THE ENGINE CYLINDER BLOCK MAIN CAPS NEED TO BE INSPECTED ON CERTAIN 5130B AND 5230 EXCAVATORS; 994D, 992G AND 854G WHEEL LOADERS; 793C, 789C, 785C HAA, 785C, 785B, 777D HAA, 777D AND 776D OFF HIGHWAY TRUCKS; D11R TRACK TYPE TRACTORS; NEW AND REMAN 35 Caterpillar


THE ENGINE CYLINDER BLOCK MAIN CAPS NEED TO BE INSPECTED ON CERTAIN 5130B AND 5230 EXCAVATORS; 994D, 992G AND 854G WHEEL LOADERS; 793C, 789C, 785C HAA, 785C, 785B, 777D HAA, 777D AND 776D OFF HIGHWAY TRUCKS; D11R TRACK TYPE TRACTORS; NEW AND REMAN 35

Usage:

Caterpillar: Confidential Yellow
THE ENGINE CYLINDER BLOCK MAIN CAPS NEED TO BE INSPECTED ON CERTAIN 5130B AND 5230 EXCAVATORS; 994D, 992G AND 854G WHEEL LOADERS; 793C, 789C, 785C HAA, 785C, 785B, 777D HAA, 777D AND 776D OFF HIGHWAY TRUCKS; D11R TRACK TYPE TRACTORS; NEW AND REMAN 3500 EN
SEBE7290-03

May 8, 2000
(Revised July 2001)
U-138
A-110
AU-82
S-64
O-124


 
Priority

THE ENGINE CYLINDER BLOCK MAIN CAPS NEED TO BE INSPECTED ON CERTAIN 5130B AND 5230 EXCAVATORS; 994D, 992G AND 854G WHEEL LOADERS; 793C, 789C, 785C HAA, 785C, 785B, 777D HAA, 777D AND 776D OFF HIGHWAY TRUCKS; D11R TRACK TYPE TRACTORS; NEW AND REMAN 3500 ENGINES

1201
PI30025
NOTE: This Program must be administered as soon as possible. When reporting the repair, use "PI30025" as the Part number and "7751" as the Group Number, "56" as the Warranty Claim Description Code and "T" as the SIMS Description Code. Exception: If the repair is done after failure, use "PI30025" as the Part Number, "7751" as the Group Number, "96" as the Warranty Claim Description Code, and "Z" as the SIMS Description Code.

NOTE: The information supplied in this service letter may not be valid after the termination date of this program. Do not perform the work outlined in this Service Letter after the termination date without first contacting your Caterpillar product analyst.

NOTE: For the proper inspection and rework procedure of 3500 Commercial Engines, refer to PI30053

NOTE: This Revised Service Letter replaces the May 8, 2000 (Revised June 2001) Service Letter. Changes have been made to the Affected Product.

COMPLETION DATE

TERMINATION DATE

November 30, 2000 November 30, 2001

PROBLEM

A process was omitted during the manufacturing of certain 3500 Engine cylinder block main caps. Because of the omitted process, there is a chance the main cap may crack and cause the crank to operate unsupported. The unsupported operation of the crank may cause the crankshaft to break and may cause an engine failure.

AFFECTED PRODUCT

Model Identification Number

793C         ATY183
             4GZ94-135, 138-202, 204-208, 212-250, 256-260
             4AR376-379, 382-383, 385-424

789C         2BW90-133, 135-149

785C HAA     5AZ90-114, 264-266, 268, 269

785C         APX160-164
             1HW87?131
785B         6HK958, 963, 966-969, 971-981, 983?987

777D HAA     2YW99-105

777D         AGC77-160, 165, 167-170, 173-176
             3PR874-1126
776D         5ER94-127
D11R         AAF132
             7PZ286-292, 294-299
             9TR304-473
             9XR160-189
5130B        4CS155-160, 162, 164-165


5230         7LL99-100

994D         3TZ251-265

992G         ADZ127-130, 132-133
             7HR254-256, 258-335, 338-386

854G         1JW237-244

ANY MACHINE SERIAL NUMBERS WITH THE FOLLOWING NEW OR REMAN ENGINES INSTALLED.

3508 MUI         99W03529-3540
                 4ZL539, 543-545, 551, 554, 556, 558, 561, 573, 575, 576,
                 586-588, 590, 593-596, 598-600, 604, 606, 607, 613, 618,
                 626, 628, 629, 633, 635, 636, 638, 639, 643, 645, 647, 649,
                 655, 657, 659, 661

3508 EUI         7YG02171-2178, 2180-2181, 2184-2190
                 5TL298-300, 305, 306, 315, 316, 321, 330, 334, 336, 338,
                 346, 349, 351, 362, 365,369, 370-376, 379, 380, 386, 390

3508 "B"         2GR1448-1945, 1947-1960, 1962-1965, 1967-2040,
                 2042-2142, 2144?2189, 2191-2195, 2197-2222,
                 2224?2226, 2228-2230, 2232-2240, 2242-2255,
                 2259-2261, 2263-2265, 2267, 2268, 2270, 2271,
                 2273-2275, 2277-2282, 2284, 2286, 2287, 2290-2292,
                 2294, 2298, 2299, 2303, 2306, 2307, 2309, 2313, 2321,
                 2326, 2332, 2337

                                       5XS171-178, 180-182


3512 MUI         96Z932-934
                 5EL201-203, 211, 213

3512 EUI         4WJ1228-1257
                 6FL208, 220, 225, 230, 236, 238, 259, 261, 269-270,
                 276-278, 284,289-290, 292, 294, 299-300, 302, 304, 399,
                 401, 403

3512 "B"         8BR544-598, 601, 604-605, 607, 614-617

3516 MUI         54Z1192-1197
                 6CL316, 319, 321, 326, 332, 336, 337, 340-343, 346-350, 352, 356
3516 EUI         2PK1565-1591, 1595, 1598, 1607
                 7CL580-581, 591-596, 600, 609-611, 618-620, 625,
                 631, 637, 638, 643-645, 649, 653, 654, 656, 658,
                 661, 665, 666, 670, 671, 673, 674, 680, 681-684,
                 687, 689-700, 702, 708, 710-713, 715, 717, 718,
                 720, 729, 735, 738-740, 746, 753, 754, 756, 758-762,
                 764, 765, 767, 772, 774, 776-780, 782, 785, 788-792,
                 794-797, 799, 800, 803, 806, 807, 811, 815, 818, 820,
                 822, 823, 826, 829, 831, 832, 834, 835, 842, 843

3516"B"          7TR573-790, 793-836, 838-859, 861-865, 867-871, 875,
                 881-887, 889-904, 906, 909-911, 913-926, 930-941,
                 943-945, 947-951, 954, 955, 959, 960, 962, 964, 965,
                 970-974, 978-994
                 7DS154-158, 162-166, 169, 170, 172-177, 180, 181

MACHINE MODELS LISTED ABOVE WITH ANY OF THE FOLLOWING CYLINDER BLOCKS INSTALLED.

CYLINDER BLOCKS

3508 115-3503 BLOCK AS. CYL. (SEQUENCE NO. 62A-001 - 94A-999)
3512 115-5154 BLOCK AS. CYL (SEQUENCE NO. 62B-001 ? 94B-999)
3516 115-5160 BLOCK AS. CYL. (SEQUENCE NO. 62C-001 - 93C-999)

NOTE: THE BLOCK SEQUENCE NUMBER IS LOCATED ON THE HORIZONTAL SURFACE ON THE TOP OF THE BLOCK BETWEEN CYLINDER #1 AND THE FRONT HOUSING. ENGINES AT OVERHAUL

Every effort should be made to inspect and peen all affected engines immediately. However, if any of the above listed engines have reached overhaul or do not have the 'D05' or 'R05' stamp during overhaul, these engines should be inspected for cracks and needle peened during the overhaul.

PARTS NEEDED

8 CYL. ONLY
1 - 7E-2631 GASKET-OIL
2 - 132-6260 SEAL-INTEGRAL

12 CYL. ONLY
1 - 7E-2630 GASKET-OIL
1 - 142-4159 SEAL-INTEGRAL

16 CYL. ONLY
1 - 7E-2632 GASKET-OIL
1 - 142-4159 SEAL-INTEGRAL
ALL
1 - 7M-7260 GASKET MAKER
2 - 3P-0657 SEAL-O-RING
1 - 6V-5101 SEAL-O-RING
2 - 109-2332 SEAL-O-RING

ACTION REQUIRED

See the attached Rework Procedure.

OWNER NOTIFICATION

U.S. and Canadian owners will receive the attached Owner Notification.
 

SERVICE CLAIM ALLOWANCES

Service Claim Allowances for Required Tooling
Part Hours
Caterpillar
Parts(D/N)
Dealer Suggested Parts
Customer Suggested Parts
       
Costs associated with Needle Peening tool.
Unlimited Hours
100%
0%
0%
       
Costs associated with Magnetic Particle Inspection Tooling or outside charges provided the dealer is not to qualified to do the inspection.
Unlimited Hours
100%
0%
0%
Product
Caterpillar
Dealer Suggested
Customer Suggested
 
Parts
Labor Hrs
Parts
Labor Hrs
Parts
Labor Hrs
793C
100%
24
0
0
0
0
789C
100%
24
0
0
0
0
785C HAA
100%
24
0
0
0
0
785B, 785C
100%
22
0
0
0
0
777D HAA
100%
22
0
0
0
0
777D/776D
100%
18
0
0
0
0
994D
100%
24
0
0
0
0
992G
100%
18
0
0
0
0
854G
100%
18
0
0
0
0
5230
100%
24
0
0
0
0
5130B
100%
18
0
0
0
0
D11R
100%
24
0
0
0
0
***** At Overhaul *****
3508
0
2
0
0
0
0
3512
0
3
0
0
0
0
3516
0
4
0
0
0
0

PARTS DISPOSITION

Handle the parts in accordance with your Warranty Bulletin on warranty parts handling.

MAKE EVERY EFFORT TO COMPLETE THIS PROGRAM AS SOON AS POSSIBLE.

Attach. (1-Owner Notification)
        (1-Rework Procedure)
        (1-Appendix)

COPY OF OWNER NOTIFICATION FOR U.S. AND CANADIAN OWNERS

XYZ Corporation
3240 Arrow Drive
Anywhere, YZ 99999

PRIORITY - THE ENGINE CYLINDER BLOCK MAIN CAPS NEED TO BE INSPECTED

MODELS INVOLVED - CERTAIN 5130B AND 5230 EXCAVATORS; 994D, 992G AND 854G WHEEL LOADERS; 789C, 793C, 785C HAA, 777D AND 776D OFF HIGHWAY TRUCKS; D11R TRACK TYPE TRACTORS; NEW AND REMAN 3500 ENGINES

Dear Caterpillar Product Owner:

A process was omitted during the manufacturing of certain 3500 Engine cylinder block main caps. Because of the omitted process, there is a chance the main cap may crack and cause the crank to operate unsupported. The unsupported operation of the crank may cause the crankshaft to break and may cause an engine failure. The main caps need to be inspected in the products listed below. You will not be charged for the service performed.

Contact your local Caterpillar dealer immediately to schedule this service. The dealer will advise you of the time required to complete this service. Please refer the dealer to their Service Letter dated May 8, 2000 when scheduling this service.

We regret the inconvenience this may cause you, but urge you to have this service performed as soon as possible to prevent unscheduled downtime.

Caterpillar Inc.

Identification #(s)
Attached to May 8, 2000 Service Letter

Rework Procedure

Required Tools:

  • 1933289 (115V) or 1933290 (230V) - AC magnetic particle inspection kit.
The following inspection tools can be used in place of the above listed kits.
    • AC magnetic particle inspection yoke1.
    • Longwave UV lamp (3650 angstrom wavelength; minimum 1000 micro w/cm2 intensity)1
  • 195-4730 Can of Commercial, fluorescent magnetic particles in suspension, preferably oil1
Note: One Can of fluorescent particles is enough to inspect up to ten engines.
  • 190-0783 peen tool or a needle peen air tool with between 12 and 20 rounded tip steel needles 3 mm (3/16 inch) in diameter.
  • A 193-0396 Peen Tool can be used for D11 engines due to the limited access created by the frame cross-member. The 193-0396 Peen tool is a compact peen tool used for peening commercial engines.
NOTE: Flat needles may be used if first rounded on a grinder. Only slight rounding of the needle edges is required.
  • Rubber to protect machined surfaces during peening (included with the 190-0783 peening tool).
NOTE: Multiple engines can be reworked with a single tool. 1See Appendix A at the end of this procedure for part numbers and tool suppliers.

This rework program shall be carried out with the bearing caps installed in the engine and the engine in the machine chassis.

The oil pan will have to be removed and covered to prevent excess debris from getting in the oil system.

This repair is best made during an oil change since the oil will have to be drained to remove the oil pan.

  1. Magnetic Particle Inspection ? Engines that have been in service must have all main caps inspected for cracks using magnetic particle inspection. Magnetic particle inspection is not required for engines that have not yet been placed into service.

  2. The magnetic particle inspection yoke must use alternating current (AC) to prevent excess residual magnetism.

DO NOT use an AC magnetic inspection tool that uses electrical current through the main bearing cap. ONLY use a tool that places a magnetic field through the cap.

When performing the inspection inside the engine, wet florescent magnetic particles should be used since black particles will be difficult to see. Dry particle testing is not recommended due to low sensitivity.

  • Use a cloth to thoroughly clean any oil from the bottom surface of the main cap.
  • Inspect the entire length of the 2 fillets on the bottom of the main cap for cracks. Refer to Illustration 1 for the location of possible crack origination. Refer to Illustrations 2 and 3 for yoke placement.
  • Energize the yoke on the cap to induce the magnetic field. Apply the magnetic particle solution between the feet of the yoke while the yoke is energized.
  • Discontinue solution prior to stopping alternating current.
  • Both front and rear of each fillet must be magnetized since alternating current does not extend through the width of the cap.
  • Using appropriate ultraviolet light source, illuminate the radius and inspect for crack indications. If present, cracks will appear at the root of the fillet radius as shown in Illustration 4. A hood or other means of blocking out ambient light may be needed to detect very small cracks.
  • No cracks in the main cap are permitted. Cracks are not repairable. Do not perform the remainder of this procedure if any cracks are found.
NOTE: If a cap is found to be cracked or broken, the engine must be repaired immediately. This repair will include removing the engine from the chassis.

Engine repair options include:

    • Replace the cracked cap and line bore the block.
    • Replacement of the block.
    • Installation of a Reman or dealer swing engine.
Dealers are expected to follow the normal warranty guidelines of repair verses replacement of the engine.
  • Demagnetize the cap after inspection by placing and energizing the yoke at previous locations and drawing yoke away while still energized. Draw the yoke away from any magnetizable components for a distance of at least 12-15 inches before discontinuing the current. This will avoid inadvertently re-magnetizing any engine components. However, it is not necessary to perform the demag operation slowly. The inspector can draw the yoke away rapidly and still be successful in demagnetizing.

Illustration 1


 


Illustration 2. Location of AC yoke for magnetic particle inspection

Illustration 3. Location of AC yoke avoiding counterweight for magnetic particle inspection.

Illustration 4. Small crack at root of main cap fillet radius seen using magnetic particle inspection method

Illustration 5 - Main cap bevel (A), cast surface (B), root of fillet radius (C), and duct tape (D) securing rubber peening mask.

Illustration 6 ? Rectangle shows area to be peened. Protect machined surfaces when reworking outside engine

  1. Remove the engine oil pan as instructed by the Disassembly and Assembly Manual for the particular machine being reworked.
  2. Needle peen the entire rough cast area on the bottom of the cap inside the rectangle shown in Illustration 6. The main areas of concern are the roots of the fillet radii along the bottom of the cap shown in Illustration 5, item C. Peen over the edge of the flat surface onto the bevel shown in Illustration 5. Peening should stop on the bevel. It is not necessary and not recommended to peen over the edge of the bevel onto the machined surface on the side of the main cap.
  • The machined bolt seat face should be protected while peening. When reworking outside the engine, use a 6 mm (1/4 inch) thick piece of rubber secured by duct tape as shown in Illustration 5. When reworking in the engine, use a 6mm (1/4 inch) thick piece of rubber that stretches over the bolt heads as shown in Illustration 7. Other similar methods of protecting the machined surfaces may also be used. One such method is four layers of duct tape over machined surfaces next to peening locations.
  • Peen with a 190-0783 or similar peening tool
  • Supply air pressure between 552 and 758 kPa (80 and 110 psi) to the peening tool.
  • Peen with between 12 and 20 rounded tip steel needles 3 mm (3/16 inch) in diameter. Do not use flat tipped or square shaped needles. The edges of flat tipped needles may be rounded off using a grinder if necessary.
  • Peen the area shown in Illustration 6 for a duration of approximately 3 minutes. Spend most of the time along the radii of the cap where the bolt faces transition to the bottom of the cap where the part number is located as indicated by the circled section in Figure 1. There is little risk of damage by peening too long. However, no additional benefit will be gained by additional peening. Peening the area for less than 3 minutes may not give the necessary material enhancement.
  • The peening angle should be approximately perpendicular to the cap. See Illustrations 8, 9, and 10
  • It may be necessary to rotate the engine so that crankshaft counterweights do not interfere with the peening process.

Illustration 7. Protecting machined surfaces when reworking inside engine.

Illustration 8. Peen starting at the base of one fillet.
 
 

Illustration 9. Continue peening across the entire as cast surface.



Illustration 10. Continue peening all the way into the base of the opposite fillet.

Note: The entire process should be at least three minutes. Going back over already peened surfaces is acceptable.

  1. Clean the main caps by wiping with a clean, oiled rag or some other method to remove any loose debris.
  2. Wipe down the connecting rods, pistons, and bottom end of the liners with a clean, oiled rag to remove any loose debris.
6.Stamp "D05" on the block adjacent to the serial number plate. The serial number plate is located on the left hand side of the engine at the rear of the block. Appendix A
Item Description Manufacturer Mfg Model No. Mfg Part No.
Magnetizing Yoke AC - 115V, 50/60 Hz
Magnaflux
Y-6
43530
Magnetizing Yoke AC ? 220V, 50/60 Hz
Magnaflux
Y-6
43540
Magnetizing Yoke AC ? 220V, 50 Hz
Tiede
JWM 220
075 001
         
UV Light & Transformer 115V, 60 Hz (also available 220V, 50Hz); Carrying handle for portability
Magnaflux
ZB-100P
600040
UV Light & Transformer 115V, 60 Hz (also available 220V, 50Hz), No carrying handle 
Magnaflux
ZB-100
600000
UV Light & Transformer Available for any power source?
Spectroline
MB-100 or SB-100P or C-100 or SSC-100
Same
UV Light & Transformer 220V, 50H
Tiede
 
121 001
         
Replacement bulb for UV lamp 100W
Magnaflux
 
507320
Replacement bulb for UV lamp 100W, Spot bulb
Spectroline
100S
100S
Replacement bulb for UV lamp 100 W
Tiede
 
121 101
         
Fluorescent particles in oil Aerosol, case of 12? Cans
Magnaflux
14AM
14AM
Fluorescent particles in oil Aerosol, 400ml
Tiede
Fluoflux
690.1

Magnaflux: Product as well as U.S. & International Sales Rep. Info can be obtained at: http://www.magnaflux.com/

Offices: 3624 W. Lake Ave / Glenwood, IL 60025, USA / Phone: 847-657-5300 / Fax: 847-657-5388
Faraday Rd, S.Dorcan Industrial Estate / Swindon, Wiltshire, SN3 5HE, England / Phone: 44-793-524566
5, SP Road, Begumpet / Hyderabad 500 016, India / Phone: 91-40-814892
Rua Piratininga / 235-Jardim Ruyce / 09990-020-Diadema-SP / Brazil / Phone: 011-55-713-2044

Tiede: Web site: http://www.tiede.de/

Tiede GmbH + Co / Rissprüfanlagen / Bahnhofstraße 94 ? 98 /D-73457 Essingen / Germany / 49(0)7365 81-0
CANDET / 124 Skyway Avenue / Rexdale, Ontario M9W 4Y9 / Canada / phone: 001 - 4162138000
Av. Independencia #1850, 1 erPiso / Jardines dela Concepcion /20120 Aguascalientes / Mexico/0052? 49123700
Av. Belgrano 369 / AR - 1092 Buenos Aires / Argentina / Telephone: 0054 - 1143314503
Unit 5, 8th Floor, Kodak House II / 39 Healthy Street East / North Point / Hongkong /Ph: 00852 - 28563280
N.S.W. Office/ 551 Pittwater Rd. / 2100 Brookvale / Australia / Telephone: 0061 - 9285700

Spectronics/Spectroline: 956 Brush Hollow Rd / Westbury NY 11590 / USA / Phone: 1-800-274-8888

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