3-32. DC MOTOR
This task covers:
C. REPAIR (AVIM)
Tool Kit, Aircraft Mechanics General, NSN 5180-00-323-4692
MOS 67 and MOS 68X
Paragraph 3-17 Gear Pump and Motor Assembly removed
Paragraph 3-33 Flexible Coupling removed
Check security of dc motor (1) mounting.
Check for failure of dc motor.
Check condition of electric wires and security of pump mounting.
Remove gear pump (2) and flexible coupling (3 and 4) in accordance with procedures of paragraphs 3-17 and 3-33
Remove six screws (5) and lock washers (6) and lift off rear case plate (7).
Tag all disconnected wiring to ease installation.
Remove attaching hardware and remove motor wire terminals. Tag them.
Remove six screws (8) and lock washers (9) connecting motor pump adapter (10) to case (11). Remove case (11).
Remove four capscrews (12) and lock washers (13) connecting motor pump adapter (10) to the cabinet.
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