± 0.013 mm (3.1496 ± 0.0005 inch) 
differential housing
5T-1030,
8W-8740,
8W-9544 
flange half of the differential case  152.588 ± 0.02 mm (6.0074 ± 0.0008 inch) 
plain half of the differential case 152.512 ± 0.02 mm (6.0044 ± 0.0008 inch) 
8W-9543,
8X-0244,
104-4698,
124-6022 
flange half of the differential case  174.81 ± 0.02 mm (6.8823 ± 0.0008 inch) 
plain half of the differential case 152.588 ± 0.02 mm (6.0074 ± 0.0008 inch) 
203-2289,
282-1775 
flange half of the differential case  174.70 ± 0.02 mm (6.8779 ± 0.0008 inch) 
plain half of the differential case 150.056 ± 0.013 mm (5.9077 ± 0.0005 inch) 
8W-6757  flange half of the differential case  108.026 ± 0.02 mm (4.25298 ± 0.0008 inch) 
plain half of the differential case 85.80 ± 0.02 mm (3.378 ± 0.0008 inch) 
1V-6983,
5V-1272,
5V-5630,
5V-9322,
6W-1565,
6W-2968,
7V-7793,
8K-6507,
8K-7581,
8V-2958,
9K-5654,
9V-5725 
flange half of the differential case  82.625 ± 0.015 mm (3.2530 ± 0.0006 inch) 
plain half of the differential case
3K-4176,
1V-5085,
8K-5992,
9K-5650 
flange half of the differential case  82.601 ± 0.013 mm (3.252 ± 0.0005 inch) 
plain half of the differential case
141-3124,
279-5128 
flange half of the differential case  241.450 ± 0.025 mm (9.50569 ± 0.001 inch) 
plain half of the differential case 489.468 ± 0.025 mm (19.2704 ± 0.001 inch) 
271-1674,
289-8600,
289-8601 
flange half of the differential case  88.975 ± 0.015 mm (3.503 ± 0.0006 inch) 
plain half of the differential case 75.045 ± 0.015 mm (2.9545 ± 0.0006 inch) 
287-8222  gear half of the differential case  88.975 ± 0.015 mm (3.503 ± 0.0006 inch) 
reaction half of the differential case 85.045 ± 0.015 mm (3.3482 ± 0.0006 inch) 
287-8228  gear half of the differential case  117.565 ± 0.015 mm (4.6285 ± 0.0006 inch) 
reaction half of the differential case 95.05 ± 0.015 mm (3.7421 ± 0.0006 inch) 
8R-9737,
144-4464 
differential housing  88.977 ± 0.013 mm (3.5030 ± 0.0005 inch) 
cover for differential housing 85.057 ± 0.013 mm (3.3487 ± 0.0005 inch) 
6W-3413,
9C-9771,
106-6580 
flange half of the differential case  90.056 ± 0.015 mm (3.5455 ± 0.0006 inch) 
plain half of the differential case 82.625 ± 0.015 mm (3.2530 ± 0.0006 inch) 
326-0535,
385-1794,
508-8369 
flange half of the differential case  88.977 ± 0.015 mm (3.5030 ± 0.0006 inch) 
plain half of the differential case 85.057 ± 0.015 mm (3.3487 ± 0.0006 inch) 
2V-3954,
9C-8278 
flange half of the differential case  104.825 ± 0.015 mm (4.127 ± 0.0006 inch) 
plain half of the differential case 110.025 ± 0.015 mm (4.3317 ± 0.0006 inch) 
1V-5869,
3K-9516,
4V-4076,
7D-5013,
8S-6995 
flange half of the differential case  127.076 ± 0.015 mm (5.003 ± 0.0006 inch) 
plain half of the differential case 110.038 ± 0.013 mm (4.3322 ± 0.0005 inch) 
173-5349,
171-4736 
flange half of the differential case  110.038 ± 0.015 mm (4.3322 ± 0.0006 inch) 
plain half of the differential case
171-6760,
323-4150 
flange half of the differential case  95.038 ± 0.015 mm (3.7417 ± 0.0006 inch) 
plain half of the differential case
171-6763,
323-4151,
333-4622 
flange half of the differential case  95.038 ± 0.015 mm (3.7417 ± 0.0006 inch) 
plain half of the differential case 110.038 ± 0.015 mm (4.3322 ± 0.0006 inch) 
333-4623  flange half of the differential case  110.038 ± 0.015 mm (4.3322 ± 0.0006 inch) 
plain half of the differential case
4V-6451,
6K-5626 
flange half of the differential case  77.838 ± 0.013 mm (3.0645 ± 0.0005 inch) 
plain half of the differential case
8R-8503  flange half of the differential case  75.038 ± 0.015 mm (2.9543 ± 0.0006 inch) 
plain half of the differential case
252-7945,
256-1109,
256-3746,
258-2398,
265-9508,
265-9509 
differential case  85.80 ± 0.015 mm (3.3780 ± 0.0006 inch) 
4E-6104,
8R-7834,
8R-8142,
104-6746,
159-7446 
large diameter of differential case  96.913 ± 0.015 mm (3.8155 ± 0.0006 inch) 
small diameter of differential case 85.80 ± 0.015 mm (3.378 ± 0.0006 inch) 
211-0095  differential housing  50.00 ± 0.013 mm (1.9685 ± 0.0005 inch) 
9K-4911  cover for differential housing  82.6008 ± 0.013 mm (3.252 ± 0.0005 inch) 
9K-1394  cover for differential housing  77.8383 ± 0.013 mm (3.0645 ± 0.0005 inch) 
4E-3191,
104-6738 
half with the gear of the differential case  88.977 ± 0.013 mm (3.5030 ± 0.0005 inch) 
plain half of the differential case 85.057 ± 0.015 mm (3.3487 ± 0.0006 inch) 
2G-6020  half with the gear of the differential case  65.062 ± 0.020 mm (2.5615 ± 0.0008 inch) 
plain half of the differential case 85.065 ± 0.020 mm (3.3490 ± 0.0008 inch) 
8G-5405  half with the gear of the differential case  85.065 ± 0.020 mm (3.3490 ± 0.0008 inch) 
plain half of the differential case 90.061 ± 0.020 mm (3.5457 ± 0.0008 inch) 
8D-4300  half with the gear of the differential case  85.065 ± 0.020 mm (3.3490 ± 0.0008 inch) 
plain half of the differential case 100.0633 ± 0.020 mm (3.9395 ± 0.0008 inch) 
3K-3396  flange half of the differential case  82.6008 ± 0.013 mm (3.252 ± 0.0005 inch) 
plain half of the differential case
8W-5112
154-2688 
flange half of the differential case  80.037 ± 0.015 mm (3.1511 ± 0.0006 inch) 
plain half of the differential case 65.038 ± 0.015 mm (2.5606 ± 0.0006 inch) 
8K-7437,
9K-5643 
cover for differential housing  82.6008 ± 0.013 mm (3.252 ± 0.0005 inch) 
8R-9281,
8R-9440,
104-3359,
136-6550,
144-4465,
372-4788 
plain half of the differential case  88.977 ± 0.013 mm (3.5030 ± 0.0005 inch) 
half with the gear of the differential case 85.057 ± 0.013 mm (3.3487 ± 0.00051 inch) 
355-1143,
436-6569 
plain half of the differential case  85.057 ± 0.015 mm (3.3487 ± 0.0006 inch) 
half with the gear of the differential case 120.745 ± 0.015 mm (4.7537 ± 0.0006 inch) 
361-7764,
434-1446 
plain half of the differential case  90.055 ± 0.015 mm (3.5455 ± 0.0006 inch) 
half with the gear of the differential case 120.745 ± 0.015 mm (4.7537 ± 0.0006 inch) 
361-7768  plain half of the differential case  90.055 ± 0.015 mm (3.5455 ± 0.0006 inch) 
half with the gear of the differential case 110.065 ± 0.015 mm (4.3333 ± 0.0006 inch) 
355-1154  plain half of the differential case  85.057 ± 0.015 mm (3.3487 ± 0.0006 inch) 
half with the gear of the differential case 114.385 ± 0.015 mm (4.5033 ± 0.0006 inch) 
8R-8141,
8R-8336,
102-7507,
102-7519,
108-2836,
127-9096,
142-0444,
148-9288 
half with the gear of the differential case  114.385 ± 0.015 mm (4.5033 ± 0.0006 inch) 
plain half of the differential case 90.054 ± 0.015 mm (3.5454 ± 0.0006 inch) 
6K-7636  flange half of the differential case  104.851 ± 0.015 mm (4.128 ± 0.0006 inch) 
plain half of the differential case 110.052 ± 0.015 mm (4.3328 ± 0.0006 inch) 
2S-6286  cover for differential housing  110.038 ± 0.013 mm (4.3322 ± 0.0005 inch) 
5K-6694  cover for differential housing  104.826 ± 0.013 mm (4.127 ± 0.0005 inch) 
9U-0471,
105-4026 
flange half of the differential case  110.060 ± 0.015 mm (4.3331 ± 0.0006 inch) 
plain half of the differential case
105-8720,
112-7521,
112-7524,
129-4304,
130-1848,
135-7496,
159-5963,
208-7534,
372-4769,
386-0310,
387-4570 
flange half of the differential case  120.745 ± 0.015 mm (4.7537 ± 0.0006 inch) 
plain half of the differential case 110.06 ± 0.015 mm (4.3331 ± 0.0006 inch) 
1V-5868  gear half of the differential case  104.826 ± 0.013 mm (4.1270 ± 0.0005 inch) 
plain half of the differential case 110.038 ± 0.013 mm (4.3322 ± 0.0005 inch) 
8R-7922,
8R-7926,
9K-2939,
9V-9486 
flange half of the differential case  114.375 ± 0.015 mm (4.5029 ± 0.0006 inch) 
plain half of the differential case 117.550 ± 0.015 mm (4.6279 ± 0.0006 inch) 
9U-0113  flange half of the differential case  120.745 ± 0.015 mm (4.7537 ± 0.0006 inch) 
plain half of the differential case 117.565 ± 0.015 mm (4.6285 ± 0.0006 inch) 
137-8859  flange half of the differential case  139.8 ± 0.015 mm (5.5039 ± 0.0006 inch) 
plain half of the differential case 114.4 ± 0.015 mm (4.5039 ± 0.0006 inch) 
6W-8261,
120-0551,
358-7234 
flange half of the differential case  152.505 ± 0.015 mm (6.0041 ± 0.0006 inch) 
plain half of the differential case 139.810 ± 0.015 mm (5.5043 ± 0.0006 inch) 
242-8686,
367-2024 
flange half of the differential case  139.81 ± 0.015 mm (5.5043 ± 0.0006 inch) 
plain half of the differential case 114.4 ± 0.015 mm (4.5039 ± 0.0006 inch) 
1V-6318  flange half of the differential case  170.066 ± 0.020 mm (6.6955 ± 0.0008 inch) 
plain half of the differential case 133.426 ± 0.020 mm (5.2530 ± 0.0008 inch) 
8R-6188  flange half of the differential case  209.687 ± 0.015 mm (8.2554 ± 0.0006 inch) 
plain half of the differential case 174.762 ± 0.015 mm (6.8804 ± 0.0006 inch) 
4V-5391,
6W-1631,
105-2073,
129-6659,
149-0191 
flange half of the differential case  90.056 ± 0.015 mm (3.5455 ± 0.0006 inch) 
plain half of the differential case 85.050 ± 0.015 mm (3.3484 ± 0.0006 inch) 
2A-6708,
8V-9808 
plain half of the differential case  85.050 ± 0.015 mm (3.3484 ± 0.0006 inch) 
flange half of the differential case 110.088 ± 0.015 mm (4.3342 ± 0.0006 inch) 
8R-4769,
100-4504 
flange half of the differential case  127.076 ± 0.015 mm (5.0030 ± 0.0006 inch) 
plain half of the differential case 110.038 ± 0.015 mm (4.3322 ± 0.0006 inch) 
8K-9585  cover for differential housing  114.376 ± 0.013 mm (4.5030 ± 0.0005 inch) 
2S-0300,
7K-9308,
8K-7398 
flange half of the differential case  114.376 ± 0.013 mm (4.5030 ± 0.0005 inch) 
plain half of the differential case 133.426 ± 0.020 mm (5.2530 ± 0.0008 inch) 
4V-8733  flange half of the differential case  114.351 ± 0.013 mm (4.5020 ± 0.0005 inch) 
plain half of the differential case 117.526 ± 0.013 mm (4.6270 ± 0.0005 inch) 
8D-2669,
5V-2756 
flange half of the differential case  90.030 ± 0.013 mm (3.5445 ± 0.0005 inch) 
plain half of the differential case 85.0316 ± 0.013 mm (3.3477 ± 0.0005 inch) 
7V-9623  flange half of the differential case  90.069 ± 0.015 mm (3.5460 ± 0.0006 inch) 
plain half of the differential case 96.932 ± 0.015 mm (3.8162 ± 0.0006 inch) 
2G-2630,
4D-5630,
4D-5730,
6D-0736,
7D-7660,
8W-6756,
101-7513,
107-7857 
plain half of the differential case  133.469 ± 0.02 mm (5.2547 ± 0.0008 inch) 
flange half of the differential case 114.437 ± 0.021 mm (4.5053 ± 0.0008 inch) 
2G-9200,
6D-8531,
6G-7560,
6G-7565,
8D-5620 
flange half of the differential case  139.857 ± 0.02 mm (5.5062 ± 0.0008 inch) 
plain half of the differential case 133.4262 ± 0.02 mm (5.253 ± 0.0008 inch) 
3D-9561,
6D-8540 
flange half of the differential case  139.776 ± 0.02 mm (5.5030 ± 0.0008 inch) 
plain half of the differential case 133.4262 ± 0.02 mm (5.253 ± 0.0008 inch) 
376-3744,
386-0311,
449-2992 
plain half of the differential case  114.4 ± 0.015 mm (4.5039 ± 0.0006 inch) 
flange half of the differential case 120.745 ± 0.015 mm (4.7537 ± 0.0006 inch) 
273-9001  plain half of the differential case  130.125 ± 0.015 mm (5.1230 ± 0.0006 inch) 
half with the gear of the differential case 139.837 ± 0.015 mm (5.5053 ± 0.0006 inch) 
5D-5580,
8D-0180 
plain half of the differential case  115.1636 ± 0.02 mm (4.5340 ± 0.0008 inch) 
flange half of the differential case 110.0633 ± 0.02 mm (4.3332 ± 0.0008 inch) 
116-8235,
154-6622 
plain half of the differential case  110.0303 ± 0.02 mm (4.3319 ± 0.0008 inch) 
flange half of the differential case 139.837 ± 0.020 mm (5.5054 ± 0.0008 inch) 
8D-9890  half with the gear of the differential case  65.062 ± 0.020 mm (2.5615 ± 0.0008 inch) 
plain half of the differential case 70.061 ± 0.020 mm (2.7583 ± 0.0008 inch) 
8D-9890  half with the gear of the differential case  65.062 ± 0.020 mm (2.5615 ± 0.0008 inch) 
plain half of the differential case 70.061 ± 0.020 mm (2.7583 ± 0.0008 inch) 
8W-5587  plain half of the differential case  65.038 ± 0.015 mm (2.5606 ± 0.0006 inch) 
flange half of the differential case 70.038 ± 0.015 mm (2.7574 ± 0.0006 inch) 
416-4654  plain half of the differential case  139.81 ± 0.015 mm (5.5043 ± 0.0006 inch) 
flange half of the differential case 152.505 ± 0.015 mm (6.0041 ± 0.0006 inch) 
365-1781  reaction half of the differential case  110.038 ± 0.015 mm (4.3322 ± 0.0006 inch) 
gear half of the differential case 120.745 ± 0.015 mm (4.7537 ± 0.0006 inch) 
287-8261  lock half of the differential case  105.05 ± 0.015 mm (4.1358 ± 0.0006 inch) 
gear half of the differential case 120.745 ± 0.015 mm (4.7537 ± 0.0006 inch) 

Crack Detection Methods

Crack detection methods or Non-Destructive Testing (NDT) are utilized for examining components for cracks without damaging the component. Visual inspection, Liquid Penetrant Testing (PT), Magnetic Particle Testing (MT), Ultrasonic Testing (UT), Radiographic Testing and Eddy Current Testing are recommended methods. There may be more than one acceptable crack detection method for the inspection of a given part, though the liquid penetrant is the most versatile. For example, the liquid penetrant method can be used when inspecting smooth machined components such as shafts, gear teeth, and splines, but using the Wet Magnetic Particle Inspection is more accurate. Refer to Table 5 for advantages and disadvantages and Table 6 for standards and requirements for these NDT methods.

Table 5
Crack Inspection Method Advantages vs. Disadvantages 
Inspection 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 NDT 
Liquid Penetrant (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 (MT)  - Portable
- Fast/Immediate Results
- Detects surface and subsurface discontinuities 
- Works on magnetic material only
- Less sensitive than Wet Magnetic Particle 
Wet Magnetic Particle (MT)  - More sensitive than Liquid Penetrant
- Detects subsurface as much as 0.13 mm (0.005 inch) 
- Requires Power for Light
- Works on magnetic parts 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 
Eddy Current Testing (ET)  - Surface and near surface flaws detectable
-Moderate speed/Immediate results
-Sensitive too small discontinuities 
- Difficult to interpret
- Only for metals
-Rough surfaces interfere with test
- Surface must be accessible to probe 
Radiographic Testing (RT)  -Detects surface and internal flaws
- Minimum part preparation
- Can inspect hidden areas 
- Not for porous materials
- Radiation protection needed
- Defect able to be detected is limited to 2% of thickness 

Table 6
Applicable Crack Detection Standards 
Type  Standard  Acceptance
Criteria 
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 - Level 2
ANSI-ASNT SNT-TC-1A Level 2 
Liquid Penetrant Testing (PT)  EN-ISO 3452
ASTM E165 
EN-ISO 23277
AWS - D1.1 
EN-ISO 9712 - Level 2
ANSI-ASNT SNT-TC-1A Level 2 
Magnetic Particle Testing (MT)  EN-ISO 17638
ASTM E709 
EN-ISO 23278 - Level 1
AWS D1.1 - Table 6.1 
EN-ISO 9712 - Level 2
ANSI-ASNT SNT-TC-1A Level 2 
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 - Level 2
ANSI-ASNT SNT-TC-1A Level 2 
Eddy Current Testing (ET)  EN-ISO 15549
ASTM E426 
EN-ISO 20807  EN-ISO 9712 - Level 2
ANSI-ASNT SNT-TC-1A Level 2 
Radiographic Testing (RT)  EN-ISO 5579
ASTM E94 
EN-ISO 10657-1  EN-ISO 9712 - Level 2
ANSI-ASNT SNT-TC-1A Level 2 


NOTICE

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.


Visual Surface Inspection (VT)



Illustration 22g06085008
Example of Visual Inspection Tools
(A) Flashlight or adequate light source
(B) Magnifying eye loupe
(C) Tape measure or other measuring device
(D) Inspection mirror
(E) Weld size inspection gauges

Components and welds that are to be inspected using PT, MT, or UT shall first be subject to visual inspection (VT). Visual Inspection is often the most cost-effective inspection method and requires little equipment as seen in Illustration 22. It is suggested that at a minimum personnel performing Visual Inspection are either trained to a company standard or have sufficient experience and knowledge about the components being inspected. It is also suggested that personnel performing visual inspections take some type of eyesight test regularly.

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.

  • Penetrant: 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 penetrant indications.

  • Wire Brush: Removes dirt and paint.

  • Cloth or Wipes: Use with cleaner and for other miscellaneous uses.

Procedure



    Illustration 23g06087907
    Typical example of checking for cracks in the welded areas.

  1. Preclean inspection area. Spray on cleaner / remover to loosen any scale, dirt, or any oil. Wipe the area to inspect with a solvent dampened cloth to remove remaining dirt and allow the area to dry. If there is visible crack remove paint using paint remover or wire brush.


    Illustration 24g06087912
    Typical example of checking for cracks in the welded areas.

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


    Illustration 25g06087914

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


    Illustration 26g06087916

  4. Before using Developer, ensure that it is mixed thoroughly by shaking can. Hold can approximately 8-12 inches away from part, apply an even, thin layer of developer over the area being inspected. A few thin layers are a better application method than one thick layer.


    Illustration 27g06084042
    Typical example of cracks found during a liquid penetrant examination.

  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 27. Clean the area of application of the developer with solvent cleaner.

Dry Magnetic Particle Testing (MT)

Materials and Equipment Required

Refer to Tooling and Equipment Table 3 for part numbers.



Illustration 28g06085930
(A) Indications shown by magnetic particle testing.
(B) Typical 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 (MT)

Materials and Equipment

Refer to Tooling and Equipment Table 3 for part numbers.



Illustration 29g06085937
(A) Indications shown by magnetic particle testing.
(B) Typical electromagnetic yoke.
(D) UV Lamp used in wet magnetic particle inspection process.


Illustration 30g06003178
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) 1.0 mL (0.034 oz) divisions, refer to Illustration 30. 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 50 mSt (5.0 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 50 mSt (5.0 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 31g03536210

  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 31 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.

Ultrasonic Testing (UT)

Refer to Tooling and Equipment Table 3 for part numbers.


NOTICE

All personnel involved in ultrasonic examinations shall be qualified to Level 2 in accordance to standards stated in Table 6.


  1. 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.

  2. There are two methods of receiving the ultrasound waveform from the transducer: reflection and attenuation.

    a. 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.

    b. 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.

Eddy Current Testing



Illustration 32g06090873
Eddy Current testing


NOTICE

All personnel involved in Eddy Current examinations shall be qualified to Level 2 in accordance to standards stated in Table 6.


Eddy Current testing (ET) is a Non-Destructive Testing (NDT) method in which eddy-current flow is induced in the test object. Changes in the flow caused by variations in the specimen are reflected in to a nearby coil or coils for subsequent analysis by suitable instrumentation and techniques. Major applications of eddy-current testing are surface inspection and tubing inspections.

Radiographic Testing



Illustration 33g06090892
Radiographic Testing

All personnel involved in radiographic examinations shall be qualified to Level 2 in accordance to standards stated in Table 6.



Illustration 34g00008666

This process is dangerous. Only qualified personnel and test equipment should be appointed to perform this type of testing.

Radiographic testing (RT) is a Non-Destructive Testing (NDT) method in which short wavelength of electromagnetic radiation is used to penetrate materials to find hidden discontinuities such as cracks. In radiographic testing, the test object is placed between the radiation source and the film, or x-ray detector. The electromagnetic radiation will penetrate the thickness of the test object and, when all the way through, will project onto the film any indications that have been in the path of the radiation waves.

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