Quantcast 3-11.4.  Inspection.

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ARMY TM 9-2815-255-24 AIR FORCE TO 38G1-95-2 MARINE CORPS TM 2815-24/4 f. Remove bolts (16), diode-trio (17), strap (14), and rectifier bridge (18) from rear housing (20). CAUTION Do  not  Insert  screwdriver  blades  deeper  than  1/16  Inch  (1.587  mm)  to  avoid  damaging  stator winding. g. Match mark front and rear housings, and remove through bolts (19).  Insert two flat tip screwdrivers in opposite openings between stator (22) and rear housing (20), refer to FIGURE 3-7. h. Pry units apart and remove rear housing (20, FIGURE 3-6) and stator (22) from front housing (30). NOTE To remove nut (23), place rotor assembly in a soft-jawed vise. i. Remove nut (23), lockwasher (24), pulley (25), fan (26), spacer (27), and woodruff key (28) from rotor assembly (29) shaft. j. Using arbor press, remove rotor assembly (29) from front housing (30). k. Remove bearing retaining screws (31) and press bearing (32) from front housing (30). 3-11.4.  Inspection. a. Inspect  brushes  for  cracks,  grooves  on  sides,  being  oil  soaked,  and  that  they  are  at  least  0.1875  inch  (4.7625 mm) long. b. Inspect rear housing for cracked or broken casting, stripped threads, and severe wear of rear bearing bore. c. Inspect fan for cracked or broken fins and for worn mounting hole. d. Inspect front housing for cracked or broken casting, stripped threads, and bore of mounting foot for elongation. 3-28


 


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