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TM9-2815-224-34&P
Engine Maintenance (Cont)
GENERAL MAINTENANCE INSTRUCTIONS (CONT).
[ 2-5.
(3) Cuts or grooves parallel to ball or roller rotation, fatigue pits (not minor machine marks or
scratches and cracks found during magnetic part icle inspection) are causes for bearing rejection.
(4) Remove drain plugs from engine system components and inspect the sediment sticking to the
plug. Grit or fine metal particles may indicate actual or potential component failure. A few fine
particles are normal. This inspect ion will help to show defective parts before internal inspection
of the component.
(5) Guidelines for rejection of gears by visual inspection are not listed because of varying conditions
for gear application. The following descriptions of wear conditions may help to determine when
parts are defective.
(a) Initial pitting may occur when gears are first started in service. When pitting reduces local high
spots so there is still enough contact area to carry load without further impairment, initial
pitting is not serious.
(b) Destructive pitting continues to progress after initial pitting. If there is not enough contact area
remaining to carry the load, rapid destruction may occur from continued operation.
(c) Abrasive wear is surface damage caused by fine particles carried in lubricant or particles
imbedded in tooth surfaces. Particles may be metal, sand or scale, or other impurities in oil or
surrounding atmosphere.
(6) Inspect all hose surfaces for broken or frayed fabric. Check for breaks caused by sharp kinks or
contact with other parts of the truck. Inspect the fitting threads for damage. Replace any
defective part. After assembly and during initial vehicle operation period, check for leaks.
(7) Inspect all wiring harnesses for chafed or burned insulation. Inspect all terminal connectors for
loose connections and broken parts.
(8) Visually inspect all castings and weldments for cracks.
standing at the rear of the engine.
Section IV. ORGANIZATION OF MAINTENANCE PROCEDURES
Maintenance Procedures
procedures have repair procedures combined with the removal and installation, while others have a
separate paragraph for repair of components. Components that are removed, repaired, and installed at the
same level of maintenance, DS or GS, will have the repair procedure integrated into the same primary
paragraph.
Components which are removed and installed at one level of maintenance but are repaired at a different
level of maintenance, will have the removal and installation in one primary paragraph and the repair in
another. Components which are removed and installed (but not repaired) at one level of maintenance will
be sent to the next designated level of maintenance.
organized in accordance with the functional group codes (FGC) used in the Maintenance Allocation Chart
(MAC). However, should you have to disassemble the engine completely, table 2-1 is provided as a guide to
help you do so. The table gives the paragraphs (tasks), the technical manuals in which they are found, and
the recommended sequence in which the tasks should be performed in order to completely disassemble the
engine. Table 2-1 can also be used as a guide to reassemble an engine by following the sequence numbers
and tasks in the reverse order.
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